阅读说明：本技术 两次做功应用的压力气体活塞喷送型旋转式发动机系统 (Pressure gas piston spraying type rotary engine system applied by two-time work doing ) 是由 施炳根 于 2018-08-29 设计创作，主要内容包括：本发明提供了两次做功应用的压力气体(含蒸汽)活塞喷送型旋转式发动机系统,作为压力气体动力能源应用模式的一次新的变革；在压力气体的应用形式上改变一次输入通过压力或释放做功的方式,通过改变应用结构,让压力气体在一次输入后实现两次应用做功的方式,让活塞在受压模式下变为圆周率同心旋转不间断运行的全部做功工作方法,并且将由活塞送入的压力气体通过压力做功后在储存的方式下进行第二次的透平释放做功应用,从而改变压力气体应用热效率低的现状,实现及完善真正高效节能的能源应用技术。本发明从科学技术和实际意义上定义和确定压力气体在应用领域实现新的利用方法,真正达到能源的完全利用,实现更加高效的压力气体内能应用模式。(The invention provides a pressure gas (containing steam) piston spraying type rotary engine system applied by two-time work, which is used as a new revolution of a pressure gas power energy application mode; the method changes the mode of once input and applying work through pressure or releasing work in the application form of pressure gas, changes the application structure to realize the mode of applying work twice after the pressure gas is once input, changes the piston into a whole work applying method of circular-rate concentric rotation uninterrupted operation in a pressure mode, and performs the second turbine releasing work applying in a storage mode after the pressure gas fed by the piston applies work through pressure, thereby changing the current situation of low thermal efficiency of the pressure gas application, and realizing and perfecting the energy application technology of real high efficiency and energy saving. The invention defines and determines a new utilization method of the pressure gas in the application field from the scientific and technical and practical meanings, thereby truly achieving the complete utilization of energy and realizing a more efficient internal energy application mode of the pressure gas.)

1. Pressure gas piston spraying type rotary engine system applied by two-time work, which comprises a plane base (51) and is characterized in that: the top of the plane base (51) is sequentially provided with a left bearing seat, a middle bearing seat and a right bearing seat from left to right, sunken tables are arranged in the left bearing seat and the middle bearing seat, and a first-stage acting unit (2) and a second-stage acting unit (21) are sequentially arranged in the sunken tables from right to left; a rotary bearing A (31) is arranged in a right bearing seat, a plane thrust bearing (32) is arranged in an intermediate bearing seat, a rotary bearing B (33) is arranged in a left bearing seat, the centers of the rotary bearing A (31) and the rotary bearing B (33) are provided with a shaft (1), the shaft (1) is of a two-section stepped shaft structure, the left ends of the two-section stepped shaft structure are small ends and are solid shafts, the right ends of the two-section stepped shaft structure are large ends, the right part of the large end is a hollow shaft, a plurality of gas conveying holes which are arranged at equal intervals are arranged on the left cylindrical surface of the hollow shaft, and the outer ring of each gas conveying hole is provided with a; the first-stage working unit (2) and the second-stage working unit (21) simultaneously complete the application of two working operations on the same concentric shaft; the two-time acting design technology is based on the acting of applying piston type pressure acting, pressure gas impulse of a steam turbine and turbine release moving mass expansion;

the first-stage working unit (2) comprises a first-stage rotor (3) and a stator on the outer ring of the first-stage rotor (3), the stator consists of a front stator (52), a middle stator (53) and a rear stator (16), and the stator on the outer ring of the shaft (1) is sequentially arranged into the front stator (52), the middle stator (53) and the rear stator (16) from right to left; a plurality of groups of gas transmission pipelines (4) which are arranged at equal intervals along the axial direction are arranged inside the first-stage rotor (3), and each group of gas transmission pipelines (4) consists of uniformly distributed channels; a piston (5) is arranged between the outer ring of the first-stage rotor (3) and the inner ring of the stator, a plurality of groups of piston spray holes (6) which are arranged at equal intervals along the axial direction are arranged on the piston (5), and each group of piston spray holes (6) consists of uniformly distributed jet holes; each gas transmission pipeline (4) is communicated with a gas transmission hole of the hollow shaft and a piston spray hole (6);

the first-stage work applying unit (2) forms a cylinder (8), a cavity (7) is arranged in the cylinder (8), and the cavity (7) is communicated with the hollow shaft of the shaft (1) through a piston spray hole (6) and a gas transmission pipeline (4); a plurality of valves (9) uniformly distributed around the circumference are arranged on the inner ring of the cylinder (8), and the valves (9) can be opened and closed along with the moving position of the piston (5), so that a partition space is formed in the cavity (7);

a plurality of exhaust holes A (10) uniformly distributed around the circumference are formed in the first-stage rotor (3), the exhaust holes A (10) are of an inclined surface structure, angular discharge spray holes (11) are formed in the inclined surface structure, the tail ends of the discharge spray holes (11) are connected with an angular nozzle (12) through a one-way valve (25), and the angular nozzle (12) can spray and release pressure gas stored in the cavity (7);

the rear stator (16) is provided with a plurality of flow guide holes (13) uniformly distributed around the circumference, the flow guide holes (13) are of a kidney-shaped hole structure, the angular nozzle (12) can alternately release the moving work of the pressure gas mass through the flow guide holes (13) and eject the residual pressure gas to the exhaust hole B (20) through the exhaust air receiving hole (15);

the second-stage work unit (21) comprises moving blades (17) and additional moving blades (22) on a first rotor, and the second-stage work unit (21) is formed in a way that an angular nozzle (12) of the first-stage work unit is jetted to the moving blades (17) and an exhaust air receiving hole (15) of the second stage through a flow guide hole (13) in a cover plate of a rear stator (16), and is jetted to the additional moving blades (22) of the work unit of the second-stage work unit (21) through an exhaust hole B (20); the internal energy of all pressure gas is released and moved to the second moving blade (18) and the subsequent moving blade (19) through the phase-changing guide hole of the first moving blade (17) and the system of the second-stage working units of the third and fourth rotors, thus completing the work of the internal energy and the mass of the whole pressure gas.

2. The working method of the pressure gas piston spraying type rotary engine system applied by two-time work doing is characterized in that: the method comprises the following operation steps:

1) and pressure gas conveying:

pressure gas is sent to the center of a first-stage rotor (3) of a first-stage power unit (2) through a gas delivery hole on a hollow shaft section of a shaft (1);

2) and forming a partition space in the cavity:

pressure gas is sequentially sent into a piston spray hole (6) on a piston (5) and a cavity (7) of a cylinder (8) through a gas transmission pipeline (4) in a first-stage rotor (3), a valve (9) can be opened and closed along with the moving position of the piston (5), and when the valve (9) is closed, a plurality of cavities (7) for isolating space are formed in the cylinder (8); the cavity (7) is a partition space for storing pressure gas;

3) and doing work for the first time:

in the cavity (7), the pressure gas is fed into the cavity along with the piston spray hole (6) and generates a reaction force on the piston (5) along with the rising of the pressure, the piston (5) rotates and moves along with the first-stage rotor (3) when being pressurized, and the movement of the piston (5) determines the application of the first work of the piston (5); when the piston (5) moves a certain distance, the valve (9) in the cylinder (8) is automatically closed; the pressure gas sent through the piston spray hole (6) is stored in the confined cavity (7) space, the cavity (7) acts on the piston (5) under the pressure of the entering gas and the reaction force of the injection (6) on the piston (5) to be used as mechanical work movement, the flow of first-stage work is determined, namely work is performed in a pressure mode, and the movement speed of the piston (5) is limited by selecting the specification of the gas pipeline conveying speed and the application of the valve (9); the piston (5) continuously moves in an overload low-speed mode;

because the pressure gas stored in the cavity (7) needs to be released after performing pressure work, the pressure gas is sent into the second-stage work system (21) through the exhaust hole A (10) on the first-stage rotor (3) and the angular nozzle (12) and performs jet work; the function of additional work is generated on the first-stage rotor, the additional work is added to the first-stage work unit and is obtained as the added 1 energy of the first-stage work, and the first-stage work efficiency is increased;

4) and performing work for the second time:

the pressure gas stored in the cavity (7) is released by doing work for the first time, and the pressure in the cavity (7) is exhausted, the gas is sprayed to a first moving blade (17) and an exhaust gas receiving hole (15) in a second-stage power unit (21) through a gas exhaust hole A (10) and an angular nozzle (12) through a flow guide hole (13) on a stator to do work and exhaust, the sprayed pressure gas is sent to the moving blade (17) and an additional moving blade (22) of the second-stage power unit (21), the moving blade (17) is used for reversing to be sprayed to the moving blade at the back and comprises a second moving blade (18) and a subsequent moving blade (19) to enter a system cavity of the second-stage power unit (21), the work application of the pressure gas mass moving energy released by all turbines of the second stage is completed, and the additional moving blade (22) is an auxiliary blade which is arranged outside the moving blade (17) and uses the exhaust gas to do;

the stored gas is in the process of working application through the second stage, the residual gas in the cavity (7) needs to be emptied in the final application stage, the emptying mode is that the residual gas passes through an exhaust hole A (10) and an angular nozzle (12) through an exhaust air receiving hole (15) formed in a cover plate of a rear stator (16), is conveyed to an emptying exhaust hole B (20) through a pipeline on the stator and is injected to an additional movable blade (22) on the outer side of the movable blade (17) to be emptied, the emptying energy is used for assisting in reusing the available working, the conventional atmosphere non-pressure space design is arranged behind the additional movable blade (22), and the second stage of all-release working application is completed.

3. The application of the pressure gas piston spraying type rotary engine system applied by two-time work is characterized in that: the first-stage working unit (2) adopts the working principle that a circumferential concentric rotary piston nozzle continuously sprays pressure gas, a switch valve (9) is additionally arranged in a cavity (7) of a cylinder (8) with a unidirectional positive circumferential rotary piston running, a plurality of independent separated cavity spaces are created in the cavity of the piston cylinder to form an independently sealed cylinder separated cavity, the pressure gas fed by the piston (5) for first working is separated and stored, and then the gas mass movement working application of second-time flush penetration and flat release is carried out, so that after the piston (5) is pressed to move and work in the process of conveying the pressure gas, the pressure gas is enabled to continuously do work released by a turbine for the second time, and the pressure of the pressure gas and the movement energy of the released gas mass are completely utilized to do work;

the input and output of the pressure gas are all completed in the whole of the concentric rotor of the piston to complete all work doing processes, the pressure gas is fed in through the center of the shaft (1) and is fed into the spray holes on the piston head through the center of the first-stage rotor (3) and the inner gas transmission pipeline (4) to do a mode of uninterruptedly spraying and conveying the pressure gas, after the first pressure moving work doing of the piston (5) is completed, the pressure gas fed in by the piston (5) is isolated and stored, the stored pressure gas energy is sent out through the exhaust spray holes on the piston rotor and is fed into the second-stage system to do work released by the second turbine, and after the work doing of the whole pressure is realized by the rotary piston, the practical application mode of once input and twice work doing is realized by the whole pressure gas released by the second turbine.

4. Use of a pressurized gas piston-injection rotary engine system for two-work applications according to claim 3, characterized in that: the piston number is determined in a mode that one or more piston heads are arranged on the circumferential rotor rotating body according to the size of the rotor, the piston heads and the nozzle body are equally arranged on the rotating rotor body, the piston heads and the nozzles are in a flat rectangular structure, and the piston bodies and the nozzles move in an infinite distance along with the rotor in a piston cavity of the cylinder; the cavity exhaust holes A (10) and the angular nozzles (12) are arranged on the body of the rotor in the same number and at intervals as the pistons and synchronously rotate with the rotor of the piston, the exhaust holes A (10) and the angular nozzles (12) do the same injection work and are used for adding all work to the first-stage rotor, and the exhaust holes A (10) and the angular nozzles (12) have the function of releasing a pressure space behind the pistons to become an atmosphere or negative pressure space;

the pressure gas is fed through the piston, and rotates to do work after being subjected to pressure, the pressure gas is required to be released by a turbine after entering a partition space of a cylinder cavity for storage, and the stored pressure gas ejected through a first-stage rotor nozzle is determined to be fed into a second-stage conventional turbine for conventional application as a second-stage work application mode; the requirement of two release spaces is adopted for the evacuation of the stored pressure gas, namely an exhaust air receiving hole (15) and an exhaust hole B (20) are designed as the pressure in an evacuation cavity body (7), and a real pressure-free space is realized behind a piston.

5. Use of a pressurized gas piston-injection rotary engine system for two-work applications according to claim 3, characterized in that: the piston cylinder is internally provided with a switch valve to cause a cylinder cavity section distribution mode, so that an application mode of piston re-motion and energy storage re-output is completed; the valves are arranged on a stator in the piston cylinder, the number of the valves is an application structure mode that the number of piston heads is doubled and 1, so that the working mode of simultaneous impulse is cancelled in an alternative exhaust mode, and the valve section distribution resistance section application on the cylinder or the outer body of the stator is adopted, so that the pressurized movement of the piston and the release and injection of a piston rotor can be separately completed in two independent isolated cavity regions; the switch valve installed on the stator is opened and closed according to the moving position of the rotary piston.

6. Use of a pressurized gas piston-injection rotary engine system for two-work applications according to claim 3, characterized in that: the whole system controls the input of pressure gas at the front end, and the application of the load of the rotary piston system adopts an overload design, namely the load is greater than the maximum work output capacity of the first stage; the rotating speed is determined by the output magnitude of the load during the rotating work process of the rotating piston; under full load operation and with determined operating conditions, the pressure cross-sectional area and the displacement speed of the piston determine the total energy input into the pressure gas to be subsequently applied.

7. Use of a pressurized gas piston-injection rotary engine system for two-work applications according to claim 3, characterized in that: the whole system application matching platform is based on one or more balanced concentric basic platforms and consists of a first-stage rotary piston structure pressurized acting and a second-stage injection release turbine, and the two acting processes work on the same concentric balance center.

Technical Field

The invention belongs to the technical field of application of power energy, relates to an energy-saving and efficient environment-friendly product, in particular to a pressure gas (containing steam) piston spraying type rotary engine system applied by twice acting and application thereof, and belongs to the process of long-term application research and development, it was found that the gas pressure and the gas mass of all pressurized compressed gases (containing steam) can exist as two parts of two meaningful energies, only the structural application mode is realized to respectively utilize work, meanwhile, pressure power sources such as steam and various compressed pressure gases (including internal combustion engines, gas turbines and liquefied gases) are determined, all pressure gas energy sources can be used for performing work twice, and the method is suitable for various small pneumatic equipment applications and large steam turbines, including all occasions using pressure gas as energy exchange.

Background

At present, most power generation systems use natural fossil energy, and application systems are applied to thermal power generation, nuclear power generation, enterprise units, individuals and other occasions where pressure gas is converted into mechanical power. However, it would be a revolutionary result if two more efficient uses of the entire pressure gas (steam-containing) power source were made; the use of the pressure gas tool now has the advantages of safety, reliability and lightness, etc., resulting in a considerable market for applications, since the application of fossil electric energy and the application of whole pressure gas are a broad concept, everywhere in our lives and works, which is essential for our human lives and now, in the future, also for the production needs of the whole society. The requirements of development and life of socioeconomic society can not be separated from electric power, and the device is also a pressure gas application device tool. Along with the increasing demand of society and economy for developing energy, the storage of earth energy resources is less and less, which is a key contradiction between human survival and development, and the energy consumption has great influence on living environment and natural environment, and the influence of the energy consumption on the nature is an inevitable problem, so that people adopt various methods in the field to meet the requirement and saving of energy, and develop various green new energy applications while saving energy.

The utilization of power energy has been increasing over time, due to advances in technology and the development of materials, and the efficiency of power energy utilization has been increasing, for example, steam turbine applications have been moving from low pressure to medium, high, ultra-high, sub-critical, super-supercritical) applications over time. The application of the steam turbine mode is from the application of condensing steam type, heat supply type, back pressure type, steam extraction type steam turbines and the like, and the application of pressure gas is necessary in all fields of the whole society; various advanced equipment materials and processes have been developed in order to save energy as much as possible, and it is the aim of the people to provide the maximum mechanical power with the least energy, and therefore great efforts and costs are made for this purpose, and the common aim is to save energy by improving efficiency. The change of improving the application efficiency of the power source energy is the responsibility and obligation of our contemporary people, so the improvement of the application efficiency of the power source energy is the pursuit of our people, but for various reasons our applied systems are the application law of once exchange work, there is no real application structure breakthrough in this field, in the long-term application, the improvement of the application efficiency of the pressure gas from 5% to about 40% is a huge change, but only the improvement of the application efficiency by changing the application technology, because the basic mode and application definition concept of the application are not changed, the full utilization of the energy of pressure, temperature and enthalpy is really achieved, which is the aim and direction of our contemporary people's efforts. In the concept of people, the energy application in the world is expected to reach the highest use efficiency in the range of the law so as to achieve the purposes of effectively utilizing energy and saving energy.

There are now two modes in the applied pressure gas energy conversion device: there are medium and small piston type, vane type; applying work by adopting primary pressure; without taking advantage of the energy of the gas mass movement. The large-scale steam turbine is applied to mass movement energy released by the mass of the pressure gas, and is not applied to gas pressure, so that the key reason that all pressure gas application equipment at present has low heat efficiency is caused.

The method is characterized in that the method adopts a principle that the pressure gas cannot do work twice according to the principle of physically defining the law of conservation of energy, an important subject for determining the utilization of energy, a physical principle that the pressure gas cannot do work twice exists, if the internal energy of an object is changed by doing work only, the change of the internal energy can be measured by the amount of the work done, the increase (or decrease) amount △ U of the system is equal to the value of the work done on the object (or the object to the outside), namely △ U-W, the second concept of the work cannot exist according to the definition, the problem is that the invention adopts two concepts of space application, the other concept of ideal gas constant temperature reversible process is defined in the law of the heat energy, because psu-p, the energy cannot be generated and disappear by the space, can be converted from one form to the other form, or is transferred from one object to the other object, the total amount of the energy does not change in the processes of transfer and conversion, the original definition of the original pressure is that the original definition of the original pressure does not release the internal energy in the first process of the pressure application, but the gas energy can be converted from the other form, and the original definition of the original system, and the original reversible process, so that the original pressure can not change from the original system can be recovered from the original thermodynamic process, the original system, and the original system can be recovered from the original thermodynamic process, so that the original system can be recovered from the original thermodynamic process, the original system can be recovered from the original system, the original system can be recovered from the original system.

The low efficiency of the piston pressure gas engine originally adopted is that the piston engine has the working time with gaps, the working mode is the working mode that the pressure is from low to high and then from high to low, the working realizes the working application concept with curves, and the reciprocating motion of the piston causes the mechanical power loss, so the piston has the results of low efficiency and low power, and the success rate is limited because of the working mode with gaps and other reasons such as material process which can not be used. The blade-type pneumatic tools used at present also have the concepts of non-concentric torque and one-time application, so that the efficiency is low, and thus the blade-type pneumatic tools cannot be provided and utilized as high-power pressure gas application equipment. The high-power steam turbine can achieve higher heat energy efficiency utilization rate, but 40% heat efficiency is a relatively low figure. It is known that because the energy collection of the steam turbine adopts the mass motion mode of the pressure gas in the expansion process, the mass and efficiency of the impulse cannot fully represent the full utilization of the energy even though the impulse mode of the pressure gas is adopted, so that the application of the mass energy existing by the mass movement of the pressure gas to push the impeller to rotate to generate work is considered to be not fully utilized. The several power modes embodied in the application expression of the steam turbine are actually applied in a segmented manner in the concept from high to low, because in the application of the several power expressions, only the energy reuse mode supplemented again by the input is applied. One key reason for the existence of the problems obtained on the basis of the tests limits the fundamental problem of thermal efficiency utilization, namely, the limitation of thermal efficiency utilization is caused because all the application modes of the pressure gas are used for completing the feeding-working-releasing processes in the same space environment at present. The key technical problem to be realized and solved is to separate the application mode of energy collection in two spaces in two structural forms simultaneously by the pressure gas.

Disclosure of Invention

In view of the above-mentioned shortcomings of the prior art, the present invention aims to provide a pressurized gas piston injection rotary engine system for twice work application and its application, which is used to solve the problems of low thermal efficiency, great technical difficulty, high application technical requirements, material application fields, etc. of pressurized gas application equipment in the prior art.

In order to achieve the purpose, in long-term practice and application, the gas pressure and the gas quality of all pressure compressed gas (containing steam) can exist as two parts of two energies, and only a structural application mode is realized to respectively utilize and do work, so that a concept that two independent spaces are respectively applied and do work is determined; therefore, the pressure gas piston spraying type rotary engine system for two-time work application is defined, and the invention utilizes the pressure utilization of a piston and the gas mass release motion utilization of a steam turbine, for example, to realize the combined application concept of the two systems to complete the two-time work application.

The invention provides a pressure gas piston spraying type rotary engine system applied by doing work twice, which comprises a plane base and is characterized in that: the top of the plane base is sequentially provided with a left bearing seat, a middle bearing seat and a right bearing seat from left to right, sunken tables are arranged in the left bearing seat and the middle bearing seat, and a first-stage acting unit and a second-stage acting unit are sequentially arranged in the sunken tables from right to left; a rotary bearing A is arranged in the right bearing seat, a plane thrust bearing is arranged in the middle bearing seat, and the plane thrust bearing can be selected according to the pressure and the size of equipment; a rotary bearing B is arranged in the left bearing seat, a shaft is arranged at the centers of the rotary bearing A and the rotary bearing B, the shaft is of a two-section stepped shaft structure, the left end of the two-section stepped shaft structure is a small end and is a solid shaft, the right end of the two-section stepped shaft structure is a big end, the right part of the big end is a hollow shaft, a plurality of gas conveying holes which are arranged at equal intervals are arranged on the cylindrical surface of the left part of the hollow shaft, and a first-stage acting unit is arranged on the outer ring of each gas conveying hole; the first-stage working unit and the second-stage working unit simultaneously complete the application of two working operations on the same concentric shaft; the two-time acting design technology is based on the acting of applying piston type pressure acting, pressure gas impulse of a steam turbine and turbine release moving mass expansion;

the first-stage working unit comprises a first-stage rotor and a stator of an outer ring of the first-stage rotor, the stator consists of a front stator, a middle stator and a rear stator, and the stator of the outer ring of the shaft is sequentially arranged into the front stator, the middle stator and the rear stator from right to left; a plurality of groups of gas transmission pipelines which are arranged at equal intervals along the axial direction are arranged in the first-stage rotor, and each group of gas transmission pipelines consists of uniformly distributed channels; a piston is arranged between the outer ring of the first-stage rotor and the inner ring of the stator, a plurality of groups of piston spray holes are arranged on the piston at equal intervals along the axial direction, and each group of piston spray holes consists of uniformly distributed jet holes; each gas transmission pipeline is communicated with a gas transmission hole of the hollow shaft and a piston spray hole;

the first-stage acting unit forms a cylinder, a cavity is arranged in the cylinder, and the cavity is communicated with the hollow shaft of the shaft through a piston spray hole and a gas transmission pipeline; the inner ring of the cylinder is provided with a plurality of valves which are uniformly distributed around the circumference, and the valves can generate opening and closing states along with the moving position of the piston, so that a partition space is formed in the cavity;

a plurality of exhaust holes A which are uniformly distributed around the circumference are formed in the first-stage rotor, the exhaust holes A are of an inclined surface structure, angular discharge spray holes are formed in the inclined surface structure, the tail ends of the discharge spray holes are connected with an angular nozzle through a one-way valve, and the angular nozzle can spray and release pressure gas stored in the cavity;

the rear stator is provided with a plurality of flow guide holes which are uniformly distributed around the circumference, the flow guide holes are of a waist-shaped hole structure, the angular nozzles can alternately do work by moving the pressure gas mass released by the flow guide holes, and the residual pressure gas is released by ejecting from the exhaust hole to the exhaust hole B through the exhaust air receiving hole;

the second-stage acting unit comprises a moving blade and an additional moving blade on the first rotor, and the angular nozzle of the first-stage acting unit is jetted to the moving blade and an exhaust receiving hole of the second stage through a flow guide hole on a rear stator cover plate and is jetted to the additional moving blade of the acting part of the second-stage acting unit through an exhaust hole B; the pressure gas is transmitted to a second moving blade and a subsequent moving blade through a first moving blade phase-changing guide hole and a system of a second-stage acting unit of a third rotor and a fourth rotor to complete the acting of the internal energy mass release movement of all pressure gas; the description of the second stage work is to determine the technical application choice according to the size of the equipment and the pressure gas level.

The working method of the pressure gas piston spraying type rotary engine system applied by two-time work doing is characterized in that: the method comprises the following operation steps:

1) and pressure gas conveying:

sending pressure gas into the center of a first-stage rotor of a first-stage power unit through a gas delivery hole on a hollow shaft section of a shaft;

2) and forming a partition space in the cavity:

the pressure gas is sent into a piston spray hole on the piston and a cavity of the cylinder in sequence through a gas transmission pipeline in the first-stage rotor, the valve can be opened and closed along with the moving position of the piston, and when the valve is closed, a plurality of cavities for separating the space are formed in the cylinder; the cavity is a partition space for storing pressure gas;

3) and doing work for the first time:

in the cavity, pressure gas is fed along with a piston spray hole, the pressure gas generates reaction force on the piston along with the rising of pressure, the piston rotates and moves along with the first-stage rotor when being pressurized, and the application of the first acting of the piston is determined by the movement of the piston; when the piston moves a certain distance, the valve in the cylinder is automatically closed; the pressure gas sent in through the piston jet orifice is stored in the limited cavity space, and the cavity acts on the piston by the pressure of the gas entering the cavity and the reaction force of the jet to move the piston as mechanical work, so that the first-stage work flow is determined, namely, the work is performed in a pressure mode, and the moving speed of the piston is limited by selecting the specification of the gas pipeline conveying speed and the application of a valve; the piston continuously moves in an overload low-speed mode;

if we agree with the power calculation formula; the reality of TN/9550 is that the power of the first stage piston is a relatively high efficiency. So we define that the use of pressurized gas can be more thermally efficient;

because the pressure gas stored in the cavity needs to be released after the pressure gas does work, the pressure gas is sent into the second-stage work doing system through the exhaust hole A and the angular nozzle on the first-stage rotor and does work of injection at the same time; the function of additional work is generated on the first-stage rotor, the additional work is added to the first-stage work unit and is obtained as the added 1 energy of the first-stage work, and the first-stage work efficiency is increased;

4) and performing work for the second time:

the pressure gas stored in the cavity by first acting is released, the pressure in the cavity is exhausted, the pressure gas is sprayed to a first moving blade in a second-stage acting unit through a guide hole on a stator through an exhaust hole A and an angular nozzle to do acting and exhaust through an air hole, the sprayed pressure gas is sent to the moving blade and an additional moving blade of the second-stage acting unit, the moving blade which is sprayed to the back by the moving blade in a reversing way comprises the second moving blade and the subsequent moving blade and enters a system cavity of the second-stage acting unit, the acting application of the pressure gas mass moving energy released by all turbines of the second stage is completed, and the additional moving blade is an auxiliary blade which is arranged outside the moving blade and uses the exhaust to do work;

during the working application process of the second stage, the stored gas needs to be emptied for the residual gas in the cavity at the final application stage, the emptying mode is that the stored gas passes through an exhaust hole A from an angular nozzle injection hole through an exhaust gas receiving hole arranged on a rear stator cover plate, is sent to an emptying exhaust hole B through a pipeline on a stator and is injected to an additional movable blade on the outer side of the movable blade to be emptied, the emptying energy is used for assisting the reuse of available working, the conventional atmosphere non-pressure space design is arranged behind the additional movable blade, and the whole releasing working application of the second stage is completed; the second-stage working principle can refer to the conventional general working principle of steam turbine design and application.

The application of the pressure gas piston spraying type rotary engine system applied by two-time work is characterized in that: the first-stage working unit adopts the working principle that a circumferential concentric rotary piston nozzle continuously sprays pressure gas, a switch valve is additionally arranged in a cylinder cavity in which a unidirectional positive circumferential rotary piston operates, a plurality of independently partitioned cavity spaces are created in the cylinder cavity of the piston, the cylinder partitioned cavities which can be independently sealed are formed, the pressure gas fed by the piston by first working is partitioned and stored, and then gas mass movement work application of second-time flush and penetration release is carried out, so that the pressure gas continuously does work of turbine release for the second time after the piston is pressed to move and work in the process of conveying the pressure gas, and the pressure of the pressure gas and the release gas mass movement energy are completely utilized to do work;

the input and output of the pressure gas are all completed in the whole of the concentric rotor of the piston to complete all work doing processes, the pressure gas is fed in through the center of the shaft and is fed into the spray holes on the piston head through the center of the first-stage rotor and the internal gas transmission pipeline to do a mode of uninterruptedly spraying and conveying the pressure gas, after the first pressure moving work of the piston is completed, the pressure gas fed in by the piston is isolated and stored, the stored pressure gas energy is sent out through the exhaust spray holes on the rotor of the piston and is fed into the second-stage system to do work released by the second turbine, and after the work done by the rotary piston is realized, the actual application mode that the rotary piston releases all the pressure gas by the second turbine to realize continuous one-time input two-.

In one embodiment of the invention, the determination of the number of the pistons is an application mode that one or more piston heads are arranged on the circumferential rotor rotating body according to the size of the rotor, the piston heads and the nozzle body are equally arranged on the rotating rotor body, the structural forms of the piston heads and the nozzles adopt flat rectangular structures, and the piston bodies and the nozzles move with the rotor in an infinite distance in a piston cavity of the cylinder; the cavity air exhaust holes A and the angular nozzles are arranged on the rotor body in the same number and at intervals as the pistons and synchronously rotate with the piston rotor, the air exhaust holes A and the angular nozzles also perform jet work and are used for fully applying work to the first-stage rotor, and the functions of the air exhaust holes A and the angular nozzles are the functions of simultaneously releasing a pressure space behind the pistons to become an atmosphere or negative pressure space;

the pressure gas is fed through the piston, and rotates to do work after being subjected to pressure, the pressure gas is required to be released by a turbine after entering a partition space of a cylinder cavity for storage, and the stored pressure gas ejected through a first-stage rotor nozzle is determined to be fed into a second-stage conventional turbine for conventional application as a second-stage work application mode; the requirement of two release spaces is adopted for the evacuation of the stored pressure gas, namely, an exhaust air receiving hole and an exhaust hole B are designed as the pressure in an evacuation cavity, and a real pressure-free space is realized behind a piston.

In one embodiment of the invention, the piston cylinder is internally provided with a mode of increasing switch valves to cause the section-lattice distribution of a cylinder cavity, so as to finish the application mode of piston re-movement and energy storage re-output; the valves are arranged on a stator in the piston cylinder, the number of the valves is an application structure mode that the number of piston heads is doubled and 1, so that the working mode of simultaneous impulse is cancelled in an alternative exhaust mode, and the valve section distribution resistance section application on the cylinder or the outer body of the stator is adopted, so that the pressurized movement of the piston and the release and injection of a piston rotor can be separately completed in two independent isolated cavity regions; the switch valve installed on the stator is opened and closed according to the moving position of the rotary piston.

In one embodiment of the invention, the whole system controls the input of the front-end pressure gas, and the application of the rotary piston system load adopts an overload design, namely the load is greater than the first-stage maximum work output capacity; the rotating speed is determined by the output magnitude of the load during the rotating work process of the rotating piston; under full load operation and with determined operating conditions, the pressure cross-sectional area and the displacement speed of the piston determine the total energy input into the pressure gas to be subsequently applied.

In an embodiment of the invention, the whole system application matching platform is based on one or more balanced concentric basic platforms and consists of a first-stage rotary piston structure pressurized work application and a second-stage injection release turbine, and the two work application processes work on the same concentric balance center.

As described above, the pressure gas piston injection type rotary engine system for two-time work application of the present invention has the following advantageous effects: the application of pressure gas from feeding-impulse-releasing-turbine is changed, and a new application mode is generated by changing the application structure, namely the application mode is changed into the utilization of central feeding-injection-pressure working-storage-injection-impulse-releasing working, and the utilization and application of all internal energy are completed by definition; the working application of the two times is completed, the utilization efficiency of the pressure gas energy is improved, and the process of two-time collection is realized; the structural mode of piston application is changed into that the piston type steam turbine continuously inputs the steam turbine to apply rotary work under pressure and jet in a central mode, the use efficiency of the steam turbine is the same as or higher than that of the steam turbine, complete energy application can be achieved twice, and noise and vibration are reduced; the implementation mode that the pressure and the turbine work are released to complete the work in different spaces is realized by adopting the work mode of two spaces, so that the complete energy application for two times is achieved, and the utilization rate of the heat efficiency is improved; the technology for realizing the full utilization of the pressure gas energy is to separately collect the pressure of the pressure gas and the mass movement energy released by the gas, so that the internal energy pressure and the mass movement energy released by the pressure gas are collected in two parts and two spaces, and the aim of doing work twice can be fulfilled; a new utilization method of the pressure gas in the application field is defined and determined in scientific and technical and practical meanings, the full utilization of energy is really achieved by changing the application structure, and a more efficient internal energy application mode of the pressure gas is realized.

Drawings

FIG. 1 is a front view of the system architecture of the present invention.

Fig. 2 is a schematic diagram of the internal structure of the first stage work-doing unit of the present invention.

In the figure: 1. a shaft; 2. a first stage work applying unit; 3. a first stage rotor; 4. a gas pipeline; 5. a piston; 6. spraying a hole on the piston; 7. a cavity; 8. a cylinder; 9. a valve; 10. an exhaust hole A; 11. a discharge orifice; 12. an angular nozzle; 13. a flow guide hole; 15. an exhaust air receiving hole; 16. a rear stator; 17. moving blades; 18. a second moving blade; 19. moving the blade subsequently; 20. an exhaust hole B; 21. a second stage work-doing unit; 22. attaching a movable blade; 25. a one-way valve; 31. a rotating bearing A; 32. a planar thrust bearing; 33. a rotating bearing B; 51. a planar base; 52. a front stator; 53. and a middle stator.

Detailed Description

The following description of the embodiments of the present invention is provided for illustrative purposes, and other advantages and effects of the present invention will become apparent to those skilled in the art from the present disclosure.

Please refer to fig. 1-2. It should be understood that the structures, ratios, sizes, and the like shown in the drawings and described in the specification are only used for matching with the disclosure of the specification, so as to be understood and read by those skilled in the art, and are not used to limit the conditions under which the present invention can be implemented, so that the present invention has no technical significance, and any structural modification, ratio relationship change, or size adjustment should still fall within the scope of the present invention without affecting the efficacy and the achievable purpose of the present invention. In addition, the terms "upper", "lower", "left", "right", "middle" and "one" used in the present specification are for clarity of description, and are not intended to limit the scope of the present invention, and the relative relationship between the terms and the terms is not to be construed as a scope of the present invention.

Referring to fig. 1, a pressurized gas piston-injection rotary engine system for two-time work application includes a planar base 51, and is characterized in that: the top of the plane base 51 is sequentially provided with a left bearing seat, a middle bearing seat and a right bearing seat from left to right, sunken tables are arranged in the left bearing seat and the middle bearing seat, and a first-stage acting unit 2 and a second-stage acting unit 21 are sequentially arranged in the sunken tables from right to left; a rotary bearing A31 is arranged in the right bearing seat, a planar thrust bearing 32 is arranged in the middle bearing seat, a rotary bearing B33 is arranged in the left bearing seat, a shaft 1 is arranged at the centers of the rotary bearing A31 and the rotary bearing B33, the shaft 1 is of a two-section stepped shaft structure, the left end of the two-section stepped shaft structure is a small end and is a solid shaft, the right end of the two-section stepped shaft structure is a large end, the right part of the large end is a hollow shaft, a plurality of gas conveying holes which are arranged at equal intervals are arranged on the cylindrical surface of the left part of the hollow shaft, and a first-stage acting unit 2 is; the first-stage working unit 2 and the second-stage working unit 21 simultaneously complete the application of two working operations on the same concentric shaft; the two-time acting design technology is based on the acting of applying piston type pressure acting, pressure gas impulse of a steam turbine and turbine release moving mass expansion;

the first-stage power unit 2 comprises a first-stage rotor 3 and a stator on the outer ring of the first-stage rotor 3, the stator consists of a front stator 52, a middle stator 53 and a rear stator 16, and the stator on the outer ring of the shaft 1 is sequentially arranged from right to left into the front stator 52, the middle stator 53 and the rear stator 16; a plurality of groups of gas transmission pipelines 4 which are equidistantly arranged along the axial direction are arranged in the first-stage rotor 3, and each group of gas transmission pipelines 4 consists of uniformly distributed channels; a piston 5 is arranged between the outer ring of the first-stage rotor 3 and the inner ring of the stator, a plurality of groups of piston spray holes 6 which are arranged at equal intervals along the axial direction are arranged on the piston 5, and each group of piston spray holes 6 consists of uniformly distributed jet holes; each gas transmission pipeline 4 is communicated with a gas transmission hole of the hollow shaft and a piston spray hole 6;

referring to fig. 2, the first-stage acting unit 2 forms a cylinder 8, a cavity 7 is arranged in the cylinder 8, and the cavity 7 is communicated with the hollow shaft of the shaft 1 through a piston spray hole 6 and a gas transmission pipeline 4; a plurality of valves 9 uniformly distributed around the circumference are arranged on the inner ring of the cylinder 8, and the valves 9 can be opened and closed along with the moving position of the piston 5, so that a partition space is formed in the cavity 7;

a plurality of exhaust holes A10 uniformly distributed around the circumference are formed in the first-stage rotor 3, the exhaust holes A10 are of an inclined surface structure, angular discharge spray holes 11 are formed in the inclined surface structure, the tail ends of the discharge spray holes 11 are connected with an angular nozzle 12 through a one-way valve 25, and the angular nozzle 12 can spray and release pressure gas stored in the cavity 7;

the rear stator 16 is provided with a plurality of flow guide holes 13 uniformly distributed around the circumference, the flow guide holes 13 are of a waist-shaped hole structure, the angular nozzle 12 can alternately do work by moving the pressure gas mass released through the flow guide holes 13, and the residual pressure gas is released by ejecting the gas from the exhaust gas receiving hole 15 to the exhaust hole B20;

the second-stage work unit 21 comprises a moving blade 17 and an additional moving blade 22 on the first rotor, the angular nozzle 12 of the first-stage work unit is used for punching to the moving blade 17 and the exhaust air receiving hole 15 of the second stage through the flow guiding hole 13 on the cover plate of the rear stator 16, and the angular nozzle is used for punching to the additional moving blade 22 of the work unit of the second-stage work unit 21 through the exhaust hole B20; the internal energy mass of all pressure gas is released and moved to work in a system of a second-stage work unit of a second moving blade 18, a subsequent moving blade 19 and a third rotor and a fourth rotor through a first moving blade 17 phase-changing guide hole, so that the work of twice work can be realized by inputting one pressure gas; the working application of all pressures of the piston 5 and the first-stage rotor 3 is defined, the turbine release working application of the second stage is defined as a turbine application mode of general conventional application, and the specific technical application basis can refer to the technical specification of the turbine application as the reference basis of the invention; the second-stage working principle can refer to the conventional general working principle of steam turbine design and application; the description of the second stage of work is a matter of choice depending on the size of the plant and the high base pressure of the pressurized gas determining technology application.

The piston 5 is continuously moved in an overload low-speed mode; the energy loss of the piston 5 movement is the resistance of the steam pipeline and the pipeline temperature loss, and the piston 5 is designed by adopting a flat pitch type structure in consideration of the current application technology and switching speed of the valve 9, and the moving speed of the piston 5 is determined as a standard pipeline pressure gas conveying speed parameter.

The working method of the pressure gas piston spraying type rotary engine system applied by two-time work doing is characterized in that: the method comprises the following operation steps:

1) and pressure gas conveying:

pressure gas is sent to the center of a first-stage rotor 3 of a first-stage power unit 2 through a gas delivery hole on a hollow shaft section of a shaft 1;

2) and forming a partition space in the cavity:

pressure gas is sequentially sent into a piston spray hole 6 on a piston 5 and a cavity 7 of a cylinder 8 through a gas transmission pipeline 4 in a first-stage rotor 3, a valve 9 can be opened and closed along with the moving position of the piston 5, and when the valve 9 is closed, a plurality of cavities 7 for isolating space are formed in the cylinder 8; the cavity 7 is a partition space for storing pressure gas;

3) and doing work for the first time:

in the cavity 7, the pressure gas is fed into the cavity along with the piston spray hole 6, the reaction force is generated on the piston 5 along with the rising of the pressure, the piston 5 rotates and moves along with the first-stage rotor 3 when being pressurized, and the movement of the piston 5 determines the application of the piston 5 for doing work for the first time; when the piston 5 moves a certain distance, the valve 9 in the cylinder 8 is automatically closed; the pressure gas sent in through the piston jet orifice 6 is stored in the confined cavity 7 space, and the cavity 7 acts on the piston 5 under the pressure of the entering gas and the reaction force of the jet 6 to move the piston 5 as mechanical work, so that the first-stage work flow is determined, namely, work is performed in a pressure mode, and the moving speed of the piston 5 is limited by selecting the specification of the gas pipeline conveying speed and the application of the valve 9; the piston 5 is continuously moved in an overload low-speed mode;

if we agree with the power calculation formula; the reality of TN/9550 is that the power of the first stage piston is a relatively high efficiency. So we define that the use of pressurized gas can be more thermally efficient;

because the pressure gas stored in the cavity 7 needs to be released after performing pressure work, the pressure gas is sent into the second-stage work system 21 through the exhaust hole A10 on the first-stage rotor 3 and the angle nozzle 12 and performs the spraying work at the same time; the function of additional work is generated on the first-stage rotor, the additional work is added to the first-stage work unit and is obtained as the added 1 energy of the first-stage work, and the first-stage work efficiency is increased;

4) and performing work for the second time:

the pressure gas stored in the cavity 7 by first acting is released, the pressure in the cavity 7 is exhausted, the pressure gas is sprayed to a first moving blade 17 and an exhaust air receiving hole 15 in a second-stage acting unit 21 through an exhaust hole A10 and an angular nozzle 12 through a diversion hole 13 on a stator to do work and exhaust, the sprayed pressure gas is sent to the moving blade 17 and an additional moving blade 22 of the second-stage acting unit 21, the moving blade 17 is reversely sprayed to the following moving blade including a second moving blade 18 and a subsequent moving blade 19 and enters a system cavity of the second-stage acting unit 21, the acting application of the pressure gas mass moving energy released by all turbines of the second stage is completed, and the additional moving blade 22 is an auxiliary blade which is arranged outside the moving blade 17 and uses exhaust to do work;

during the process of applying the stored gas through the second stage of work, the residual gas in the cavity 7 needs to be evacuated in the final application stage, the evacuation mode is that the residual gas passes through an exhaust hole 15 arranged on a cover plate of a rear stator 16 from an angular nozzle 12 through an exhaust hole A10, is sent to an evacuation exhaust hole B20 through a pipeline on the stator and is injected onto an additional movable blade 22 on the outer side of the movable blade 17 to be evacuated to assist in reusing the available work, and the conventional atmosphere non-pressure space design is arranged behind the additional movable blade 22 to finish the application of the second stage of releasing the work; the rotor blades 17 of the second stage power generation unit 21 are designed for use in large and high pressure systems.

The application of the pressure gas piston spraying type rotary engine system applied by two-time work is characterized in that: the first-stage acting unit 2 adopts the working principle that a circumferential concentric rotary piston nozzle continuously sprays pressure gas, a switch valve 9 is additionally arranged in a cylinder cavity 7 in which a unidirectional positive circumferential rotary piston operates, a plurality of independent partitioned cavity spaces are created in the cylinder cavity of the piston to form an independent closed cylinder partitioned cavity, the pressure gas fed by the piston 5 for first acting is partitioned and stored, and then gas mass movement acting application of second-time flush penetration and flat release is carried out, so that after the piston 5 is pressed to move and act in the process of conveying the pressure gas, the pressure gas continuously acts for the second time to release the work of a turbine, and the pressure of the pressure gas and the movement energy of the released gas mass are completely utilized to act;

in such a working process, the whole rotor has done twice work, i.e. once pressure and once injection, and the twice work is done under two environmental conditions, i.e. the concept of 1+1 work is realized and completed; then the first-stage rotor 3 can continuously rotate to operate through continuous jet release, and the pressurized gas sent into the cylinder cavity is subjected to all work application through the process; then the gas enters the working application released by the second-stage pressure gas mass turbine, so that the realization of the two-time working can be affirmatively confirmed, and therefore, the whole pressure gas application process can be definitely known to be a scientific, high-efficiency and complete program, and the reality of improving the use efficiency is determined;

the input and output of the pressure gas are all completed in the whole of the concentric rotor of the piston to complete all work doing processes, the pressure gas is fed in through the center of the shaft 1 and is fed into spray holes on the piston head through the center of the first-stage rotor 3 and the internal gas transmission pipeline 4 to do a mode of uninterruptedly spraying and conveying the pressure gas, after the first pressure moving work doing of the piston 5 is completed, the pressure gas fed in by the piston 5 is stored in a separation mode, the stored pressure gas energy is sent out through exhaust spray holes on the piston rotor and is fed into a second-stage system to do work released by the second turbine, and after the work doing of the whole pressure is realized by the rotary piston, the practical application mode of once input and twice work doing of the whole pressure gas through the turbine releasing is realized;

the piston number is determined in a mode that one or more piston heads are arranged on the circumferential rotor rotating body according to the size of the rotor, the piston heads and the nozzle body are equally arranged on the rotating rotor body, the piston heads and the nozzles are in a flat rectangular structure, and the piston bodies and the nozzles move in an infinite distance along with the rotor in a piston cavity of the cylinder; the cavity exhaust holes A10 and the angular nozzle 12 are arranged on the body of the rotor in the same number and interval positions of the pistons and rotate synchronously with the rotor of the pistons, the exhaust holes A10 and the angular nozzle 12 also perform jet work and are used for increasing and fully performing work on the first-stage rotor, and the exhaust holes A10 and the angular nozzle 12 are used for releasing a pressure space behind the pistons into an atmosphere or negative pressure space;

the pressure gas is fed through the piston, and rotates to do work after being subjected to pressure, the pressure gas is required to be released by a turbine after entering a partition space of a cylinder cavity for storage, and the stored pressure gas ejected through a first-stage rotor nozzle is determined to be fed into a second-stage conventional turbine for conventional application as a second-stage work application mode; the requirement of two release spaces is adopted for the evacuation of the stored pressure gas, namely, an exhaust air receiving hole 15 and an exhaust hole B20 are designed as the pressure in the exhaust cavity body 7, and a real pressure-free space is realized behind the piston;

the piston cylinder is internally provided with a switch valve to cause a cylinder cavity section distribution mode, so that an application mode of piston re-motion and energy storage re-output is completed; the valves are arranged on a stator in the piston cylinder, the number of the valves is an application structure mode that the number of piston heads is doubled and 1, so that the working mode of simultaneous impulse is cancelled in an alternative exhaust mode, and the valve section distribution resistance section application on the cylinder or the outer body of the stator is adopted, so that the pressurized movement of the piston and the release and injection of a piston rotor can be separately completed in two independent isolated cavity regions; the switch valve arranged on the stator is opened and closed according to the moving position requirement of the rotary piston;

the whole system controls the input of pressure gas at the front end, and the application of the load of the rotary piston system adopts an overload design, namely the load is greater than the maximum work output capacity of the first stage; the rotating speed is determined by the output magnitude of the load during the rotating work process of the rotating piston; under the conditions of full-load operation and determined working conditions, the total energy input into pressure gas applied later is determined by the pressure section area and the moving speed of the piston;

the whole system application matching platform is based on one or more balanced concentric basic platforms and consists of a first-stage rotary piston structure pressurized acting and a second-stage injection release turbine, and the two acting processes work on the same concentric balance center.