阅读说明：本技术 一种多维度高速飞行能实时高效排放的隔膜密封夹持组件 (Membrane sealing and clamping assembly capable of achieving real-time and efficient discharge in multi-dimensional high-speed flight ) 是由 李玉峰 于 2021-07-02 设计创作，主要内容包括：本申请公开了一种多维度高速飞行能实时高效排放的隔膜密封夹持组件,包括：夹持结构以及隔膜结构,其中：夹持结构包括外夹持环以及内夹持环；隔膜结构包括橡胶隔膜以及密封环；橡胶隔膜与密封环通过外夹持环与内夹持环组装压紧在一起,并且密封环夹持固定在外夹持环与内夹持环之间。本申请的多维度高速飞行能实时高效排放的隔膜密封夹持组件,橡胶隔膜采用超薄、超柔软多棱筋实现多维度无阻滞实时高效排放,铆钉式L型组合环夹持方式实现了零夹气密封隔离,同时通过焊接衬底解决了超薄焊接难题。(The application discloses sealed centre gripping subassembly of diaphragm that high-speed flight of multidimension degree can high-efficiently discharge in real time includes: clamping structure and diaphragm structure, wherein: the clamping structure comprises an outer clamping ring and an inner clamping ring; the diaphragm structure comprises a rubber diaphragm and a sealing ring; the rubber diaphragm and the sealing ring are assembled and pressed together through the outer clamping ring and the inner clamping ring, and the sealing ring is clamped and fixed between the outer clamping ring and the inner clamping ring. The utility model provides a sealed centre gripping subassembly of diaphragm that multidimension degree high speed flight can high-efficiently discharge in real time, the rubber diaphragm adopts ultra-thin, super soft many arris muscle to realize that multidimension degree does not have real-time high-efficiently discharge of retardation, and rivet formula L type combined ring centre gripping mode has realized the sealed isolation of zero clamp gas, has solved the ultra-thin welding difficult problem through the welding substrate simultaneously.)

1. The utility model provides a sealed centre gripping subassembly of diaphragm that high-speed flight of multidimension degree can high-efficiently discharge in real time which characterized in that, includes clamping structure and diaphragm structure, wherein:

the clamping structure comprises an outer clamping ring and an inner clamping ring;

the diaphragm structure comprises a rubber diaphragm and a sealing ring;

the rubber diaphragm and the sealing ring are assembled and pressed together through the outer clamping ring and the inner clamping ring, and the sealing ring is clamped and fixed between the outer clamping ring and the inner clamping ring;

the sealing clamping assembly is connected with the thin-wall shell of the storage box in a welding mode through the outer clamping ring.

2. The multi-dimensional high-speed flight real-time efficient vented membrane seal clamp assembly of claim 1, wherein:

the cross section of the outer clamping ring is of an inverted L shape, the cross section of the inner clamping ring is of a regular L shape, and the outer clamping ring and the inner clamping ring are connected in a matched mode to form a rectangular space;

the sealing ring is clamped and fixed between the outer clamping ring and the inner clamping ring and is positioned in the rectangular space.

3. The multi-dimensional high-speed flying real-time efficient discharging diaphragm sealing clamping assembly according to claim 2, wherein the top end of the outer clamping ring extends vertically upwards to form a connecting end, and the connecting end of the outer clamping ring is fixedly connected with the upper end ring wall of the inner clamping ring through a rivet to form the rectangular space.

4. The multi-dimensional high-speed flight real-time efficient venting diaphragm seal clamp assembly of claim 3, wherein a weld substrate is formed on the outside of the bottom end of the outer clamp ring, and the seal clamp assembly is welded to the upper tank shell and the lower tank shell through the weld substrate.

5. The multi-dimensional high-speed flying diaphragm sealing and clamping assembly capable of achieving real-time and efficient discharging according to claim 4, wherein the sealing and clamping assembly, the upper storage tank shell and the lower storage tank shell are welded through argon arc welding, and the distance between a welding substrate and the sealing ring is not less than 18 mm.

6. The multi-dimensional high-speed flying diaphragm sealing and clamping assembly capable of achieving real-time and efficient discharge according to claim 4, wherein a through hole groove is formed in a circular ring surface, attached to the inner wall of the storage box shell, of the outer clamping ring.

7. The multi-dimensional high-speed flying diaphragm sealing and clamping assembly capable of achieving real-time and efficient discharge according to claim 6, wherein the width of the through hole grooves is 4-6 mm, and 3-5 through hole grooves are uniformly distributed along the annular surface of the outer clamping ring.

8. The multi-dimensional high-speed flight real-time efficient discharge diaphragm sealing and clamping assembly according to claim 6, wherein the rubber diaphragm is made of butyl rubber and has a thickness of 0.8mm to 1.0 mm.

9. The multi-dimensional high-speed flying real-time and efficient discharging diaphragm sealing and clamping assembly according to claim 8, wherein a plurality of multi-edge ribs are uniformly distributed on the outer surface of the rubber diaphragm.

10. The multi-dimensional high-speed flight real-time efficient vented membrane seal clamp assembly of claim 9, wherein:

the multi-edge ribs are semicircular edges;

the multi-edge rib and the rubber diaphragm are integrally formed.

Technical Field

The application relates to the technical field of pressure vessel design, in particular to a diaphragm sealing clamping assembly capable of achieving real-time, non-blocking and efficient discharge through multi-dimensional high-speed flight.

Background

With the continuous progress of scientific and technological technology, high requirements are also provided for the rapid flight of a small aircraft at high altitude, the real-time work in flight and various harsh space environments, and the pressure-drop type diaphragm storage tank needs to be subjected to the harsh space environments such as a ground test gravity environment, a microgravity environment, a high vacuum environment, a return section vacuum atmosphere environment (more than 50 km), a short-term overload environment and the like. The traditional design of the existing diaphragm storage tank has the technical problems of low liquid sealing and discharging efficiency, low instantaneity, gas-liquid interpenetration and poor sealing performance in a high-speed flight state, and the defect that the diaphragm is easy to damage after the non-metal diaphragm and the thin-wall metal shell are integrally formed by welding heat.

Aiming at the technical problems of low discharge efficiency, low instantaneity and poor sealing performance of the traditional diaphragm storage tank in a high-speed flight state in the related art and the defects of damage of welding heat influence on the diaphragm, an effective solution is not provided at present.

Disclosure of Invention

The utility model provides a sealed centre gripping subassembly of diaphragm that high-speed flight of multidimension degree can high-efficiently discharge in real time adopts ultra-thin, super soft many arris muscle through the rubber diaphragm, realizes that multidimension degree does not have real-time high-efficiently discharge of retardation, realizes through rivet formula L type composite ring centre gripping mode that zero presss from both sides the gas seal and keeps apart, solves ultra-thin welding difficult problem through the welding substrate simultaneously, reduces the damage of welding thermal influence to the diaphragm.

In order to achieve the purpose, the application provides a membrane sealing and clamping assembly which is capable of achieving real-time and efficient discharge in multi-dimensional high-speed flight.

According to the sealed centre gripping subassembly of diaphragm that multidimension degree high speed flight can high-efficiently discharge in real time of this application, include: clamping structure and diaphragm structure, wherein: the clamping structure comprises an outer clamping ring and an inner clamping ring; the diaphragm structure comprises a rubber diaphragm and a sealing ring; the rubber diaphragm and the sealing ring are assembled and pressed together through the outer clamping ring and the inner clamping ring, and the sealing ring is clamped and fixed between the outer clamping ring and the inner clamping ring; and the sealing clamping assembly is welded and connected with the thin-wall shell of the storage box through the outer clamping ring.

Furthermore, the cross section of the outer clamping ring is of an inverted L shape, the cross section of the inner clamping ring is of a regular L shape, and the outer clamping ring and the inner clamping ring are connected in a matched mode to form a rectangular space; the sealing ring is clamped and fixed between the outer clamping ring and the inner clamping ring and is positioned in the rectangular space.

Furthermore, the top end of the outer clamping ring extends upwards vertically to form a connecting end, and the connecting end of the outer clamping ring is fixedly connected with the upper end ring wall of the inner clamping ring through a rivet to form a rectangular space.

Furthermore, a welding substrate is formed on the outer side of the bottom end of the outer clamping ring, and the sealing clamping assembly is connected with the upper storage box shell and the lower storage box shell in a welding mode through the welding substrate.

Furthermore, the sealing clamping assembly, the upper storage tank shell and the lower storage tank shell are welded by argon arc welding, and the distance between the welding substrate and the sealing ring is not less than 18 mm.

Furthermore, a through hole groove is formed in the circular ring surface of the outer clamping ring, which is tightly attached to the inner wall of the storage box shell.

Furthermore, the width of the through hole groove is between 4mm and 6mm, and 3 to 5 through hole grooves are uniformly distributed along the annular surface of the outer clamping ring.

Furthermore, the rubber diaphragm is made of butyl rubber, and the thickness of the rubber diaphragm is between 0.8mm and 1.0 mm.

Furthermore, a plurality of multi-edge ribs are uniformly distributed on the outer surface of the rubber diaphragm.

Furthermore, the multi-edge ribs are semi-circular edges; the multi-edge rib and the rubber diaphragm are integrally formed.

In the embodiment of the application, the diaphragm sealing and clamping assembly capable of achieving real-time and efficient discharge in multi-dimensional high-speed flight is provided, the diaphragm sealing and clamping assembly has good gas-liquid sealing performance, has the capabilities of achieving good rigid support with an ultra-thin wall shell and preventing welding heat influence, has the capability of achieving multi-dimensional non-blocking high-discharge-efficiency liquid discharge in a high-speed flight state, is practical for real-time supply of a storage tank in an ultra-low-pressure acceleration environment, and meanwhile improves the discharge reliability and the operation safety of products. The method comprises the following specific steps:

(1) the application has provided a sealed centre gripping subassembly of diaphragm to the high requirement of gas-liquid altogether formula diaphragm storage tank "zero gas inclusion" degasification deionized water supply that falls, has realized the multiaspect contact extrusion formula of grip ring rectangle space and diaphragm structure sealing ring and has closely laminated, has possessed high sealing performance under the high low temperature environment (examined-10 ℃ - +70 ℃) simultaneously, has improved that traditional two-sided sealed mode that compresses tightly receives influences such as thermal expansion shrinkage and appear sealed not good not enough of effect, has reached the high-efficient sealed purpose of gas-liquid.

(2) Aiming at the current situation that the rubber diaphragm is easily damaged by large heat generated by high-temperature argon arc welding of a shell of a storage tank, a welding substrate is arranged on a sealing clamping assembly, the welding substrate is 18-23 mm away from a sealing ring of a diaphragm structure, the influence of welding transfer heat on rubber is effectively reduced, and the transferred temperature is reduced to the acceptable range of rubber materials, so that the welding heat influence is effectively avoided, meanwhile, a rigid support is provided for welding of an ultra-thin-wall shell (0.4mm), the assembling and welding of the diaphragm are possible, and the gas-liquid permeation and the liquid discharge caused by the defects of damaged and adhered rubber diaphragm caused by overlarge welding heat are effectively avoided.

(3) Aiming at the high standard requirements of the storage tank for realizing multi-dimensional real-time non-blocking liquid supply and high-discharge-efficiency liquid discharge under the low-pressure high-speed flying environment, the outer surface of the rubber diaphragm is provided with the multi-edge rib, so that the situation that the rubber diaphragm is attached to the inner wall of the storage tank in a large area in the operation process of the storage tank to form a sealing belt to prevent the supply of liquid is avoided, and the liquid discharge efficiency reaches more than 99 percent.

In conclusion, the diaphragm sealing clamping assembly capable of achieving real-time and efficient discharging in multidimensional high-speed flight has the advantages that the rubber diaphragm is ultrathin, ultra-soft and multi-edge ribs are adopted to achieve multidimensional non-stagnation real-time and efficient discharging, zero-clamping gas sealing isolation is achieved in a rivet type L-shaped combined ring clamping mode, and meanwhile the ultrathin welding problem is solved through welding a substrate.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this application, serve to provide a further understanding of the application and to enable other features, objects, and advantages of the application to be more apparent. The drawings and their description illustrate the embodiments of the invention and do not limit it. In the drawings:

FIG. 1 is a schematic diagram of an overall structure of a multi-dimensional high-speed flying real-time efficient venting diaphragm seal clamping assembly according to an embodiment of the application;

FIG. 2 is a schematic cross-sectional view of a multi-dimensional high-speed flying high-efficiency venting diaphragm seal clamping assembly according to an embodiment of the present disclosure;

FIG. 3 is an enlarged, fragmentary, schematic structural view of a diaphragm structure provided in accordance with an embodiment of the present application;

FIG. 4 is a schematic view of a partial enlarged structure of a clamping structure provided according to an embodiment of the present application;

in the figure: 1-outer clamping ring, 2-inner clamping ring, 3-rivet, 4-welding substrate, 5-rubber diaphragm, 6-sealing ring, 7-multi-edge rib and 8-through hole groove.

Detailed Description

In order to make the technical solutions better understood by those skilled in the art, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only partial embodiments of the present application, but not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.

It should be noted that the terms "first," "second," and the like in the description and claims of this application and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It should be understood that the data so used may be interchanged under appropriate circumstances such that embodiments of the application described herein may be used. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.

In this application, the terms "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings. These terms are used primarily to better describe the present application and its embodiments, and are not used to limit the indicated devices, elements or components to a particular orientation or to be constructed and operated in a particular orientation.

Moreover, some of the above terms may be used to indicate other meanings besides the orientation or positional relationship, for example, the term "on" may also be used to indicate some kind of attachment or connection relationship in some cases. The specific meaning of these terms in this application will be understood by those of ordinary skill in the art as appropriate.

In addition, the term "plurality" shall mean two as well as more than two.

It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.

The diaphragm sealing and clamping assembly mainly realizes the separation of gas and liquid in the falling pressure type diaphragm storage tank and meets the requirement of the supply of 'zero gas inclusion' degassed deionized water in a liquid cavity. Meanwhile, the liquid in the storage tank is ensured not to be influenced by mechanical environments such as acceleration and the like in the high-speed flying process, and the real-time high-discharge-efficiency discharge can be met. The structure design of the device needs to solve the problem of high-quality sealing in the storage tank and real-time high-efficiency supply in a high-speed state, and overcomes the defects of low discharge efficiency, poor sealing property and large welding heat influence in the traditional design.

The difficulty lies in that: firstly, the system has high requirements on discharged liquid, the liquid cavity is required to be degassed deionized water with zero gas inclusion, certain risks and technical problems exist in the sealing performance of the isolation interface, the higher requirements are provided for the sealing performance of the diaphragm clamping assembly serving as the gas-liquid isolation interface, and the gas in the gas cavity is not allowed to permeate into the liquid cavity. And secondly, the shell of the falling-pressure type diaphragm storage tank is an ultra-thin-wall shell (the wall thickness is 0.4mm), the air cavity shell, the diaphragm clamping assembly and the liquid cavity shell are formed by welding, the gas-liquid cavity isolation interface belongs to contact between a non-metal material and a metal material, high-temperature heat can be generated in the welding process, rubber at the sealing position is easily heated and damaged to cause adhesion through the heat conduction effect of the metal clamping structure, the technical problem that high temperature is easily damaged exists, and high-efficiency sealing cannot be realized. The falling-pressure type diaphragm storage tank needs to be subjected to various severe environment tests in a high-speed flying environment, and meanwhile, the deionized water is supplied in a multidimensional state in real time, so that the technical problems of flow limitation, stagnation, flow blocking and the like easily caused by the influence of a dynamic environment in multidimensional high-speed and real-time supply exist, on one hand, the flow rate is not allowed to be influenced in the supply process, and on the other hand, the high-discharge-efficiency discharge of the storage tank is ensured.

The three technical problems of adhesion of rubber sealing contact points and high liquid cavity discharge efficiency under multi-dimensional high-speed flight caused by welding high-temperature thermal stress are solved, the novel design of the diaphragm sealing clamping assembly capable of realizing real-time high-efficiency discharge of the storage box in an ultra-low pressure acceleration environment is realized by adopting an ultra-thin ultra-soft multi-edge diaphragm design structure (the discharge efficiency reaches more than 99 percent), stable overturning of the rubber diaphragm 5 in the acceleration operation environment is realized, mass center deviation in liquid discharge is avoided, and convenience is provided for accurate control of flight attitude of a small aircraft. The adoption of the diaphragm material butyl rubber with better service life and performance reduces gas permeation, realizes zero gas inclusion sealing isolation and ensures the supply of degassed deionized water. The novel rivet type metal clamping ring combined structure is introduced to lock the bottom for welding, so that the influence of high-temperature heat transfer on the diaphragm structure in the welding process is avoided. The structure related to the application has successfully passed flight verification on a certain type of lander.

The sealed centre gripping subassembly of diaphragm that multi-dimension high-speed flight can high-efficiently discharge in real time of this application embodiment includes: clamping structure and diaphragm structure, wherein: the clamping structure comprises an outer clamping ring 1 and an inner clamping ring 2; the diaphragm structure comprises a rubber diaphragm 5 and a sealing ring 6; the rubber diaphragm 5 and the sealing ring 6 are assembled and pressed together through the outer clamping ring 1 and the inner clamping ring 2, and the sealing ring 6 is clamped and fixed between the outer clamping ring 1 and the inner clamping ring 2; the sealing clamping assembly is connected with the thin-wall shell of the storage box in a welding mode through the outer clamping ring 1.

Specifically, the outer clamping ring 1 is arranged on the circumference of the inner wall of the closely-attached ultrathin-wall shell, is matched with the inner clamping ring 2 for use, and is used for clamping and fixing the diaphragm structure. The rubber diaphragm 5 is made of butyl rubber, the selection principle is that the rubber diaphragm has good I-grade compatibility with a storage medium, the butyl rubber has good compatibility with deionized water, the thickness of the rubber diaphragm 5 is generally 0.8-1.0 mm, the main purpose of the rubber diaphragm is to isolate gas and liquid in a storage tank, and the gas pushes the liquid to meet the supply requirement in a microgravity or severe acceleration environment when the diaphragm is overturned. The assembly of outer clamping ring 1 and inner clamping ring 2 can adopt the connected mode such as rivet, and this application does not do specifically and restricts, all belongs to this application scope of protection. The outer clamping ring 1 is welded with the thin-wall shell of the storage tank (comprising the upper shell of the storage tank and the lower shell of the storage tank), so that the 'integral forming' of the non-metal component and the metal component is skillfully realized, the sealing effect of 'zero penetration' is realized, and meanwhile, the membrane overturning is realized through the participation of the non-metal rubber membrane 5.

Furthermore, the cross section of the outer clamping ring 1 is of an inverted L shape, the cross section of the inner clamping ring 2 is of a regular L shape, and the outer clamping ring 1 and the inner clamping ring 2 are connected in a matched mode to form a rectangular space; the sealing ring 6 is clamped and fixed between the outer clamping ring 1 and the inner clamping ring 2 and is positioned in the rectangular space.

Specifically, outer clamping ring 1 uses with the cooperation of interior clamping ring 2, and the combination forms the rectangle space for place diaphragm structure sealing ring 6, and rectangle space size of a dimension is decided by diaphragm structure sealing ring 6's size, material compression coefficient, sealing performance, obtains through the sealing member standard, and this application does not do not specifically limit. More specifically, the sealing ring 6 adopts circular structure and rubber diaphragm 5 to form a whole through the mould, and the rectangle space that forms through the grip ring is fixed and extrusion seal, and 6 sizes of sealing ring should be supporting with grip ring rectangle region, satisfy sealed manual requirement, realize that the high efficiency of gas, liquid is sealed, and 6 radiuses of sealing ring generally take the value 3 ~ 4 mm.

Furthermore, the top end of the outer clamping ring 1 extends vertically upwards to form a connecting end, and the connecting end of the outer clamping ring 1 is connected and fixed with the upper end ring wall of the inner clamping ring 2 through a rivet 3 to form a rectangular space. The number of the rivets 3 is determined by the diameter of the clamping ring, and 24 rivet holes are generally arranged on a uniform circle with the diameter of 180 mm-260 mm. Its main purpose is to secure the retaining ring and to increase the rigidity of the ultra thin walled column section housing of the tank. The rivet 3 is used for connecting the inner clamping ring 2 and the outer clamping ring 1, and meanwhile, one side of the rivet 3, which can be contacted with the diaphragm structure, needs to be subjected to rounding and deburring treatment to prevent the diaphragm structure from being scratched.

Further, a welding substrate 4 is formed on the outer side of the bottom end of the outer clamping ring 1, and the sealing clamping assembly is connected with the upper storage box shell and the lower storage box shell in a welding mode through the welding substrate 4. The sealing clamping assembly, the upper storage tank shell and the lower storage tank shell are welded by argon arc welding, and the distance from the top of the welding substrate 4 to the bottom (or the bottom of the rectangular space) of the sealing ring 6 is not less than 18mm, generally not less than 18 mm-23 mm.

Specifically, the welding substrate 4 is assembled with the storage tank ultrathin-wall shell into a whole, and is connected with the storage tank upper shell, the sealing clamping assembly and the storage tank lower shell through welding, so that the assembly welding of a final product is completed. The welding substrate 4 and the part of the clamping ring for clamping the sealing ring 6 are kept at a certain distance, so that the damage influence of welding heat on the sealing ring 6 can be effectively avoided, and the sealing ring 6 and the clamping ring are prevented from being adhered or damaged due to the influence of the welding heat on the sealing ring 6. The main purpose is to connect each component, ensure the rigidity and roundness of the ultra-thin wall shell during welding, and avoid the splashing redundant material generated in the welding process as the lock bottom.

Furthermore, a through hole groove 8 is formed in the circular ring surface of the outer clamping ring 1, which is tightly attached to the inner wall of the storage box shell.

Preferably, the width of the through hole grooves 8 is 4-6 mm, and 3-5 through hole grooves are uniformly distributed along the annular surface of the outer clamping ring 1.

Specifically, four through hole grooves 8 with the width of 5mm are formed in the annular surface, close to the inner wall of the storage box shell, of the outer clamping ring 1, so that air is prevented from being trapped in the cavity outside the outer clamping ring 1, and welding is not facilitated.

Furthermore, a plurality of multi-edge ribs 7 are uniformly distributed on the outer surface of the rubber diaphragm 5.

Specifically, many arriss muscle 7 are arranged at the many arriss of rubber diaphragm 5 surface through the mould, many arriss muscle 7 cross section is semicircular structure and with rubber diaphragm 5 integrated into one piece, many arriss muscle structure of watermelon lamella is formed to a week, many arriss muscle 7 radius is about 0.9 ~ 1.2mm, 12 ~ 16 general equipartitions according to actual conditions, prevent that rubber diaphragm 5 from hugging closely the inner wall of storage tank and forming liquid seal and leading to most liquid can't discharge and reduced emission efficiency, avoided receiving environmental impact such as acceleration and microgravity and retardation liquid's smooth and easy discharge simultaneously in high-speed flight, therefore two arris clearance can suitably set up lessly less, avoid large tracts of land contact casing inner wall, in the position that half membrane many arriss intersect, can set up the arriss that length differs, both can improve emission efficiency, the intensive equipartition of arris has been reduced again. The combination of the radius and the number of the multi-edge ribs jointly determines that liquid is not sealed, and high discharge efficiency is guaranteed.

The utility model provides a sealed centre gripping subassembly of diaphragm that multidimension degree high-speed flight ability was discharged in real time high efficiency has good gas-liquid sealing performance, have with the super thin wall casing between good rigid support with prevent welding heat affected ability, have the ability that can realize the undamped high discharge efficiency of multidimension degree and discharge liquid under the high-speed flight state, it is very practical to supply in real time under the super low pressure acceleration environment to the storage tank, has improved product discharge reliability, operational safety nature simultaneously.

The application discloses a specific embodiment of the sealed centre gripping subassembly of diaphragm that multidimension degree high-speed flight can high-efficiently discharge in real time:

a rubber diaphragm sealing and clamping assembly on a lander of a certain model is characterized in that a sealing and clamping ring structure with the maximum outer diameter of 260mm is adopted, the thickness of the clamping ring is 1-1.5 mm, 24 rivets with the diameter of 3.5mm are connected and fixed, a rectangular sealing area with the diameter of 7.3mm multiplied by 4.4mm is formed, the clamping diameter is 6mm of a sealing ring to realize the connection of a storage box shell and the diaphragm structure, a welding seam substrate is arranged at the position which is minimum about 18mm away from the bottom of a rectangular space (18mm can avoid the heat influence of welding on the sealing ring), the thickness of the substrate is 1.5mm, the width of the substrate is 6.5mm, 16 semicircular edges with the radius of 1mm are uniformly distributed on the outer curved surface of the rubber diaphragm with the thickness of 0.9mm, 4 semicircular edges are long edges, 12 semicircular edges are short edges, and the drainage of liquid is realized.

The above description is only a preferred embodiment of the present application and is not intended to limit the present application, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application.