阅读说明：本技术 一种用于探空的大气参数测量装置 (Atmospheric parameter measuring device for sounding ) 是由 郑德智 张亚军 曹先彬 王帅 张军 于 2019-08-30 设计创作，主要内容包括：本发明公开了一种用于探空的大气参数测量装置,包括锥顶、平衡杆、上螺旋桨、下螺旋桨、传动模块、增速模块、直流发电机、载物壳、惯性发电模块、无线携能通信模块、传感器载台、底座、气囊、低功耗传感器。通过本发明的技术方案,能够利用风能、微波、惯性、太阳能四种方式产生电能,保障所搭载低功耗传感器的供能,使测量装置昼夜均能产生电能,保证所携带低功耗传感器的工作状态,以便测量当前位置大气的温度、湿度、风速、压强、云水粒子形态参数；通过两个螺旋桨旋转提供的升力使测量装置浮空飞行,体型小巧,重量轻,方便搭载低功耗传感器进行大规模的探空大气参数测量实验,同时可以实现反向控制测量装置的浮空飞行状态。(The invention discloses an atmospheric parameter measuring device for sounding, which comprises a conical top, a balance rod, an upper propeller, a lower propeller, a transmission module, a speed-increasing module, a direct-current generator, a carrying shell, an inertial power generation module, a wireless energy-carrying communication module, a sensor carrying platform, a base, an air bag and a low-power-consumption sensor. According to the technical scheme, the electric energy can be generated by utilizing four modes of wind energy, microwave, inertia and solar energy, the energy supply of the carried low-power-consumption sensor is guaranteed, the measuring device can generate the electric energy day and night, and the working state of the carried low-power-consumption sensor is guaranteed, so that the temperature, the humidity, the wind speed, the pressure and the cloud water particle form parameters of the atmosphere at the current position can be measured conveniently; the lift that provides through two screw rotations makes measuring device float and fly, and the size is small and exquisite, and light in weight conveniently carries on low-power consumption sensor and carries out large-scale exploration atmospheric parameter and measure the experiment, can realize reverse control measuring device's float flight state simultaneously.)

1. An atmospheric parameter measuring device for exploration is characterized by comprising a conical top (1), a balance rod (2), an upper propeller (3), a lower propeller (4), a transmission module (5), a speed increasing module (6), a direct current generator (7), a carrying shell (8), an inertia generating module (9), a wireless energy-carrying communication module (10), a sensor carrying platform (11), a base (12), an air bag (13) and a low-power consumption sensor, wherein,

the cone top (1) is connected with the balance rod (2) through threads, the bottom of the balance rod (2) is sequentially connected with the upper propeller (3) and the lower propeller (4), the upper propeller (3) and the lower propeller (4) are both of bamboo dragonfly-simulated structures, and the rotating directions of the upper propeller and the lower propeller are opposite;

the transmission module (5) comprises an upper transmission rod (51), a lower transmission rod (52), a ball bearing (53) and a conical gear (54), wherein the upper transmission rod (51) is sleeved outside the lower transmission rod (52), a gear disc is arranged at the bottom of the upper transmission rod (51), the upper propeller (3) is connected with the lower transmission rod (52), the lower propeller (4) is connected with the upper transmission rod (51), the rotation directions of the upper transmission rod (51) and the lower transmission rod (52) are opposite, the ball bearing (53) is sleeved at the bottom of the lower transmission rod (52), and the conical gear (54) is sleeved on the ball bearing (53);

the speed increasing module (6) comprises a gear ring (61) and a star gear (62) meshed with the gear ring (61), the conical gear (54) can be meshed with a gear disc at the bottom of the upper transmission rod (51) and the gear ring (61) to combine and transmit the rotating force of the upper transmission rod (51) and the rotating force of the lower transmission rod (52) to the gear ring (61), and the gear ring (61) drives the star gear (62) to rotate to increase the rotating speed;

the star-shaped gear (62) is fixedly connected with a rotor of the direct current generator (7) to drive the rotor of the direct current generator (7) to rotate and cut magnetic induction lines to generate electric energy; the bottom of the direct current generator (7) is fixed with the top of the carrying shell (8) through screws;

the carrying shell (8) is a cylindrical hollow shell, and four axial grooves are uniformly formed in the outer wall of the carrying shell (8);

the outer sides of the inertia power generation module (9), the wireless energy-carrying communication module (10) and the sensor carrier (11) are respectively provided with a threaded hole corresponding to an axial groove of the carrying shell (8), and the inertia power generation module (9), the wireless energy-carrying communication module (10) and the sensor carrier (11) are movably arranged in the carrying shell through screws and the axial groove of the carrying shell (8) and are arranged in a layered manner;

the inertial power generation module (9) comprises a spherical shell (91) of an external winding coil, a magnetic solid ball (92) capable of freely moving in the spherical shell and a chassis (93), wherein when the measuring device swings, the magnetic solid ball (92) rotates, and a magnetic induction line cutting the spherical shell (91) of the external winding coil generates induced electromotive force;

the wireless energy-carrying communication module (10) is used for collecting energy of wireless electromagnetic waves in a space and can be in wireless communication with a terminal;

the sensor carrying platform (11) is used for carrying the low-power consumption sensor; the low-power consumption sensor comprises a temperature sensor, a humidity sensor, a wind speed sensor, an atmospheric pressure sensor and a cloud water particle form sensor;

the base (12) is fixedly connected with the bottom of the object carrying shell (8) through screws.

2. An atmospheric parameter measurement device for sounding according to claim 1, characterized in that the output end of the DC generator (7) carries a load with adjustable power, and the rotation speed of the DC generator (7) is controlled by adjusting the power of the load.

3. An atmospheric parameter measurement device for sounding according to claim 1 or 2, characterized in that the base (12) is provided with an annular air bag (13).

4. An atmospheric parameter measurement device for sounding according to claim 1 or 2, characterized in that the surfaces of the cone top (1), the upper propeller (3), the lower propeller (4), the transmission module (5), the speed increasing module (6), the carrier shell (8) and the base (12) are coated with a layer of solar energy in a solar energy collecting material collecting environment to power the low power consumption sensor.

5. The atmospheric parameter measurement device for sounding out of claim 1 or 2, characterized in that the frequency band of the wireless electromagnetic wave for collecting energy by the wireless energy-carrying communication module (10) comprises 6G frequency band, 0.3GHz-3THz microwave frequency band.

6. An atmospheric parameter measurement device for use in exploration vehicles according to any of claims 1 to 5, characterized in that said measurement device is capable of operating in an aeronautical or near space or in an aeronautical space.

Technical Field

The invention belongs to the technical field of atmospheric parameter measurement, and particularly relates to an atmospheric parameter measuring device with a self-generating function and used for sounding.

Background

Generally defined, an area 20 kilometers below the ground is called an aviation space; the space is called in the area more than 100 kilometers away from the ground; and the area 20-100 kilometers away from the ground is used as the adjacent space, is a transition area of the space and the aviation space, is a blank area which is not developed by human beings in a large scale, and has very important strategic significance and utilization value. This area is above the flight airspace of commercial aircraft, but below the orbiting satellites. Although some aircraft and satellites, airships are technically able to reach the near space, they must consume a large amount of fuel for a long period of time.

With the rapid development of modern high and new technologies, the information countermeasure space is not limited to land, sea and low altitude any more, and the adjacent space also becomes a new battlefield of modern war, and is an important link of the national security system. The adjacent space is used as an effective link for connecting an air-space battlefield, plays a crucial role in the air-space integrated combined battle in the future and is highly valued by more and more countries. Measurement of various atmospheric parameters in an adjacent space depends on deployment of sensors, and how to deploy a large number of sensor nodes in the adjacent space is a problem to be solved urgently at present.

In the existing atmospheric parameter measuring device for sounding, the energy supply usually adopts a method of carrying a lithium battery and a solar cell panel, but the weight of the aerostat is increased, and meanwhile, the aerostat cannot work at night due to the fact that solar energy is needed for charging. In addition, in the atmospheric parameter measuring device who is used for exploring in the current, its working space and position have certain limitation, inconvenient in time adjustment as required. Furthermore, in the existing atmospheric parameter measuring device for sounding, the cost of the device is generally high, and if the atmospheric parameter is measured in a large scale, the cost of the measurement is also higher.

Disclosure of Invention

In order to solve the defects of the prior art, the invention provides the atmospheric parameter measuring device for sounding, the atmospheric parameter measuring device is floated and flies by virtue of the lifting force provided by the rotation of the two propellers, the atmospheric parameter measuring device is small and exquisite in size and light in weight, and a low-power-consumption sensor is conveniently carried to carry out large-scale sounding atmospheric parameter measurement experiments including an aerospace space, a near space and an aerospace space.

The specific technical scheme of the invention is as follows: an atmospheric parameter measuring device for sounding is characterized by comprising a conical top, a balance rod, an upper propeller, a lower propeller, a transmission module, a speed-increasing module, a direct-current generator, a carrying shell, an inertial power generation module, a wireless energy-carrying communication module, a sensor carrying platform, a base, an air bag and a low-power-consumption sensor, wherein,

the cone top is connected with the balance rod through threads, the bottom of the balance rod is sequentially connected with the upper propeller and the lower propeller, the upper propeller and the lower propeller are of bamboo dragonfly-simulated structures, and the rotating directions of the upper propeller and the lower propeller are opposite;

the transmission module comprises an upper transmission rod, a lower transmission rod, a ball bearing and a bevel gear, the upper transmission rod is sleeved outside the lower transmission rod, the bottom of the upper transmission rod is provided with a gear disc, the upper propeller is connected with the lower transmission rod, the lower propeller is connected with the upper transmission rod, the rotation directions of the upper transmission rod and the lower transmission rod are opposite, the ball bearing is sleeved at the bottom of the lower transmission rod, and the bevel gear is sleeved on the ball bearing;

the speed increasing module comprises a gear ring and a star gear meshed with the gear ring, the conical gear can be meshed with the gear disc at the bottom of the upper transmission rod and the gear ring to combine and transmit the rotating force of the upper transmission rod and the lower transmission rod to the gear ring, and the gear ring drives the star gear to rotate to increase the rotating speed;

the star-shaped gear is fixedly connected with a rotor of the direct current generator to drive the rotor of the direct current generator to rotate and cut the magnetic induction line to generate electric energy; the bottom of the direct current generator is fixed with the top of the carrying shell through a screw;

the carrying shell is a cylindrical hollow shell, and four axial grooves are uniformly formed in the outer wall of the carrying shell;

the outer sides of the inertia power generation module, the wireless energy-carrying communication module and the sensor carrying platform are respectively provided with a threaded hole corresponding to the axial groove of the carrying shell, and the inertia power generation module, the wireless energy-carrying communication module and the sensor carrying platform are movably arranged in the carrying shell through screws and the axial groove of the carrying shell and are arranged in a layered manner;

the inertial power generation module comprises a spherical shell of an external winding coil, a magnetic solid ball capable of freely moving in the spherical shell and a chassis, wherein when the measuring device flutters in the air in front, back, left and right directions, the magnetic solid ball swings to cut a magnetic induction line of the spherical shell of the external winding coil to generate induced electromotive force;

the wireless energy-carrying communication module is used for collecting energy of wireless electromagnetic waves in a space and can be in wireless communication with a terminal;

the sensor carrying platform is used for carrying the low-power consumption sensor; the low-power consumption sensor comprises a temperature sensor, a humidity sensor, a wind speed sensor, an atmospheric pressure sensor and a cloud water particle form sensor;

the base is fixedly connected with the bottom of the object carrying shell through a screw.

Furthermore, the output end of the direct current generator carries a load with adjustable power, and the rotating speed of the direct current generator is controlled by adjusting the power of the load.

Furthermore, an annular air bag is arranged on the base.

Furthermore, the cone top, the upper propeller, the lower propeller, the transmission module, the speed increasing module, the object carrying shell and the surface of the base are all coated with a layer of solar energy in a solar energy collecting material collecting environment to supply power for the low-power consumption sensor.

Furthermore, the frequency band of the wireless electromagnetic wave for collecting energy by the wireless energy-carrying communication module comprises a 6G frequency band and a frequency band of 0.3GHz-3THz microwave.

Further, the measuring device can be operated in an aviation space or an adjacent space or an aviation space.

The invention has the beneficial effects that:

1. the power is generated by four modes of wind energy, microwave, inertia and solar energy, and electric energy is generated by day and night, so that the energy supply of the low-power consumption sensor is guaranteed;

2. the atmospheric parameter measuring device for sounding is small in size and light in weight, and is convenient to carry a low-power consumption sensor to carry out large-scale sounding atmospheric parameter measurement experiments;

3. the mounting positions of the inertia generating device, the wireless energy-carrying communication module and the sensor carrier can be adjusted through an axial groove on the outer wall of the carrying shell, so that the gravity center of the whole measuring device is changed, and the floating flight of the measuring device is more stable;

4. in addition to power generation, reverse control may also be implemented. The rotating speed of the direct current generator is controlled through the load with adjustable power, and then the floating flight state of the measuring device is adjusted;

5. the measuring device of the invention can be operated in an aviation space or an adjacent space or an aviation space.

Drawings

In order to illustrate embodiments of the present invention or technical solutions in the prior art more clearly, the drawings which are needed in the embodiments will be briefly described below, so that the features and advantages of the present invention can be understood more clearly by referring to the drawings, which are schematic and should not be construed as limiting the present invention in any way, and for a person skilled in the art, other drawings can be obtained on the basis of these drawings without any inventive effort. Wherein:

FIG. 1 is a general block diagram of an atmospheric parameter measuring device of the present invention;

FIG. 2 is an exploded view of FIG. 1;

FIG. 3 is a schematic view of the ball bearing connection of the atmospheric parameter measurement device of the present invention;

FIG. 4 is a structural view of a speed increasing device of the atmospheric parameter measuring device of the present invention;

FIG. 5 is a partial enlarged view of the atmospheric parameter measurement device of the present invention;

fig. 6 is a sectional view of an inertial power generation module of the atmospheric parameter measurement device of the present invention.

The reference numbers illustrate:

1-conical top; 2-a balance bar; 3-upper propeller; 4-lower propeller; 5-a transmission module; 51-upper drive rod; 52-lower drive link; 53-ball bearings; 54-a conical gear; 6-a speed increasing module; 61-gear ring; 62-a star gear; 7-a direct current generator; 8-carrying shell; 9-an inertial power generation module; 91-spherical shell; 92-solid sphere; 93-a chassis; 10-a wireless energy-carrying communication module; 11-a sensor stage; 12-a base; 13-air bag.

Detailed Description

In order that the above objects, features and advantages of the present invention can be more clearly understood, a more particular description of the invention will be rendered by reference to the appended drawings. It should be noted that the embodiments of the present invention and features of the embodiments may be combined with each other without conflict.

In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the scope of the present invention is not limited by the specific embodiments disclosed below.

The general structure of the invention is as shown in figure 1, the bamboo dragonfly-like structure is an atmospheric parameter measuring device for sounding with self-generating function, and the atmospheric parameter measuring device can be used for carrying various low-power consumption sensors and supplying power to the low-power consumption sensors, so that the low-power consumption sensors can work in aerospace space, near space and aviation space.

Specifically, as shown in fig. 2, the atmospheric parameter measuring device for sounding is characterized by comprising a cone top 1, a balance rod 2, an upper propeller 3, a lower propeller 4, a transmission module 5, a speed increasing module 6, a direct current generator 7, a carrying shell 8, an inertia generating module 9, a wireless energy carrying communication module 10, a sensor carrying platform 11, a base 12, an air bag 13 and a low-power consumption sensor (not shown), wherein the cone top 1 is connected with the balance rod 2 through threads, the bottom of the balance rod 2 is sequentially connected with the upper propeller 3 and the lower propeller 4, the upper propeller 3 and the lower propeller 4 are both of a bamboo dragonfly-like structure, and the rotation directions of the upper propeller 3 and the lower propeller 4 are opposite; when the measuring device flies in the air in a floating way, the balance rod 2 balances the whole measuring device through self rotation so as to ensure that the measuring device is in a normal floating flying state; under the action of wind power and gravity, the upper propeller 3 and the lower propeller 4 rotate to provide lift force for the measuring device, the two propellers rotate in opposite directions, and the self-rotation of the measuring device can be counteracted while the lift force is provided.

As shown in fig. 3-4, the transmission module 5 includes an upper transmission rod 51, a lower transmission rod 52, a ball bearing 53, and a bevel gear 54, the upper transmission rod 51 is sleeved outside the lower transmission rod 52, the bottom of the upper transmission rod 51 is a gear disc, the upper propeller 3 is connected with the lower transmission rod 52, the lower propeller 4 is connected with the upper transmission rod 51, the upper propeller 3 transmits a rotation force through the lower transmission rod 52, the lower propeller 4 transmits a rotation force through the upper transmission rod 51, the rotation directions of the upper transmission rod 51 and the lower transmission rod 52 are opposite, the ball bearing 53 is sleeved at the bottom of the lower transmission rod 52, and the bevel gear 54 is sleeved on the ball bearing 53, so as to reduce the friction force of the bevel gear;

the speed increasing module 6 comprises a gear ring 61 and a star gear 62 meshed with the gear ring 61, the conical gear 54 can be meshed with a gear disc at the bottom of the upper transmission rod 51 and the gear ring 61 to combine and transmit the rotating force of the upper transmission rod 51 and the lower transmission rod 52 to the gear ring 61, and the gear ring 61 drives the star gear 62 to rotate to increase the rotating speed;

the star gear 62 is fixedly connected with the rotor of the direct current generator 7 to drive the rotor of the direct current generator 7 to rotate, and cuts the magnetic induction lines to generate electric energy; the bottom of the direct current generator 7 is fixed with the top of the carrying shell 8 through screws;

as shown in fig. 5, the carrying shell 8 is a cylindrical hollow shell, and four axial grooves are uniformly formed in the outer wall of the carrying shell 8; the outer sides of the inertia power generation module 9, the wireless energy-carrying communication module 10 and the sensor carrier 11 are respectively provided with a threaded hole corresponding to an axial groove of the carrying shell 8, the inertia power generation module 9, the wireless energy-carrying communication module 10 and the sensor carrier 11 are movably mounted inside the carrying shell through screws and the axial groove of the carrying shell 8 and are arranged in a layered mode, the mounting positions of the inertia power generation module 9, the wireless energy-carrying communication module 10 and the sensor carrier 11 can be flexibly adjusted, the gravity center of the measuring device is changed, and floating flight of the measuring device is stable.

As shown in fig. 6, the inertia generating module 9 includes a spherical shell 91 of an external coil, a magnetic solid ball 92 capable of freely moving in the spherical shell, and a chassis 93, when the measuring device floats in the air and swings up and down and left and right, the magnetic solid ball 92 rotates to cut the magnetic induction line of the spherical shell 91 of the external coil to generate induced electromotive force, and the inertia generating module 9 converts the swing of the measuring device into electric energy.

The wireless energy-carrying communication module 10 is used for collecting energy of wireless electromagnetic waves in a space and simultaneously can carry out wireless communication with a terminal;

the sensor stage 11 is used for mounting a low-power consumption sensor (not shown); low power sensors (not shown) including temperature sensors, humidity sensors, wind speed sensors, barometric pressure sensors, and cloud water particle morphology sensors; the base 12 is fixedly connected with the bottom of the carrying shell 8 through screws.

In some embodiments, the output end of the dc generator 7 carries a load with adjustable power, and the reverse control can be realized by adjusting the power of the load to control the rotating speed of the dc generator 7, and further adjust the floating flight state of the measuring device.

In some embodiments, a ring-shaped air bag 13 is arranged on the base 12, and the air bag 13 can release colored smoke to facilitate the recovery of the measuring device, and meanwhile, provides buoyancy when the measuring device falls into water to ensure that the measuring device does not sink into water.

In some embodiments, the surfaces of the cone top 1, the upper propeller 3, the lower propeller 4, the transmission module 5, the speed increasing module 6, the carrier housing 8 and the base 12 are coated with a layer of solar energy in a solar energy collecting material collecting environment to power a low power consumption sensor (not shown).

In some embodiments, the frequency band of the wireless electromagnetic wave collected by the wireless energy-carrying communication module 10 includes a 6G frequency band and a frequency band of 0.3GHz-3THz microwave.

The measuring device can be operated in an aviation space or an adjacent space or an aviation space.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, a first feature being "on," "above" or "over" a second feature includes the first feature being directly on or obliquely above the second feature, or simply indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

In the present invention, the terms "first", "second", "third", and "fourth" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. The term "plurality" means two or more unless expressly limited otherwise.

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