CN107651159B - Aerostatics zero pressure differential circular exhaust apparatus - Google Patents
Aerostatics zero pressure differential circular exhaust apparatus Download PDFInfo
- Publication number
- CN107651159B CN107651159B CN201710738251.3A CN201710738251A CN107651159B CN 107651159 B CN107651159 B CN 107651159B CN 201710738251 A CN201710738251 A CN 201710738251A CN 107651159 B CN107651159 B CN 107651159B
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- guide rod
- shell
- exhaust
- sealing cover
- reinforcing rib
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
Abstract
The invention relates to a zero-pressure-difference circular exhaust device of an aerostat, which comprises a shell and is characterized in that: the bottom of the shell is provided with an exhaust sealing cover; the shell is internally provided with a power transmission device for driving the exhaust sealing cover to move up and down; the shell and the exhaust sealing cover are both circular; a trapezoidal male die is arranged below the shell along the circumferential direction, a trapezoidal female die is correspondingly arranged above the exhaust sealing cover along the circumferential direction, and the male die and the female die are matched to form sealing. The invention has simple and reasonable structure, light weight, high strength, good sealing performance and easy assembly.
Description
Technical Field
The invention relates to a zero differential pressure exhaust device of an aerostat.
Background
The high-altitude aerostat is developed and can be applied to a near space, wherein the near space is 20-100 kilometers away from the surface of the earth, the air in the space is thinner and thinner from low to high, so that most airplanes have difficulty in flying in the space and even cannot fly, the universal gravitation in the space is too large relative to satellites, and the cost is huge if the high-altitude aerostat operates in the space for a long time in a certain altitude orbit. The aerostat is much lower in cost and can be suspended on the stratosphere for a long time, the high-altitude aerostat can replace a synchronous satellite for communication, television broadcasting, monitoring, scientific experiments and the like in civilian use, the high-altitude aerostat can be used as a general platform with functions of military communication, remote investigation, information, navigation, early warning and the like in military use, the aerostat has extremely high economic value and strategic value in military use and civil use, and the service life of the aerostat is also widely concerned by various circles. When the aerostat is lifted from the ground, the capsule body of the aerostat needs to be filled with enough gas to achieve the effect that the buoyancy of the capsule body is larger than the buoyancy of the air, then the capsule body can be lifted, the air is thinner and thinner along with the fact that the capsule body flies higher and higher, the air pressure is smaller and smaller, the gas volume pressure in the aerostat can be increased, and in order to avoid the explosion of the capsule body of the aerostat caused by the overlarge internal and external pressure difference, an exhaust device is needed. The existing aerostat exhaust device has the defects of complex structure, heavier weight or lighter weight but poorer strength.
Disclosure of Invention
The invention aims to provide a zero-pressure-difference exhaust device of an aerostat, which has the advantages of simple and reasonable structure, light weight, high strength, good sealing performance and easiness in assembly.
The technical scheme for realizing the purpose of the invention is as follows:
the utility model provides an aerostatics zero differential pressure exhaust apparatus, includes the casing, its characterized in that: the bottom of the shell is provided with an exhaust sealing cover; the shell is internally provided with a power transmission device for driving the exhaust sealing cover to move up and down; the shell and the exhaust sealing cover are both circular; a trapezoidal male die is arranged below the shell along the circumferential direction, a trapezoidal female die is correspondingly arranged above the exhaust sealing cover along the circumferential direction, and the male die and the female die are matched to form sealing.
Furthermore, power transmission has lead screw, screw nut, transmission piece, and the vertical setting of lead screw can be rotated by exhaust motor drive, and screw nut installs on the lead screw, but up-and-down motion under the lead screw drives, but transmission piece up-and-down motion under screw nut drives.
Further, a spring is arranged between the screw nut and the transmission block, the transmission block is installed on the guide rail, and the guide rail is located on the outer side of the screw.
Furthermore, the upper part of the exhaust sealing cover is connected with a second guide rod, the second guide rod is vertically arranged, and the second guide rod is connected with a transmission block.
Furthermore, a travel switch shifting sheet is arranged on the second guide rod; an upper travel micro switch and a lower travel micro switch are arranged in the shell, are controlled by a travel switch shifting piece and are used for controlling the starting and stopping of the exhaust motor.
Furthermore, a supporting mechanism is arranged in the shell and consists of a first guide rod and a plurality of reinforcing rib plates, the first guide rod is vertically arranged, is positioned at the central position of the inner ends of the plurality of reinforcing rib plates and is fixedly connected with the reinforcing rib plates, and the outer ends of the reinforcing rib plates are fixed with the shell; the second guide rod is positioned on the inner side of the first guide rod, and the first guide rod is provided with a strip-shaped through hole.
Furthermore, the shell and the reinforcing rib plate are both in hollow design, the shell and the exhaust sealing cover of the reinforcing rib plate are both made of carbon fiber and PMI composite board, and the first guide rod and the second guide rod are both made of carbon fiber material; all parts of the power transmission device are made of aluminum alloy materials.
The invention has the following beneficial effects:
the bottom of the shell is provided with an exhaust sealing cover; the shell is internally provided with a power transmission device for driving the exhaust sealing cover to move up and down; the power transmission device is provided with a lead screw, a lead screw nut and a transmission block, the lead screw is vertically arranged and can be driven to rotate by an exhaust motor, the lead screw nut is installed on the lead screw and can move up and down under the drive of the lead screw, and the transmission block can move up and down under the drive of the lead screw nut. According to the invention, the trapezoidal male die is arranged below the shell along the circumferential direction, the trapezoidal female die is correspondingly arranged above the exhaust sealing cover along the circumferential direction, and the male die and the female die are matched to form sealing, so that the sealing property of the exhaust device is effectively ensured. The invention has simple and reasonable structure, light weight, high strength, good sealing performance and easy assembly.
The upper part of the exhaust sealing cover is connected with a second guide rod, the second guide rod is vertically arranged, and the second guide rod is connected with a transmission block; a travel switch shifting sheet is arranged on the second guide rod; an upper travel micro switch and a lower travel micro switch are arranged in the shell, are controlled by a travel switch shifting piece and are used for controlling the starting and stopping of the exhaust motor. The invention carries out exhaust control through the stroke microswitch, so that the exhaust control has stronger working reliability.
According to the invention, the spring is arranged between the screw nut and the transmission block and serves as a buffer element, so that the switch plectrum can trigger the microswitch again to stop the operation of the exhaust motor after the exhaust sealing cover is fully sealed, and the sealing performance of the exhaust device after exhaust reset is further ensured.
A supporting mechanism is arranged in a shell and consists of a first guide rod and a plurality of reinforcing rib plates, the first guide rod is vertically arranged, is positioned at the central position of the inner ends of the reinforcing rib plates and is fixedly connected with the reinforcing rib plates, and the outer ends of the reinforcing rib plates are fixed with the shell; the second guide rod is positioned on the inner side of the first guide rod, and the first guide rod is provided with a strip-shaped through hole.
The shell and the reinforcing rib plate are all in hollow design, the shell, the reinforcing rib plate and the exhaust sealing cover are all made of carbon fiber and PMI composite plates, and the first guide rod and the second guide rod are made of carbon fiber materials; all parts of the power transmission device are made of aluminum alloy materials, so that the performance of light weight, firm structure and easy assembly is further ensured.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the transmission of the present invention;
FIG. 3 is a schematic view of the support structure within the housing of the present invention;
FIG. 4 is a schematic view of the construction of the vent seal cover of the present invention;
FIG. 5 is an enlarged view of part A, showing the structure of the microswitch part of the present invention;
fig. 6 is a schematic view of the structure of the sealing portion of the present invention.
Detailed Description
As shown in fig. 1, the bottom of the shell 2 is provided with an exhaust sealing cover 3; the shell 2 is internally provided with a power transmission device 1 for driving the exhaust sealing cover 3 to move up and down. The shell 2 and the exhaust sealing cover 3 are both circular. As shown in fig. 6, a trapezoidal male die 15 is arranged below the shell along the circumferential direction, a trapezoidal female die 16 is correspondingly arranged above the exhaust sealing cover along the circumferential direction, and the male die 15 and the female die 16 are matched to form sealing.
As shown in fig. 2 and fig. 1, the power transmission device has a lead screw 4, a lead screw nut 5 and a transmission block 6, the lead screw 4 is vertically arranged and can be driven to rotate by an exhaust motor through a speed reducer assembly 7, the lead screw nut 5 is installed on the lead screw 4 and can move up and down under the drive of the lead screw 4, and the transmission block 6 can move up and down under the drive of the lead screw nut 5. Be equipped with spring 8 between screw nut 5 and the driving block 6, driving block 6 installs on guide rail 9, and guide rail 9 is located the lead screw 4 outside.
As shown in fig. 4 and fig. 1, the upper part of the exhaust sealing cover 3 is connected with a second guide rod 10, the second guide rod 10 is vertically arranged, and the second guide rod 10 is externally connected with a reinforcing rib 11. The second guide rod 10 is connected with the transmission block 6, and a travel switch shifting sheet is arranged on the second guide rod 10; as shown in fig. 5 and 1, an up-stroke microswitch 18 and a down-stroke microswitch 18 are arranged in the shell, and the microswitch 18 is arranged on the mounting block 17. Is controlled by a travel switch plectrum and is used for controlling the start and stop of the exhaust motor. In implementation, the microswitch 18 is an avionics product and has the excellent characteristics of cold resistance and low temperature resistance.
As shown in fig. 3 and fig. 1, a supporting mechanism is arranged in the shell, the supporting mechanism is composed of a first guide rod 12 and a plurality of reinforcing rib plates 13, the first guide rod 12 is vertically arranged, is positioned at the central position of the inner ends of the plurality of reinforcing rib plates 13 and is fixedly connected with the reinforcing rib plates 13, and the outer ends of the reinforcing rib plates 13 are fixed with the inner side of the shell 2; the second guide rod is positioned at the inner side of the first guide rod 12, and the first guide rod 12 is provided with a strip-shaped through hole.
The shell 2 and the reinforcing rib plate 13 are both in hollow design, the shell 2, the reinforcing rib plate 13 and the exhaust sealing cover 3 are all made of carbon fiber and PMI composite plates, and the first guide rod 12 and the second guide rod 10 are all made of carbon fiber materials; each component of the power transmission device 1 is made of an aluminum alloy material.
When the aerostat is lifted, the exhaust motor is started, the exhaust motor drives the screw rod 4 to rotate through the speed reducer assembly 7, the screw rod nut 5 drives the exhaust sealing cover 3 to slowly move downwards through the transmission block 6, when the designed stroke is reached, the switch shifting sheet on the second guide rod 10 triggers the lower stroke microswitch, the exhaust motor stops rotating, and the valve reaches the maximum opening stroke.
When the aerostat reaches a stable state, the exhaust motor drives the screw rod 4 to rotate reversely, the screw rod nut 5 drives the exhaust sealing cover 3 to slowly move upwards through the transmission block 6, when the exhaust sealing cover is tightly sealed, the switch shifting sheet on the second guide rod 10 triggers the upper-stroke microswitch, and the exhaust motor stops rotating. The spring 8 between the screw nut 5 and the transmission block 6 is used as a buffer element, so that the exhaust sealing cover firstly compresses the sealing strip to achieve a sealing effect, then the exhaust motor rotates for a short time, the microswitch is triggered again, the problem that the microswitch is triggered by the switch plectrum and the motor stops rotating is solved, the microswitch is triggered by the switch plectrum after the exhaust sealing cover is fully sealed, the exhaust motor is stopped, and the sealing performance of the exhaust device after exhaust resetting is further ensured.
Claims (1)
1. The utility model provides a circular exhaust apparatus of aerostatics zero-pressure differential, includes the casing, its characterized in that: the bottom of the shell is provided with an exhaust sealing cover; the shell is internally provided with a power transmission device for driving the exhaust sealing cover to move up and down; the shell and the exhaust sealing cover are both circular; a trapezoidal male die is arranged below the shell along the circumferential direction, a trapezoidal female die is correspondingly arranged above the exhaust sealing cover along the circumferential direction, and the male die and the female die are matched to form sealing; the power transmission device is provided with a lead screw, a lead screw nut and a transmission block, wherein the lead screw is vertically arranged and can be driven to rotate by an exhaust motor, the lead screw nut is arranged on the lead screw and can move up and down under the drive of the lead screw, and the transmission block can move up and down under the drive of the lead screw nut; a spring is arranged between the screw nut and the transmission block, the transmission block is arranged on a guide rail, and the guide rail is positioned outside the screw;
a supporting mechanism is arranged in the shell and consists of a first guide rod and a plurality of reinforcing rib plates, the first guide rod is vertically arranged, is positioned at the central position of the inner ends of the plurality of reinforcing rib plates and is connected and fixed with the reinforcing rib plates, and the outer ends of the reinforcing rib plates are fixed with the shell; the second guide rod is positioned at the inner side of the first guide rod, and the first guide rod is provided with a strip-shaped through hole;
the upper part of the exhaust sealing cover is connected with a second guide rod, the second guide rod is vertically arranged, and the second guide rod is externally connected with a reinforcing rib; the second guide rod is connected with the transmission block, and a travel switch shifting piece is arranged on the second guide rod; an upper travel micro switch and a lower travel micro switch are arranged in the shell, the micro switches are arranged on the mounting block, and the start and stop of the exhaust motor are controlled by a travel switch shifting piece;
when the exhaust sealing cover is tightly sealed, the switch shifting sheet on the second guide rod triggers the upper travel micro switch, and the exhaust motor stops rotating; a spring between the screw nut and the transmission block is used as a buffer, so that the exhaust sealing cover firstly compresses the sealing strip, then the exhaust motor rotates for a small time, and then the microswitch is triggered;
the shell and the reinforcing rib plate are all in hollow design, the shell, the reinforcing rib plate and the exhaust sealing cover are all made of carbon fiber and PMI composite plates, and the first guide rod and the second guide rod are made of carbon fiber materials; all parts of the power transmission device are made of aluminum alloy materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710738251.3A CN107651159B (en) | 2017-08-24 | 2017-08-24 | Aerostatics zero pressure differential circular exhaust apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710738251.3A CN107651159B (en) | 2017-08-24 | 2017-08-24 | Aerostatics zero pressure differential circular exhaust apparatus |
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| Publication Number | Publication Date |
|---|---|
| CN107651159A CN107651159A (en) | 2018-02-02 |
| CN107651159B true CN107651159B (en) | 2020-01-14 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710738251.3A Active CN107651159B (en) | 2017-08-24 | 2017-08-24 | Aerostatics zero pressure differential circular exhaust apparatus |
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| CN (1) | CN107651159B (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| EP3875918A1 (en) | 2020-03-02 | 2021-09-08 | Husqvarna Ab | Transmitter device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102700703A (en) * | 2012-06-05 | 2012-10-03 | 中国电子科技集团公司第三十八研究所 | Air intake and exhaust device and aerostat with same |
| CN104029812A (en) * | 2014-06-25 | 2014-09-10 | 中国科学院光电研究院 | Electric control valve and stratospheric airship intake and exhaust integrated device |
| CN104132176A (en) * | 2014-07-18 | 2014-11-05 | 中国科学院光电研究院 | Photoelectric control valve of aerostat |
| CN105129067A (en) * | 2015-07-16 | 2015-12-09 | 中国科学院光电研究院 | Current limiting closed exhaust valve used for aerostat and control method used for limiting same |
| RU2588364C1 (en) * | 2015-02-02 | 2016-06-27 | Акционерное общество "Долгопрудненское конструкторское бюро автоматики" (АО "ДКБА") | Device for automatic gas valve of airship |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2848734Y (en) * | 2005-09-16 | 2006-12-20 | 孟庆华 | Domestic grain storage box |
| CN200995834Y (en) * | 2007-01-12 | 2007-12-26 | 金春斌 | Sealed article container |
| CN203450546U (en) * | 2013-11-21 | 2014-02-26 | 纪腾云 | Box cover structure of injection molding food container |
| CN107013734B (en) * | 2017-06-02 | 2023-08-25 | 陈丽端 | Electric valve opening and closing protector |
-
2017
- 2017-08-24 CN CN201710738251.3A patent/CN107651159B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102700703A (en) * | 2012-06-05 | 2012-10-03 | 中国电子科技集团公司第三十八研究所 | Air intake and exhaust device and aerostat with same |
| CN104029812A (en) * | 2014-06-25 | 2014-09-10 | 中国科学院光电研究院 | Electric control valve and stratospheric airship intake and exhaust integrated device |
| CN104132176A (en) * | 2014-07-18 | 2014-11-05 | 中国科学院光电研究院 | Photoelectric control valve of aerostat |
| RU2588364C1 (en) * | 2015-02-02 | 2016-06-27 | Акционерное общество "Долгопрудненское конструкторское бюро автоматики" (АО "ДКБА") | Device for automatic gas valve of airship |
| CN105129067A (en) * | 2015-07-16 | 2015-12-09 | 中国科学院光电研究院 | Current limiting closed exhaust valve used for aerostat and control method used for limiting same |
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| Publication number | Publication date |
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| CN107651159A (en) | 2018-02-02 |
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