CN112751586A - Radio frequency communication system for aircraft - Google Patents
Radio frequency communication system for aircraft Download PDFInfo
- Publication number
- CN112751586A CN112751586A CN202110067389.1A CN202110067389A CN112751586A CN 112751586 A CN112751586 A CN 112751586A CN 202110067389 A CN202110067389 A CN 202110067389A CN 112751586 A CN112751586 A CN 112751586A
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- block
- radio frequency
- frequency communication
- fixed
- communication system
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B1/00—Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
- H04B1/38—Transceivers, i.e. devices in which transmitter and receiver form a structural unit and in which at least one part is used for functions of transmitting and receiving
- H04B1/40—Circuits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/08—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with rubber springs ; with springs made of rubber and metal
- F16F15/085—Use of both rubber and metal springs
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B15/00—Suppression or limitation of noise or interference
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Mobile Radio Communication Systems (AREA)
Abstract
The invention discloses a radio frequency communication system for an aircraft, relates to the technical field of auxiliary devices for aircraft radio frequency communication, and aims to solve the problem that equipment is damaged and cannot be normally used due to the fact that internal equipment is not well protected when the existing radio frequency communication system for the aircraft is used. The upper end of the fixed bottom block is provided with a fixed upper square block, the inside side of the fixed upper square block is provided with a limiting inner block, the limiting inner block is connected with the fixed bottom block in a welded mode, the inside of the limiting inner block is provided with a placing bottom plate, the placing bottom plate is fixedly connected with the fixed bottom block through a buffer spring, a buffering soft cushion block is arranged below the inside of the fixed upper square block, the upper end of the placing bottom plate is provided with a radio frequency communication module, the outside of the radio frequency communication module is provided with a supporting vertical column, the upper end of the supporting vertical column is provided with a buffering convex block, an anti-interference module is arranged above the radio frequency communication module, and the anti-interference module and the supporting vertical column are fixedly.
Description
Technical Field
The invention relates to the technical field of auxiliary devices for aircraft radio frequency communication, in particular to a radio frequency communication system for an aircraft.
Background
Aircraft (flight vehicle) is an apparatus flying in the atmosphere or in the space (space) outside the atmosphere, and the aircraft is classified into 3 types: aircraft, spacecraft, rockets, and missiles. The radio frequency communication system for the aircraft is used when the aircraft flies in the atmosphere and is called as an aircraft, such as a balloon, an airship, an airplane and the like, and the aircraft flies by the static buoyancy of air or the aerodynamic force generated by the relative motion of the air.
The problem that equipment is damaged and cannot be normally used due to the fact that the existing radio frequency communication system for the aircraft is not good enough in protection of internal equipment when in use is solved.
Disclosure of Invention
The present invention provides a radio frequency communication system for an aircraft, so as to solve the problem that the existing radio frequency communication system for an aircraft is often damaged and cannot be used normally due to insufficient protection of internal equipment when in use.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a radio frequency communication system that aircraft was used, includes fixed bottom block, the upper end of fixed bottom block is provided with fixed square, the inside side of fixed square is provided with spacing interior piece, and spacing interior piece and fixed bottom block welded connection, the inside of spacing interior piece is provided with places the bottom plate, and places the bottom plate and pass through buffer spring fixed connection with fixed bottom block, the inside below of fixed square is provided with buffering cushion block, the upper end of placing the bottom plate is provided with radio frequency communication module, radio frequency communication module's outside is provided with supports the upstand, the upper end of supporting the upstand is provided with buffering lug, radio frequency communication module's top is provided with anti-interference module, and anti-interference module and support the upstand pass through division board fixed connection, anti-interference module and radio frequency communication module pass through electric connection.
Preferably, four corners of fixed bottom block below all are provided with the bolt and place the hole, the below of fixed bottom block is provided with anti-skidding filler strip fixed block, and anti-skidding filler strip fixed block passes through draw-in groove welded connection with fixed bottom block, the below of anti-skidding filler strip fixed block is provided with anti-skidding filler strip, and anti-skidding filler strip passes through the stickness with anti-skidding filler strip fixed block and is connected.
Preferably, two moving handles are arranged above the fixed upper square block and are welded with the fixed upper square block through clamping grooves, a movable overhauling cover is arranged on one side of the fixed upper square block and is fixedly connected with the fixed upper square block through the clamping grooves, and a movable overhauling cover handle is arranged below the movable overhauling cover and is welded with the movable overhauling cover.
Preferably, the two sides of the placing bottom plate are provided with sliding rolling balls, the sliding rolling balls are connected with the placing bottom plate through the clamping grooves in a rotating mode, the sliding rolling balls are provided with a plurality of parts, and the two sides of the fixed upper square are provided with ventilating cover plates.
Preferably, one side of the ventilation cover plate is provided with a clamping column placing groove, the clamping column placing grooves are four, four corners of one side of the ventilation cover plate are provided with limiting clamping columns, the limiting clamping columns are connected with the ventilation cover plate in a welded mode, one ends of the limiting clamping columns extend to the inside of the clamping column placing grooves, one sides of the limiting clamping columns are provided with conical fixture blocks, and the conical fixture blocks are connected with the limiting clamping columns in a welded mode.
Preferably, the one end of ventilation apron is provided with the circulation round hole, and the circulation round hole is provided with a plurality of, the outside of ventilation apron is provided with spacing inner block, and just spacing inner block passes through the stickness with fixed last square and is connected.
Compared with the prior art, the invention has the beneficial effects that:
1. this kind of radio frequency communication system that aircraft was used compares with current aircraft radio frequency communication auxiliary device, has been equipped with buffer spring, buffering cushion piece and buffering lug, and buffer spring, buffering cushion piece and buffering lug's design can let this kind of radio frequency communication system that aircraft was used protect the internal equipment better when using, has solved the radio frequency communication system that current aircraft was used often because to protect the problem that leads to the impaired unable normal use of equipment to the internal equipment not good enough.
2. Compared with the existing auxiliary device for aircraft radio frequency communication, the radio frequency communication system for the aircraft is provided with the anti-interference module, the design of the anti-interference module can ensure that the information transmission of the radio frequency communication system for the aircraft is safer when in use, and the problem that the information cannot be transmitted due to the fact that communication signals are interfered frequently when the existing radio frequency communication system for the aircraft is used is solved.
Drawings
FIG. 1 is a front view of the overall structure of the present invention;
FIG. 2 is a cross-sectional view of the overall construction of the present invention;
fig. 3 is a partially enlarged view of the area a of fig. 2 according to the present invention.
In the figure: 1. fixing the bottom block; 2. a bolt placing hole; 3. a vent cover plate; 4. fixing the upper square block; 5. A circular flow hole; 6. moving the handle; 7. overhauling the movable cover; 8. a movable cover handle; 9. the antiskid filler strip fixing block; 10. an anti-slip filler strip; 11. sliding the ball; 12. limiting the inner block; 13. a buffer spring; 14. a column clamping placement groove; 15. a conical fixture block; 16. placing a bottom plate; 17. supporting the vertical column; 18. a radio frequency communication module; 19. a partition plate; 20. an anti-interference module; 21. buffering the soft cushion block; 22. a buffer bump; 23. limiting the inner block; 24. and limiting the clamping column.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Referring to fig. 1-3, an embodiment of the present invention is shown: a radio frequency communication system for an aircraft comprises a fixed bottom block 1, a fixed upper square block 4 is arranged at the upper end of the fixed bottom block 1, a limit inner block 12 is arranged at the square inside the fixed upper square block 4, the limit inner block 12 is welded with the fixed bottom block 1, the limit inner block 12 is more firmly connected with the fixed bottom block 1, a placing bottom plate 16 is arranged inside the limit inner block 12, the placing bottom plate 16 is fixedly connected with the fixed bottom block 1 through a buffer spring 13, the placing bottom plate 16 is more firmly connected with the fixed bottom block 1, a buffer soft cushion block 21 is arranged below the inside of the fixed upper square block 4, a radio frequency communication module 18 is arranged at the upper end of the placing bottom plate 16, a supporting vertical column 17 is arranged outside the radio frequency communication module 18, a buffer lug 22 is arranged at the upper end of the supporting vertical column 17, an anti-interference module 20 is arranged above the radio frequency communication module 18, and the anti-interference module 20 is fixedly connected with the supporting vertical column 17, the connection between the anti-interference module 20 and the supporting vertical column 17 is firmer, and the anti-interference module 20 is electrically connected with the radio frequency communication module 18.
Further, four corners of fixed bottom block 1 below all are provided with the bolt and place hole 2, the below of fixed bottom block 1 is provided with anti-skidding filler strip fixed block 9, and anti-skidding filler strip fixed block 9 passes through draw-in groove welded connection with fixed bottom block 1, it is more firm to let anti-skidding filler strip fixed block 9 be connected with fixed bottom block 1, the below of anti-skidding filler strip fixed block 9 is provided with anti-skidding filler strip 10, and anti-skidding filler strip 10 passes through the stickness with anti-skidding filler strip fixed block 9 and is connected, let anti-skidding filler strip 10 be more firm with being connected of anti-skidding filler strip fixed block 9.
Further, the upper side of the fixed upper square block 4 is provided with a moving handle 6, the moving handle 6 is connected with the fixed upper square block 4 through a clamping groove in a welded mode, the moving handle 6 is more firmly connected with the fixed upper square block 4, the moving handle 6 is provided with two, one side of the fixed upper square block 4 is provided with an overhauling movable cover 7, the overhauling movable cover 7 is fixedly connected with the fixed upper square block 4 through the clamping groove, a movable cover handle 8 is arranged below the overhauling movable cover 7, the movable cover handle 8 is connected with the overhauling movable cover 7 in a welded mode, and the movable cover handle 8 is more firmly connected with the overhauling movable cover 7.
Further, the both sides of placing bottom plate 16 all are provided with slip spin 11, and slip spin 11 with place bottom plate 16 and pass through the draw-in groove and rotate and be connected, let slip spin 11 more firm with the connection of placing bottom plate 16, slip spin 11 is provided with a plurality of, and the both sides of fixed square 4 all are provided with the apron of ventilating 3.
Further, one side of ventilation apron 3 is provided with card post standing groove 14, and card post standing groove 14 is provided with four, four corners of ventilation apron 3 one side all are provided with spacing calorie of post 24, and spacing calorie of post 24 and ventilation apron 3 welded connection, let spacing calorie of post 24 more firm with ventilation apron 3's connection, the one end of spacing calorie of post 24 extends to the inside of card post standing groove 14, one side of spacing calorie of post 24 is provided with toper fixture block 15, and toper fixture block 15 and spacing calorie of post 24 welded connection, let toper fixture block 15 more firm with spacing calorie of connection of post 24.
Further, the one end of the cover plate 3 of ventilating is provided with circulation round hole 5, and the circulation round hole 5 is provided with a plurality of, and the outside of the cover plate 3 of ventilating is provided with spacing inner block 23, and spacing inner block 23 passes through the stickness with fixed square 4 and is connected, lets spacing inner block 23 and fixed square 4's connection more firm.
The working principle is as follows: when the radio frequency communication system for the aircraft is used, the radio frequency communication system for the aircraft is taken to a position needing to be used, then the bolt can be taken out and placed in the bolt placing hole 2, at the moment, the radio frequency communication system for the aircraft can be better fixed, when the radio frequency communication system for the aircraft is impacted, the buffer spring 13, the buffer soft cushion block 21 and the buffer bump 22 in the upper square block 4 can be fixed, the probability of internal damage of the radio frequency communication system for the aircraft can be greatly reduced, and when the radio frequency communication system for the aircraft carries out signal transmission, the anti-interference module 20 can enable the signal transmission to be safer at the moment.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. A radio-frequency communication system for an aircraft, comprising a fixed bottom block (1), characterized in that: the upper end of the fixed bottom block (1) is provided with a fixed upper square block (4), a limit inner block (12) is arranged at the inner side of the fixed upper square block (4), the limit inner block (12) is welded with the fixed bottom block (1), a placing bottom plate (16) is arranged inside the limit inner block (12), the placing bottom plate (16) is fixedly connected with the fixed bottom block (1) through a buffer spring (13), a buffer soft cushion block (21) is arranged below the inner side of the fixed upper square block (4), a radio frequency communication module (18) is arranged at the upper end of the placing bottom plate (16), a supporting vertical column (17) is arranged outside the radio frequency communication module (18), a buffer convex block (22) is arranged at the upper end of the supporting vertical column (17), an anti-interference module (20) is arranged above the radio frequency communication module (18), and the anti-interference module (20) is fixedly connected with the supporting vertical column (17) through a partition plate (19), the anti-interference module (20) is electrically connected with the radio frequency communication module (18).
2. A radio frequency communication system for an aircraft according to claim 1, wherein: four corners of fixed bottom piece (1) below all are provided with the bolt and place hole (2), the below of fixed bottom piece (1) is provided with anti-skidding filler strip fixed block (9), and anti-skidding filler strip fixed block (9) pass through draw-in groove welded connection with fixed bottom piece (1), the below of anti-skidding filler strip fixed block (9) is provided with anti-skidding filler strip (10), and anti-skidding filler strip (10) are connected through the stickness with anti-skidding filler strip fixed block (9).
3. A radio frequency communication system for an aircraft according to claim 1, wherein: the movable maintenance square block is characterized in that a moving handle (6) is arranged above the fixed upper square block (4), the moving handle (6) is connected with the fixed upper square block (4) through a clamping groove in a welded mode, the number of the moving handles (6) is two, a movable maintenance cover (7) is arranged on one side of the fixed upper square block (4), the movable maintenance cover (7) is fixedly connected with the fixed upper square block (4) through the clamping groove, a movable cover handle (8) is arranged below the movable maintenance cover (7), and the movable cover handle (8) is connected with the movable maintenance cover (7) in a welded mode.
4. A radio frequency communication system for an aircraft according to claim 1, wherein: the novel square placement machine is characterized in that sliding rolling balls (11) are arranged on two sides of the placement base plate (16), the sliding rolling balls (11) are connected with the placement base plate (16) in a rotating mode through clamping grooves, the sliding rolling balls (11) are provided with a plurality of parts, and ventilating cover plates (3) are arranged on two sides of the fixed upper square (4).
5. A radio frequency communication system for an aircraft according to claim 4, wherein: one side of ventilation apron (3) is provided with card post standing groove (14), and blocks post standing groove (14) and be provided with four, four corners of ventilation apron (3) one side all are provided with spacing card post (24), and spacing card post (24) and ventilation apron (3) welded connection, the one end of spacing card post (24) extends to the inside of card post standing groove (14), one side of spacing card post (24) is provided with toper fixture block (15), and toper fixture block (15) and spacing card post (24) welded connection.
6. A radio frequency communication system for an aircraft according to claim 4, wherein: one end of the ventilation cover plate (3) is provided with a circulation round hole (5), the circulation round hole (5) is provided with a plurality of, the outside of the ventilation cover plate (3) is provided with a limiting inner block (23), and the limiting inner block (23) is connected with the fixed upper square (4) through viscosity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110067389.1A CN112751586B (en) | 2021-01-19 | 2021-01-19 | Radio frequency communication system for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110067389.1A CN112751586B (en) | 2021-01-19 | 2021-01-19 | Radio frequency communication system for aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112751586A true CN112751586A (en) | 2021-05-04 |
| CN112751586B CN112751586B (en) | 2022-05-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110067389.1A Active CN112751586B (en) | 2021-01-19 | 2021-01-19 | Radio frequency communication system for aircraft |
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| Country | Link |
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| CN (1) | CN112751586B (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060029492A1 (en) * | 2004-08-04 | 2006-02-09 | Inventec Corporation | Three-dimensionally vibration-preventing buffering mechanism |
| CN107431164A (en) * | 2016-02-24 | 2017-12-01 | 日本碍子株式会社 | The method to set up of cell apparatus, battery unit and cell apparatus |
| CN108133680A (en) * | 2017-12-28 | 2018-06-08 | 徐州赛恩斯源新材料科技有限公司 | A kind of holographic projector of good damping effect |
| CN109730135A (en) * | 2019-02-01 | 2019-05-10 | 扬州兴湖食品有限公司 | A kind of refrigerator of the aquatic product transportation with defencive function |
| CN210840282U (en) * | 2019-11-26 | 2020-06-23 | 苏州乐仪智能科技有限公司 | Protective device of thermometer temperature controller |
| CN111372401A (en) * | 2020-03-09 | 2020-07-03 | 合肥学院 | Anti-interference electronic information equipment |
| CN211809024U (en) * | 2020-03-20 | 2020-10-30 | 宁波市拓欧金属制品有限公司 | Engine right suspension support |
-
2021
- 2021-01-19 CN CN202110067389.1A patent/CN112751586B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060029492A1 (en) * | 2004-08-04 | 2006-02-09 | Inventec Corporation | Three-dimensionally vibration-preventing buffering mechanism |
| CN107431164A (en) * | 2016-02-24 | 2017-12-01 | 日本碍子株式会社 | The method to set up of cell apparatus, battery unit and cell apparatus |
| CN108133680A (en) * | 2017-12-28 | 2018-06-08 | 徐州赛恩斯源新材料科技有限公司 | A kind of holographic projector of good damping effect |
| CN109730135A (en) * | 2019-02-01 | 2019-05-10 | 扬州兴湖食品有限公司 | A kind of refrigerator of the aquatic product transportation with defencive function |
| CN210840282U (en) * | 2019-11-26 | 2020-06-23 | 苏州乐仪智能科技有限公司 | Protective device of thermometer temperature controller |
| CN111372401A (en) * | 2020-03-09 | 2020-07-03 | 合肥学院 | Anti-interference electronic information equipment |
| CN211809024U (en) * | 2020-03-20 | 2020-10-30 | 宁波市拓欧金属制品有限公司 | Engine right suspension support |
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| Publication number | Publication date |
|---|---|
| CN112751586B (en) | 2022-05-03 |
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Address after: 210042 building 3, no.6, Suyuan Road, Xuanwu District, Nanjing City, Jiangsu Province Patentee after: Nanjing Yubao Technology Co.,Ltd. Address before: 210042 building 3, no.6, Suyuan Road, Xuanwu District, Nanjing City, Jiangsu Province Patentee before: NANJING YOUBEST TECHNOLOGY CO.,LTD. |