CN203674392U - Hypersonic aerocraft telemetering antenna window connection apparatus - Google Patents
Hypersonic aerocraft telemetering antenna window connection apparatus Download PDFInfo
- Publication number
- CN203674392U CN203674392U CN201320616563.4U CN201320616563U CN203674392U CN 203674392 U CN203674392 U CN 203674392U CN 201320616563 U CN201320616563 U CN 201320616563U CN 203674392 U CN203674392 U CN 203674392U
- Authority
- CN
- China
- Prior art keywords
- antenna
- box
- window
- windows
- heat insulating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Details Of Aerials (AREA)
Abstract
The utility model provides a dypersonic aerocraft telemetering antenna window connection apparatus. The apparatus comprises a covering, an antenna window, an antenna, a heat insulating gasket, a rubber gasket, an antenna box and connection screws. The antenna box is a square box, and is fixedly connected to the inner surface of the covering. The rubber gasket is square-shaped, and is arranged at the bottom of the antenna box. The antenna is provided with a stepped panel and a lower wiring post. The antenna is disposed inside the antenna box, and the wiring post passes through a through hole on the bottom of the antenna box and is connected with a cable. The heat insulation gasket is square-shaped, and is arranged on the periphery of the stepped panel of the antenna. The antenna window is a cube, and is internally provided with a stepped cavity matching with the stepped panel of the antenna. The antenna is sleeved by the antenna window. The antenna window, the heat insulating gasket made of glass fiber reinforced plastics, the antenna and the antenna box are all provided with connection holes at four corners, and are fastened by the connection bolts.
Description
Technical field
The utility model relates to aerospace craft technical field, is specifically related to hypersonic aircraft antenna windows jockey.
Background technology
In aviation flight test, mainly realize by telemetering antenna the function of measuring and control data being transmitted back to ground observing and controlling equipment constantly, normally work for guarantee antenna, need to carry out conservation treatment to it, increase antenna windows.Antenna windows is quartzy material, has wave transparent and heat insulating function, and antenna windows is fragility material, is subject to shock loading and easily damages, and need to carry out vibration damping encapsulation process.
Utility model content
For solving the requirement of telemetering antenna window connection reliability, the utility model proposes a kind of hypersonic aircraft antenna windows jockey.
A kind of hypersonic aircraft telemetering antenna window jockey, comprises covering, antenna windows, antenna, heat insulating mattress, rubber sheet gasket, antenna box, attachment screw; Antenna box is square box body, is fixed on covering inner surface, and rubber sheet gasket is block form, be placed in antenna box bottom, antenna has a stairstepping flat board, under have binding post, antenna is placed in antenna box, binding post is connected with cable through the through hole of antenna box bottom, and heat insulating mattress is block form, is socketed on antenna stairstepping flat board, the antenna windows side of being body, inside be provided with stairstepping cavity, antenna windows stairstepping cavity and antenna have a stairstepping writing board shape to adapt, and antenna windows is socketed on antenna; Four jiaos of antenna windows, heat insulating mattress, antenna, antenna box are provided with connecting hole, tighten with attachment screw.
The utility model adopts rubber sheet gasket, and material self deformation quantity is large, can, by the compressive deformation of self in the time receiving impact, reduce the impact to antenna windows, plays vibration isolation sealing function.Heat insulating mattress adopts heat-proof quality good material, is socketed on antenna, can well completely cut off outside heat, protection antenna.The utility model is simple in structure, safe and reliable, cost is low, the process-cycle is short, is applicable to heat insulation, sealing, the vibration damping of aerospace craft telemetering antenna window.
Brief description of the drawings
Fig. 1: the utility model telemetering antenna connecting overall structural representation;
Fig. 2: the utility model telemetering antenna connection diagram;
Fig. 3: the utility model telemetering antenna window connection diagram;
Fig. 4: the utility model telemetering antenna window construction schematic diagram;
Fig. 5: the utility model telemetering antenna heat insulating mattress structural representation;
Fig. 6: the utility model telemetering antenna rubber sheet gasket structural representation;
Fig. 7: the utility model telemetering antenna box structural representation.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described further.
A kind of hypersonic aircraft telemetering antenna window jockey, comprises covering 1, antenna windows 2, antenna 3, heat insulating mattress 4, rubber sheet gasket 5, antenna box 6, attachment screw 7.As shown in Figure 1, Figure 2, Figure 3 shows.
Antenna box 6 is square box body, as shown in Figure 7, be fixed on covering 1 inner surface, rubber sheet gasket 5 is block form, as shown in Figure 6, be placed in antenna box 6 bottoms, antenna 3 has a stairstepping flat board, under have binding post, antenna 3 is placed in antenna box 6, binding post is connected with cable through the through hole of antenna box 6 bottoms, heat insulating mattress 4 is block form, as shown in Figure 5, be socketed on antenna 3 stairstepping flat boards, antenna windows 2 side's of being bodies, as shown in Figure 4, inside be provided with stairstepping cavity, antenna windows 2 stairstepping cavitys and antenna 3 have a stairstepping writing board shape to adapt, antenna windows 2 is socketed on antenna 3.6 four jiaos of antenna windows 2, heat insulating mattress 4, antenna 3, antenna box are provided with connecting hole, tighten with attachment screw 7.Described rubber sheet gasket 5 is silicon rubber material, and described heat insulating mattress 4 is fiberglass pad.
Claims (1)
1. a hypersonic aircraft telemetering antenna window jockey, comprises covering (1), antenna windows (2), antenna (3), heat insulating mattress (4), rubber sheet gasket (5), antenna box (6), attachment screw (7), antenna box (6) is square box body, be fixed on covering (1) inner surface, rubber sheet gasket (5) is block form, be placed in antenna box (6) bottom, antenna (3) has a stairstepping flat board, under have binding post, antenna (3) is placed in antenna box (6), binding post is connected with cable through the through hole of antenna box (6) bottom, heat insulating mattress (4) is block form, be socketed on antenna (3) stairstepping flat board, antenna windows (2) side of being body, inside be provided with stairstepping cavity, antenna windows (2) stairstepping cavity and antenna (3) have a stairstepping writing board shape to adapt, antenna windows (2) is socketed on antenna (3), (6) four jiaos of antenna windows (2), heat insulating mattress (4), antenna (3), antenna box are provided with connecting hole, tighten with attachment screw (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320616563.4U CN203674392U (en) | 2013-09-30 | 2013-09-30 | Hypersonic aerocraft telemetering antenna window connection apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320616563.4U CN203674392U (en) | 2013-09-30 | 2013-09-30 | Hypersonic aerocraft telemetering antenna window connection apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203674392U true CN203674392U (en) | 2014-06-25 |
Family
ID=50970651
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320616563.4U Expired - Fee Related CN203674392U (en) | 2013-09-30 | 2013-09-30 | Hypersonic aerocraft telemetering antenna window connection apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203674392U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105914463A (en) * | 2016-06-28 | 2016-08-31 | 湖北航天技术研究院总体设计所 | Flexible connection device for high-temperature resistant radome |
| CN107732413A (en) * | 2017-09-22 | 2018-02-23 | 南京航空航天大学 | It is installed on the antenna feeder being connected in aircraft horizontal tail with radio altimeter |
-
2013
- 2013-09-30 CN CN201320616563.4U patent/CN203674392U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105914463A (en) * | 2016-06-28 | 2016-08-31 | 湖北航天技术研究院总体设计所 | Flexible connection device for high-temperature resistant radome |
| CN105914463B (en) * | 2016-06-28 | 2018-07-31 | 湖北航天技术研究院总体设计所 | A kind of flexible connecting device of high temperature resistant antenna house |
| CN107732413A (en) * | 2017-09-22 | 2018-02-23 | 南京航空航天大学 | It is installed on the antenna feeder being connected in aircraft horizontal tail with radio altimeter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204726664U (en) | Unmanned vehicle | |
| CN203674392U (en) | Hypersonic aerocraft telemetering antenna window connection apparatus | |
| CN203930096U (en) | Digital campus weather station | |
| CN103545594B (en) | A kind of hypersonic aircraft telemetry antenna window erecting device | |
| WO2009102373A3 (en) | Modules and methods for biasing power to a multi-engine power plant suitable for one engine inoperative flight procedure training | |
| CN204822073U (en) | Many rotor unmanned aerial vehicle's software protective housing | |
| FR2976913B1 (en) | COMBINED EMERGENCY BEACON AND FLIGHT RECORDER DEVICE FOR AIRCRAFT AND AIRCRAFT EQUIPPED WITH SUCH A DEVICE | |
| MX2007015026A (en) | Toy aircraft. | |
| CN204776007U (en) | Many rotors of agricultural plant protection unmanned vehicles | |
| CN107631856A (en) | A kind of dynamometry, pressure measurement, angular surveying, vibration suppression allpurpose model | |
| CN203672523U (en) | Comprehensive unmanned plane engine test bench | |
| CN102519701A (en) | Vehicle-mounted aeroelastic test platform system | |
| CN203516585U (en) | Large-area compound damping vibration attenuation structure applicable to spacecraft | |
| WO2009105404A3 (en) | Wireless landing gear verification system | |
| CN206114474U (en) | Atmospheric environment remote sensing monitoring mechanism | |
| CN102991873A (en) | Egg protection device | |
| CN204985504U (en) | A honeycomb damping vibration damper for surface feature spectrum appearance standard board | |
| CN204495528U (en) | A kind of side knock enhanced type semi-submersible lng floating impacts platform | |
| CN204219777U (en) | aerial toy | |
| CN208057091U (en) | A kind of oil pumping machine well head defroster | |
| CN202961879U (en) | Inflating type remote control airplane | |
| CN205719012U (en) | A kind of ultrasound probe collision prevention device | |
| CN203793653U (en) | Maintenance covering cap connecting device for on-water floating recorder | |
| CN104696404A (en) | Vibration reduction device for flight sensor of unmanned aerial vehicle | |
| CN103112580A (en) | Balloon flying machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140625 Termination date: 20150930 |
|
| EXPY | Termination of patent right or utility model |