CN210897591U - Detachable structure for aircraft antenna - Google Patents
Detachable structure for aircraft antenna Download PDFInfo
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- CN210897591U CN210897591U CN201922419254.8U CN201922419254U CN210897591U CN 210897591 U CN210897591 U CN 210897591U CN 201922419254 U CN201922419254 U CN 201922419254U CN 210897591 U CN210897591 U CN 210897591U
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- antenna
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- aircraft antenna
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Abstract
The utility model belongs to aircraft antenna installation field relates to a detachable construction for aircraft antenna, on aircraft covering (1) internal surface, installation buckle (2) carry out buckle formula installation and dismantlement to aircraft antenna (3). This structure utilizes current ripe buckle device, carries out buckle formula installation to aircraft antenna, to the destruction problem of organism covering and antenna when solving aircraft antenna and dismantling, and the dismantlement of antenna is simple moreover, and the time spent is short, and work efficiency is high, great improvement aircraft antenna's maintenance efficiency. And the antenna is arranged on the inner surface of the airplane, and the outer surface is not opened, so that the aerodynamic appearance of the airplane cannot be damaged. The utility model discloses can be applied to the antenna installation field of various aircraft widely, have apparent market prospect and economic benefits.
Description
Technical Field
The invention belongs to the field of aircraft antenna installation, and relates to a detachable structure suitable for an aircraft antenna.
Background
The current installation of an onboard antenna is as shown in fig. 3 and 4, and is assembled with an aircraft skin 1 through bolts 4, but the aircraft antenna 3 is often required to be disassembled for testing or replacement, and the disassembly is time-consuming and labor-consuming for the installation method, and even the structure of an aircraft body and the structure of the antenna are damaged. In view of the current situation, a new detachable method suitable for an aircraft antenna is urgently needed to be researched.
Disclosure of Invention
The purpose of the invention is: the detachable structure for the aircraft antenna solves the problem of damage to an engine body skin and the aircraft antenna when the aircraft antenna is detached, simplifies the detaching procedure, shortens the detaching time and improves the maintenance efficiency of the aircraft antenna.
The technical scheme of the invention is as follows:
a detachable structure for an aircraft antenna, comprising:
and (3) installing a buckle 2 on the inner surface of the aircraft skin 1, and carrying out buckle type installation and disassembly on the aircraft antenna 3.
The buckle 2 is a rotatable movable buckle.
And a card slot device corresponding to the buckle is arranged on the antenna.
The buckle 2 is screwed on the inner surface of the aircraft skin 1.
The buckle 2 is welded on the inner surface of the aircraft skin 1.
The buckle 2 is an elastic metal buckle.
The invention has the advantages that: this structure utilizes current ripe buckle device, carries out buckle formula installation to aircraft antenna, to the destruction problem of organism covering and antenna when solving aircraft antenna and dismantling, and the dismantlement of antenna is simple moreover, and the time spent is short, and work efficiency is high, great improvement aircraft antenna's maintenance efficiency. And the antenna is arranged on the inner surface of the airplane, and the outer surface is not opened, so that the aerodynamic appearance of the airplane cannot be damaged. The invention can be widely applied to the field of antenna installation of various airplanes, and has remarkable market prospect and economic benefit.
Drawings
Fig. 1 is a schematic diagram of an antenna card of the present invention.
Fig. 2 is a schematic view of the antenna detachment of the present invention.
Fig. 3 is a schematic view of a conventional antenna screw connection.
Fig. 4 is a schematic diagram of a conventional antenna detachment.
Detailed Description
As shown in fig. 1 and 2, the invention utilizes the mature movable buckle device in the prior art to install the buckle 2 on the inner surface of the aircraft skin 1 and carry out the buckle type installation and disassembly of the aircraft antenna 3.
The buckle 2 is a rotatable movable buckle. And a card slot device corresponding to the buckle is arranged on the antenna.
The buckle 2 is an elastic metal buckle, can be screwed on the inner surface of the aircraft skin 1, and can also be welded.
Claims (6)
1. A knockdown structure for an aircraft antenna, comprising:
and a buckle (2) is arranged on the inner surface of the aircraft skin (1) to carry out buckle type installation and disassembly on the aircraft antenna (3).
2. A detachable structure for an aircraft antenna according to claim 1, characterised in that said clasp (2) is a movable clasp that can rotate.
3. A demountable structure for an aircraft antenna according to claim 1, wherein a slot means corresponding to the snap is mounted on the antenna.
4. A knockdown structure for an aircraft antenna according to claim 1, characterized in that said snap (2) is screwed onto the inner surface of the aircraft skin (1).
5. A knockdown structure for an aircraft antenna according to claim 1, characterized in that said clasp (2) is welded to the inner surface of the aircraft skin (1).
6. A knockdown structure for an aircraft antenna according to claim 1, characterized in that said clasp (2) is a resilient metal clasp.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922419254.8U CN210897591U (en) | 2019-12-27 | 2019-12-27 | Detachable structure for aircraft antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922419254.8U CN210897591U (en) | 2019-12-27 | 2019-12-27 | Detachable structure for aircraft antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210897591U true CN210897591U (en) | 2020-06-30 |
Family
ID=71341074
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922419254.8U Active CN210897591U (en) | 2019-12-27 | 2019-12-27 | Detachable structure for aircraft antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210897591U (en) |
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2019
- 2019-12-27 CN CN201922419254.8U patent/CN210897591U/en active Active
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