CN214227117U - Airborne antenna array double-layer outer mounting frame with host - Google Patents
Airborne antenna array double-layer outer mounting frame with host Download PDFInfo
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- CN214227117U CN214227117U CN202022585477.4U CN202022585477U CN214227117U CN 214227117 U CN214227117 U CN 214227117U CN 202022585477 U CN202022585477 U CN 202022585477U CN 214227117 U CN214227117 U CN 214227117U
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- host computer
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- fixing bolt
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Abstract
The utility model discloses an airborne antenna array double-deck outer mounting bracket who contains host computer, including the aircraft fuselage, install first mounting on the aircraft fuselage, connect the dead lever on the first mounting, the second mounting is connected to the lower extreme of dead lever, and the second mounting is installed on equipment host computer surface, installs the host board under the equipment host computer, and third mounting and fixing bolt are installed respectively at the both ends of host board, connect antenna boom under the fixing bolt, install the antenna module under the antenna boom. This double-deck outer mounting bracket of airborne antenna array who contains host computer, install on the mainboard by first mounting, dead lever, second mounting and third mounting on the aircraft fuselage, mainboard and dead lever and first mounting and third mounting form triangle stable structure, realize fixed mainboard, by fixing bolt connection on antenna boom on the mainboard, install the antenna module of being no less than one on the antenna boom, form the antenna array, reach easy dismounting, it is fixed firm, support reliable effect.
Description
Technical Field
The utility model relates to a mounting bracket technical field specifically is an airborne antenna array double-deck outer mounting bracket who contains host computer.
Background
The antenna is a converter, the guided wave that propagates on the transmission line becomes the electromagnetic wave that propagates in the unbounded medium, or carry out the opposite transform, be used for launching or receiving the part of electromagnetic wave in radio equipment, airborne antenna mounting bracket is the device that supports antenna structure and make the antenna move in stipulated airspace, make the antenna move according to predetermined law through antenna control system, or follow the target motion, when military aircraft carries out special task, because need install airborne antenna additional temporarily in aircraft fuselage side, the influence of position height and flight angle often leads to the holding power not enough during flight simultaneously, the subassembly is firm inadequately, the dismouting is also inconvenient, easily take place the collision damage, to these defects, thereby design an airborne antenna array bilayer outer mounting bracket that contains the host computer.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a machine that contains host computer carries double-deck outer mounting bracket of antenna array has easy dismounting, and is fixed firm, supports reliable advantage, has solved the problem among the prior art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an airborne antenna array double-deck outer mounting bracket that contains host computer, includes the aircraft fuselage, install first mounting on the aircraft fuselage, be connected with the dead lever on the first mounting, the lower extreme of dead lever is connected with the second mounting, the second mounting is installed on equipment host computer surface, installs the mainboard under the equipment host computer, third mounting and fixing bolt are installed respectively to the both ends of mainboard, the equal symmetry of third mounting and fixing bolt sets up on the mainboard, be connected with antenna boom under the fixing bolt, install the antenna assembly of being no less than one under the antenna boom.
Preferably, the main board and the antenna bracket are provided with lightening holes.
Preferably, one end of the fixing bolt is fixed on the mainboard through a nut, and the other end of the fixing bolt is fixed on the antenna bracket through a nut.
Preferably, the antenna assembly passes through the antenna bracket and is fixed on the antenna bracket.
Preferably, the antenna support is in the shape of a long-strip groove.
Compared with the prior art, the beneficial effects of the utility model are as follows:
this double-deck outer mounting bracket of airborne antenna array that contains host computer, through first mounting on the aircraft fuselage, the dead lever, second mounting and third mounting are installed on the mainboard, dead lever fixedly connected with second mounting, enough rigidity has, mainboard and dead lever and original first mounting and third mounting form the triangle stable structure on the aircraft, realize the fixed of mainboard jointly, install the equipment host computer on the mainboard, through fixing bolt fixed connection on antenna boom on the mainboard, antenna boom is rectangular recess form, mainboard and antenna boom are for realizing subtracting the weight, all can be equipped with lightening hole, install the antenna module of being no less than one on the antenna boom, form the antenna array, constitute the mounting bracket at last, thereby reach easy dismounting, it is fixed firm, support reliable effect.
Drawings
Fig. 1 is a front view of the present invention;
fig. 2 is a side view of the present invention;
fig. 3 is a top view of the present invention;
fig. 4 is a schematic diagram of the present invention.
In the figure: 1. an aircraft fuselage; 2. a first fixing member; 3. fixing the rod; 4. a second fixing member; 5. a device host; 6. a main board; 7. a third fixing member; 8. fixing the bolt; 9. an antenna mount; 10. an antenna assembly.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, a dual-layer external mounting frame for an airborne antenna array including a main frame, which includes an aircraft body 1, which is an important component of an aircraft and mainly functions to fix wings, a tail wing, and a landing gear to form an integral body, a first fixing member 2 is installed on the aircraft body 1, a fixing rod 3 is connected to the first fixing member 2, the fixing rod 3 has sufficient rigidity, a second fixing member 4 is connected to the lower end of the fixing rod 3, the second fixing member 4 is installed on the surface of an equipment main frame 5, a main board 6 is installed below the equipment main frame 5 and can be processed to reduce weight holes to achieve the effect of reducing weight, a third fixing member 7 and a fixing bolt 8 are respectively installed at two ends of the main board 6, the main board 6 and the fixing rod 3 and the original first fixing member 2 and third fixing member 7 on the aircraft form a triangular stable structure to jointly realize the fixing of the main board 6, the third fixing member 7 and the fixing bolt 8 are symmetrically installed on the main board 6, fixing bolt 8 is by hexagonal head and ring flange and screw rod two parts one kind of fastener of constituteing, need with the nut cooperation, a part for the fastening connection two have the through-hole, play the fixed action, be connected with antenna boom 9 under fixing bolt 8, antenna boom 9 is rectangular recess form, fixing bolt 8's one end is passed through the nut and is fixed on mainboard 6, fixing bolt 8's the other end passes through the nut and fixes on antenna boom 9, be equipped with the lightening hole for losing weight on the antenna boom 9, install antenna module 10 no less than one under the antenna boom 9, can install a plurality of antenna modules 10, form the antenna array, antenna module 10 passes antenna boom 9 and fixes on antenna boom 9.
The working principle is as follows: install aircraft fuselage 1 on host board 6 through first mounting 2, dead lever 3, second mounting 4 and third mounting 7, host board 6 passes through fixing bolt 8 fixed connection on antenna boom 9, installs the antenna module 10 that is no less than one on antenna boom 9, forms the antenna array, constitutes the mounting bracket at last.
In summary, the following steps: the airborne antenna array double-layer external mounting frame comprises a main frame, wherein an aircraft body 1 is arranged on a main board 6 through a first fixing piece 2, a fixed rod 3, a second fixing piece 4 and a third fixing piece 7, the fixed rod 3 is fixedly connected with the second fixing piece 4 and has enough rigidity, the main board 6, the fixed rod 3 and the original first fixing piece 2 and the original third fixing piece 7 on the aircraft form a triangular stable structure to jointly realize the fixing of the main board 6, an equipment main frame 5 is arranged on the main board 6, the main board 6 is fixedly connected on an antenna bracket 9 through a fixed bolt 8, the antenna bracket 9 is in a strip groove shape, the main board 6 and the antenna bracket 9 can be provided with lightening holes for lightening, at least one antenna assembly 10 is arranged on the antenna bracket 9 to form an antenna array, and finally the mounting frame is formed, so that the purposes of convenient assembly and disassembly and firm fixing are achieved, and the effect of reliable support.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an airborne antenna array double-deck outer mounting bracket that contains host computer, including aircraft fuselage (1), a serial communication port, install first mounting (2) on aircraft fuselage (1), be connected with dead lever (3) on first mounting (2), the lower extreme of dead lever (3) is connected with second mounting (4), install on equipment host computer (5) surface second mounting (4), install mainboard (6) under equipment host computer (5), third mounting (7) and fixing bolt (8) are installed respectively to the both ends of mainboard (6), third mounting (7) and fixing bolt (8) equal symmetry set up on mainboard (6), be connected with antenna boom (9) under fixing bolt (8), install antenna assembly (10) that are no less than one under antenna boom (9).
2. The double-layer external mounting frame for the airborne antenna array comprising the host computer according to claim 1, wherein the host board (6) and the antenna support (9) are provided with lightening holes.
3. The double-layer external mounting frame for the airborne antenna array comprising the host computer according to claim 1, wherein one end of the fixing bolt (8) is fixed on the host board (6) through a nut, and the other end of the fixing bolt (8) is fixed on the antenna bracket (9) through a nut.
4. A dual-layer external mount for an airborne antenna array including a host machine according to claim 1 wherein the antenna assembly (10) passes through the antenna mount (9) and is secured to the antenna mount (9).
5. The double-layer outer mount for an airborne antenna array including a main unit according to claim 1, wherein the antenna support (9) is in the form of a strip groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022585477.4U CN214227117U (en) | 2020-11-10 | 2020-11-10 | Airborne antenna array double-layer outer mounting frame with host |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022585477.4U CN214227117U (en) | 2020-11-10 | 2020-11-10 | Airborne antenna array double-layer outer mounting frame with host |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214227117U true CN214227117U (en) | 2021-09-17 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022585477.4U Active CN214227117U (en) | 2020-11-10 | 2020-11-10 | Airborne antenna array double-layer outer mounting frame with host |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214227117U (en) |
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2020
- 2020-11-10 CN CN202022585477.4U patent/CN214227117U/en active Active
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