CN206639909U - A kind of aircraft airborne antenna mounting seat - Google Patents
A kind of aircraft airborne antenna mounting seat Download PDFInfo
- Publication number
- CN206639909U CN206639909U CN201720242729.9U CN201720242729U CN206639909U CN 206639909 U CN206639909 U CN 206639909U CN 201720242729 U CN201720242729 U CN 201720242729U CN 206639909 U CN206639909 U CN 206639909U
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- China
- Prior art keywords
- aircraft
- supporting plate
- antenna
- bearing
- stringer
- 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.)
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Abstract
The utility model discloses a kind of aircraft airborne antenna mounting seat, including aircraft skin, first bearing, second bearing, first aircraft stringer, second aircraft stringer, rivet, first supporting plate, second supporting plate, fixing screws, cable connector, antenna, sealant, it is fixedly connected between first bearing and the first aircraft stringer by rivet, pass through rivet interlacement between second bearing and the second aircraft stringer, sealed between second supporting plate surface and bottom surface of antenna by sealing and paste connection, the fixing screws are through antenna and both the first supporting plate are fixed together and the cavity where fixing screws is tightly connected by sealant, also it is fixedly connected between first supporting plate and antenna by plate nut and is coated with sealing between the first supporting plate and antenna.This aircraft is arranged in aircraft stringer with airborne antenna mounting seat antenna pedestal, fixed to utilize former riveting by machine nail position as far as possible, reduces influence of the installation to aircraft surfaces aerodynamic configuration.
Description
Technical field
It the utility model is related to a kind of aircraft airborne antenna mounting seat.
Background technology
Aircraft antenna is often arranged on antenna pedestal, but the pneumatic outer of aircraft is sometimes influenced whether after antenna pedestal installation
Shape, thus improve a kind of aircraft airborne antenna mounting seat reduce that influence of the installation to aircraft surfaces aerodynamic configuration become can
OK.
Utility model content
The purpose of this utility model is to provide a kind of aircraft airborne antenna mounting seat, to solve above-mentioned background technology
The problem of middle proposition.
To achieve the above object, the utility model provides following technical scheme：A kind of aircraft airborne antenna mounting seat,
Including aircraft skin, the first bearing, the second bearing, the first aircraft stringer, the second aircraft stringer, rivet, the first supporting plate, the second support
Plate, fixing screws, cable connector, antenna, sealant, fixed between first bearing and the first aircraft stringer by rivet
Connection, by rivet interlacement between second bearing and the second aircraft stringer, integrally connects between the first bearing and the first supporting plate
Connect, integrally connected between the second bearing and the second supporting plate, sealed and pasted by sealing between the second supporting plate surface and bottom surface of antenna
Connection, the fixing screws are through antenna and both the first supporting plate are fixed together and the cavity where fixing screws passes through
Sealant is tightly connected, be also fixedly connected between the first supporting plate and antenna by plate nut and the first supporting plate and antenna it
Between be coated with sealing, the cable connector is nested in aircraft skin.
Preferably, the aircraft skin perforate is live perforate.
Preferably, first bearing, the second bearing, the first supporting plate and the second supporting plate use extra super duralumin alloy 7075-
T6 materials are made and precision is ensured by numerical control frame.
Compared with prior art, the beneficial effects of the utility model are：This aircraft antenna seat profile is smaller, is ensureing
The aerodynamic configuration of aircraft is not influenceed on the premise of installation reliability；Antenna seating face has carried out protective treatment；Antenna pedestal is arranged on
It is fixed to utilize former riveting by machine nail position as far as possible in aircraft stringer, reduce influence of the installation to aircraft surfaces aerodynamic configuration.
Brief description of the drawings
Fig. 1 is the utility model scheme of installation.
Fig. 2 is the utility model structure diagram.
In figure：1- aircraft skins, 2- antennas, the bearings of 3- first, the bearings of 4- second, 5- rivets, the supporting plates of 6- first, 7- second
Supporting plate, the aircraft stringers of 8- first, the aircraft stringers of 9- second, 10- cable connectors, 11- fixing screws, 12- sealants.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Refer to Fig. 1-2, a kind of embodiment provided by the utility model：A kind of aircraft airborne antenna mounting seat, bag
Include aircraft skin 1, the first bearing 3, the second bearing 4, the first aircraft stringer 8, the second aircraft stringer 9, rivet 5, the first supporting plate 6,
Second supporting plate 7, fixing screws 11, cable connector 10, antenna 2, sealant 12, the aircraft stringer 8 of the first bearing 3 and first
Between be fixedly connected by rivet 5, connected between the aircraft stringer 9 of the second bearing 4 and second by rivet 5, the first bearing 3
The integrally connected between the first supporting plate 6, integrally connected between the second bearing 4 and the second supporting plate 7, the surface of the second supporting plate 7 and antenna 2
Sealed between bottom surface by sealing and paste connection, both are fixed on one by the fixing screws 11 through the supporting plate 6 of antenna 2 and first
Rise and the cavity where fixing screws 11 is tightly connected by sealant 12, also pass through support between the first supporting plate 6 and antenna 2
Crab bolt is fixedly connected and sealing is coated between the first supporting plate 6 and antenna 2, and the cable connector 10 is nested in aircraft skin
In 1, the perforate of aircraft skin 1 is live perforate, and the first bearing 3, the second bearing 4, the first supporting plate 6 and the second supporting plate 7 use
Extra super duralumin alloy 7075-T6 materials are made and precision is ensured by numerical control frame.
Specifically used mode：In the utility model, pass through aircraft skin 1, the first bearing 3, the second bearing 4, the first aircraft
It is stringer 8, the second aircraft stringer 9, rivet 5, the first supporting plate 6, the second supporting plate 7, fixing screws 11, cable connector 10, antenna 2, close
Envelope putty 12 constitutes the present apparatus, and the first bearing 3, the second bearing 4, the first supporting plate 6 and the second supporting plate 7 are extra super duralumin alloy
7075-T6, precision are ensured by numerical control frame, wherein the first bearing 3 and the corner angle of the second bearing 4 fall blunt and remove flash removed, the
One bearing 3, the second bearing 4, the first supporting plate 6 and the second supporting plate 7 and aircraft skin joint place profile and skin shape syntype at this,
Antenna mounting technique index meets HB6088 relevant regulations, after surface uses yellow anodization, sprays epoxy zinc chromate primer, appearance
Face sprays the unglazed white paint of epoxy nitro.Antenna mounting technique is that directional aerial plane left-right deviation does not allow more than 5 ゜；Orient day
Line installs optical axis angle and the angle of axis does not allow more than 1 ゜；Directional aerial mounting plane is not to be exceeded+2 with horizontal plane angle
The ゜ of ゜~5；Some other shelter of directional aerial Edge Distance and discontinuous plan have to be larger than 46cm；It is special apart from other antennas
It is not that the higher antenna of profile and L-band transponder aerial should be greater than 80cm；Antenna mounting locations are at the top of aircraft
It is forward.The distance of the second bearing of distance 4 of first bearing 3 is 300mm, and the length of the first bearing 3 and the second bearing 4 is 310mm.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (3)
1. a kind of aircraft airborne antenna mounting seat, including aircraft skin (1), the first bearing (3), the second bearing (4), first
Aircraft stringer (8), the second aircraft stringer (9), rivet (5), the first supporting plate (6), the second supporting plate (7), fixing screws (11), cable
Joint (10), antenna (2), sealant (12), it is characterised in that：Between first bearing (3) and the first aircraft stringer (8)
It is fixedly connected, is connected between second bearing (4) and the second aircraft stringer (9) by rivet (5), first by rivet (5)
Integrally connected between bearing (3) and the first supporting plate (6), integrally connected between the second bearing (4) and the second supporting plate (7), the second support
Sealed between plate (7) surface and antenna (2) bottom surface by sealing and paste connection, the fixing screws (11) through antenna (2) and
Both are fixed together by the first supporting plate (6) and the cavity where fixing screws (11) is sealed by sealant (12) and connected
Connect, be also fixedly connected and between the first supporting plate (6) and antenna (2) by plate nut between the first supporting plate (6) and antenna (2)
Sealing is coated with, the cable connector (10) is nested in aircraft skin (1).
A kind of 2. aircraft airborne antenna mounting seat according to claim 1, it is characterised in that the aircraft skin
(1) perforate is live perforate.
A kind of 3. aircraft airborne antenna mounting seat according to claim 1, it is characterised in that first bearing
(3), the second bearing (4), the first supporting plate (6) and the second supporting plate (7) are made simultaneously using extra super duralumin alloy 7075-T6 materials
And precision is ensured by numerical control frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720242729.9U CN206639909U (en) | 2017-03-14 | 2017-03-14 | A kind of aircraft airborne antenna mounting seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720242729.9U CN206639909U (en) | 2017-03-14 | 2017-03-14 | A kind of aircraft airborne antenna mounting seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206639909U true CN206639909U (en) | 2017-11-14 |
Family
ID=60249127
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720242729.9U Active CN206639909U (en) | 2017-03-14 | 2017-03-14 | A kind of aircraft airborne antenna mounting seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206639909U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639309A (en) * | 2018-07-16 | 2018-10-12 | 中国人民解放军海军航空大学青岛校区 | A kind of aircraft airborne antenna mounting seat |
-
2017
- 2017-03-14 CN CN201720242729.9U patent/CN206639909U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639309A (en) * | 2018-07-16 | 2018-10-12 | 中国人民解放军海军航空大学青岛校区 | A kind of aircraft airborne antenna mounting seat |
| CN108639309B (en) * | 2018-07-16 | 2024-01-23 | 中国人民解放军海军航空大学青岛校区 | Airborne antenna mounting base for airplane |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |