CN109319090A - A kind of installation method of embedded conformal antenna cover - Google Patents
A kind of installation method of embedded conformal antenna cover Download PDFInfo
- Publication number
- CN109319090A CN109319090A CN201811190605.6A CN201811190605A CN109319090A CN 109319090 A CN109319090 A CN 109319090A CN 201811190605 A CN201811190605 A CN 201811190605A CN 109319090 A CN109319090 A CN 109319090A
- Authority
- CN
- China
- Prior art keywords
- antenna house
- mouth frame
- antenna
- structure mouth
- supporting element
- 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.)
- Granted
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Details Of Aerials (AREA)
- Support Of Aerials (AREA)
Abstract
The invention belongs to aero-manufacturing technology fields, it is related to a kind of installation method of embedded conformal antenna cover, the manufacturing technology state that the present invention passes through control antenna house and body mouth frame, select technological equipment appropriate, plan reasonable flow of installation, in the way of technological compensa tion, the accuracy of manufacture requirement to antenna house and body mouth frame is reduced, ensure that the installation of embedded conformal antenna cover meets detail of design requirement.
Description
Technical field
The invention belongs to aero-manufacturing technology fields, and in particular to a kind of mounting technique of embedded conformal antenna cover.
Background technique
Antenna house is a kind of special component on aircraft, according to equipment performance and the difference of installation position, structure shape
Formula and shape are had nothing in common with each other.Antenna house is usually made of composite material, is not only needed to meet equipment electric property requirement, be also needed to meet
Pneumatic force request.
The existing mounting technique of antenna house is: antenna house is installed with complete finished product state and body, i.e., antenna house binding face,
Edge is net side state, and connecting hole is all produced；Body connecting hole, assembling connecting piece are prepared by the connecting hole on antenna house；It is complete
At the installation of antenna house.Its advantage is that: antenna house state is complete, without carrying out secondary operation when being installed with body, assembly quickly,
It is high-efficient；The disadvantage is that: it is required that antenna house, body accuracy of manufacture height, harmony are good, meet binding face, connecting hole assembly demand.
The method is suitable for body appearance bridging type antenna house.For embedding bridging type antenna house, antenna is not only considered
The compactness of cover and body faying surface also needs consideration to require with housing construction border clearance fit, shape (conformal) deviation requirement,
Existing method is not able to satisfy installation requirement.
Summary of the invention
The purpose of the present invention is: airframe two sides need to install embedded conformal antenna cover, to realize conformal design and set
Meter requires.It is required that solving the technical problem in the installation of embedded conformal antenna cover: 1. antenna house and body fitting surface are bonded
Problem；2. antenna house and body border fit clearance problem；3. antenna house and body shape deviation problem；4. antenna house and body
Resetting problem.
The technical scheme is that providing a kind of installation method of embedded conformal antenna cover, include the following steps:
Step 1: interior shape supporting element is fixed on the machine body, the interior shape supporting element is for right during according to adjustment
Antenna house conformal support；Antenna house is buckled on interior shape supporting element by lifting, so that the antenna on antenna house periphery and body
The structure mouth frame in region is corresponding；
Step 2: backfit is carried out to antenna house periphery and structure mouth frame, so that between antenna house and the cooperation of structure mouth frame border
Gap, binding face gap and shape scale meet installation requirement；
Step 3: drilling antenna house location hole on antenna house and position admittedly relative to structure mouth frame by antenna house
Tightly, then the connecting hole that antenna house is mutually fixedly connected with structure mouth frame is drilled；
Step 4: antenna house is hung body, fastener is installed in structure mouth frame；
Step 5: antenna house is mounted in structure mouth frame after coating sealant in structure mouth frame；
Step 6: disassembly antenna house, and to sealant shaping；
Step 7: interior shape supporting element of dismantling, antenna house is mounted in structure mouth frame, and coat waterproof coating.
Further, also antenna house is fastened on interior shape supporting element by tensing bandage into step 3 in step 1.
Beneficial effects of the present invention
The present invention selects technological equipment appropriate by the manufacturing technology state of control antenna house and body mouth frame, plans
Reasonable flow of installation is reduced and is wanted to the accuracy of manufacture of antenna house and body mouth frame in the way of technological compensa tion
It asks, ensure that the installation of embedded conformal antenna cover meets detail of design requirement.
Detailed description of the invention
Fig. 1 is schematic diagram of the invention；
Fig. 2 is the schematic diagram of the prior art；
Wherein: the embedded conformal antenna cover of 1-, 2- antenna mounting surface, 3 bodies, 4 aircraft horizontal tectonics faces, 5 aircrafts are symmetrical
Shape supporting element, 7 tense bandage in median plane, 6-.
Specific embodiment
The present invention is described in further details below.Referring to Fig. 1 and 2, a kind of peace of embedded conformal antenna cover is provided
Dress method, includes the following steps:
Step 1: interior shape supporting element is fixed on the machine body, the interior shape supporting element is for right during according to adjustment
Antenna house conformal support；Antenna house is buckled on interior shape supporting element by lifting, so that the antenna on antenna house periphery and body
The structure mouth frame in region is corresponding；
Step 2: backfit is carried out to antenna house periphery and structure mouth frame, so that between antenna house and the cooperation of structure mouth frame border
Gap, binding face gap and shape scale meet installation requirement；
Step 3: drilling antenna house location hole on antenna house and position admittedly relative to structure mouth frame by antenna house
Tightly, then the connecting hole that antenna house is mutually fixedly connected with structure mouth frame is drilled；
Step 4: antenna house is hung body, fastener is installed in structure mouth frame；
Step 5: antenna house is mounted in structure mouth frame after coating sealant in structure mouth frame；
Step 6: disassembly antenna house, and to sealant shaping；
Step 7: interior shape supporting element of dismantling, antenna house is mounted in structure mouth frame, and coat waterproof coating.
Further, also antenna house is fastened on interior shape supporting element by tensing bandage into step 3 in step 1.
Claims (2)
1. a kind of installation method of embedded conformal antenna cover, includes the following steps:
Step 1: interior shape supporting element is fixed on the machine body, the interior shape supporting element is used for during according to adjustment to antenna
Cover conformal support；Antenna house is buckled on interior shape supporting element by lifting, so that the antenna area on antenna house periphery and body
Structure mouth frame it is corresponding；
Step 2: backfit is carried out to antenna house periphery and structure mouth frame, so that antenna house and structure mouth frame border fit clearance, patch
Conjunction face gap and shape scale meet installation requirement；
Step 3: drill antenna house location hole on antenna house and antenna house is subjected to positioning and fastening relative to structure mouth frame, then
Drill the connecting hole that antenna house is mutually fixedly connected with structure mouth frame；
Step 4: antenna house is hung body, fastener is installed in structure mouth frame；
Step 5: antenna house is mounted in structure mouth frame after coating sealant in structure mouth frame；
Step 6: disassembly antenna house, and to sealant shaping；
Step 7: interior shape supporting element of dismantling, antenna house is mounted in structure mouth frame, and coat waterproof coating.
2. a kind of installation method of embedded conformal antenna cover as described in claim 1, it is characterised in that: in step 1 to step
Also antenna house is fastened on interior shape supporting element by tensing bandage in rapid three.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811190605.6A CN109319090B (en) | 2018-10-12 | 2018-10-12 | Installation method of embedded conformal antenna cover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811190605.6A CN109319090B (en) | 2018-10-12 | 2018-10-12 | Installation method of embedded conformal antenna cover |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109319090A true CN109319090A (en) | 2019-02-12 |
| CN109319090B CN109319090B (en) | 2022-06-28 |
Family
ID=65261438
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811190605.6A Active CN109319090B (en) | 2018-10-12 | 2018-10-12 | Installation method of embedded conformal antenna cover |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109319090B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111029770A (en) * | 2019-12-26 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Bearable sandwich structure of vertical antenna array |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102237571A (en) * | 2010-04-09 | 2011-11-09 | 古野电气株式会社 | Radome, antenna device and radar apparatus |
| CN105415710A (en) * | 2015-11-03 | 2016-03-23 | 上海无线电设备研究所 | Antenna housing structure and forming method and die thereof |
| CN106976248A (en) * | 2017-01-12 | 2017-07-25 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | Embedded type composite material conformal antenna cover |
| CN107046173A (en) * | 2017-04-20 | 2017-08-15 | 哈尔滨哈玻拓普复合材料有限公司 | A kind of composite pressure-resistance structure RECTIFYING ANTENNA cover and its manufacture method |
| CN107380401A (en) * | 2016-04-29 | 2017-11-24 | 埃姆普里萨有限公司 | It is used in particular for aircraft antenna dome being attached to the quick connection assembly of housing construction |
-
2018
- 2018-10-12 CN CN201811190605.6A patent/CN109319090B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102237571A (en) * | 2010-04-09 | 2011-11-09 | 古野电气株式会社 | Radome, antenna device and radar apparatus |
| CN105415710A (en) * | 2015-11-03 | 2016-03-23 | 上海无线电设备研究所 | Antenna housing structure and forming method and die thereof |
| CN107380401A (en) * | 2016-04-29 | 2017-11-24 | 埃姆普里萨有限公司 | It is used in particular for aircraft antenna dome being attached to the quick connection assembly of housing construction |
| CN106976248A (en) * | 2017-01-12 | 2017-07-25 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | Embedded type composite material conformal antenna cover |
| CN107046173A (en) * | 2017-04-20 | 2017-08-15 | 哈尔滨哈玻拓普复合材料有限公司 | A kind of composite pressure-resistance structure RECTIFYING ANTENNA cover and its manufacture method |
Non-Patent Citations (1)
| Title |
|---|
| 周槿: "雷达天线罩装配工艺设计概述", 《电子机械工程》 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111029770A (en) * | 2019-12-26 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Bearable sandwich structure of vertical antenna array |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109319090B (en) | 2022-06-28 |
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