CN205873767U - Aircraft ventral antenna house installation car - Google Patents
Aircraft ventral antenna house installation car Download PDFInfo
- Publication number
- CN205873767U CN205873767U CN201620741297.1U CN201620741297U CN205873767U CN 205873767 U CN205873767 U CN 205873767U CN 201620741297 U CN201620741297 U CN 201620741297U CN 205873767 U CN205873767 U CN 205873767U
- Authority
- CN
- China
- Prior art keywords
- antenna house
- vehicle frame
- frame
- longeron
- support post
- 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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Links
- 238000009434 installation Methods 0.000 title abstract description 6
- 210000001015 abdomen Anatomy 0.000 claims description 17
- 229910000831 Steel Inorganic materials 0.000 claims description 8
- 239000010959 steel Substances 0.000 claims description 8
- 238000004804 winding Methods 0.000 abstract 1
- 238000010276 construction Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 239000013536 elastomeric material Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
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- Support Of Aerials (AREA)
Abstract
The utility model discloses an aircraft ventral antenna house installation car, the frame that includes the rectangular frame structure constituteed by crossbeam and longeron with span a set of antenna house bracket on the frame is provided with a set of support post in pairs on the longeron of frame both sides, the support post with the connecting seat one -to -one at antenna house bracket both ends, support post top are provided with the fixed pulley, have set firmly the movable pulley on the antenna house bracket connection seat, and the frame is provided with the leading wheel all around, from fixing many wire rope that draw forth on the winding device on the frame pass through in proper order around fixed pulley and its below behind the leading wheel the movable pulley forms a plurality of laborsaving assembly pulleys, the activity is provided with quick -release pin between antenna house bracket connection seat and the solebar. The utility model discloses simple structure is convenient for make, uses high -efficient, convenience, can satisfy installation, dismantlement, the short -distance transport of aircraft ventral antenna house and the function of placing, various, the safe and reliable of function.
Description
Technical field
This utility model relates to aircraft suspension member loading equipments technical field, especially relates to a kind of aircraft belly antenna cover peace
Entrucking.
Background technology
Owing to aircraft belly antenna enclosure volume is relatively big, and aircraft bottom space is narrow and small, hanging point is relatively low, therefore existing in use
Ground handling equipment when mounting, it is impossible to meet and use requirement.When employing manually mounts, efficiency is low, reliability is the highest.
Summary of the invention
This utility model provides a kind of aircraft belly antenna cover to install car, it is therefore intended that solve existing ground handling equipment without
The problem that method mounts aircraft belly antenna cover.
For achieving the above object, this utility model can take following technical proposals:
Car installed by aircraft belly antenna cover described in the utility model, including the rectangular frame knot being made up of crossbeam and longeron
The vehicle frame of structure and across one group of antenna house bracket on described vehicle frame, vehicle frame two side girder has been arranged in pairs one group and has supported vertical
The connection seat one_to_one corresponding at post, described support post and described antenna house bracket two ends, support post top is provided with fixed pulley,
Being installed with movable pulley in antenna house carrier connecting base, vehicle frame surrounding is provided with directive wheel, from the coiling being fixed on described vehicle frame
The a plurality of steel wire rope drawn on device is formed multiple around fixed pulley and described movable pulley below successively after described directive wheel
Laborsaving assembly pulley；It is movably set with Quick-release pin between described antenna house carrier connecting base and longitudinal beam.
Described frame cross and antenna house carrier connecting base surface configuration have buffer protection layer.
It is provided with stretching structure on described longitudinal beam.
Folding arm rest, workbox and hoisting ring it is provided with on described vehicle frame.
The aircraft belly antenna cover that this utility model provides installs car, simple in construction, it is simple to manufacture, and it is efficient, convenient to use,
Disclosure satisfy that the function of the installation of aircraft belly antenna cover, dismounting, short-distance transport and placement, diverse in function, safe and reliable.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the enlarged drawing in A portion in Fig. 1.
Fig. 3 is the enlarged drawing in B portion in Fig. 1.
Fig. 4 is the enlarged drawing in C portion in Fig. 1.
Fig. 5 is the structural representation of antenna house bracket in Fig. 1.
Fig. 6 is the enlarged drawing in D portion in Fig. 5.
Fig. 7 is the structural representation of folding arm rest in Fig. 1.
Detailed description of the invention
As shown in figs. 1-7, car installed by aircraft belly antenna cover described in the utility model, forms including by crossbeam and longeron
Rectangular frame structure vehicle frame 1 and across two antenna house brackets 2 on vehicle frame 1.Car body short distance transition for convenience
Transport, is provided with stretching structure on longeron.In the present embodiment, vehicle frame 1 longeron is accessed trocar sheath two ends by trocar sheath and set
Front longitudinal and floor side member composition, it is possible to use other common form.At forward and backward longeron, road wheel is installed.
The forward and backward longeron of vehicle frame 1 is respectively fixed with a pair support post 3, support post 3 and antenna house bracket 2 two ends
Connection seat 201 one_to_one corresponding, support post 3 top is installed with fixed pulley 301, and antenna house bracket 2 connects and is installed with on seat 201
Movable pulley 202, vehicle frame 1 surrounding is provided with directive wheel 101, and four steel wire ropes 5 draw from the Winder 4 being fixed on vehicle frame 1
Go out, and drawn location by the directive wheel 101 on vehicle frame 1 housing, when causing at first support post 3, just choose a steel
The cord 5 fixed pulley 301 at this and movable pulley below 202 form a laborsaving assembly pulley, remaining steel wire rope 5 continue by
Directive wheel 101 draws, and is coiled into three laborsaving assembly pulleys to its excess-three respectively.
Above-mentioned Winder 4, therefore can be hand by folding as it is shown on figure 3, because aircraft belly antenna cover lighter in weight
Handle 401, manually by steel wire rope 5 rolling or unreel, so that the movable pulley 202 being connected with steel wire rope 5 rises or falls, reaches to make
The purpose of antenna house bracket 2 lifting.Also offer on the relevant position of vehicle frame 1 longeron additionally, antenna house bracket 2 connects seat 201
There is through hole, be fitted with Quick-release pin 6 in through-holes, when making vehicle move, connect seat 201 and be fixed together with vehicle frame 1 longeron.
In order to avoid, during transport, mounting, aircraft belly antenna cover collides make with vehicle frame 1, antenna house bracket 2
Become surface damage, be all stained with the buffer protection layer of elastomeric material at vehicle frame 1 crossbeam inner surface and connection seat 201 upper surface.
For the ease of push-and-pull car body, longeron trocar sheath is provided with folding arm rest 7 as shown in Figure 7.This is collapsible
Handrail 7 includes the bearing 701 being welded on longeron trocar sheath, and its upper end offers 3 through holes, the Quick-release pin passed in through hole
Crank handrail 703 is fixed on bearing 701 by 702, and realizes folder function by changing connection orientation.It is welded at vehicle frame 1
Workbox 8 on floor side member, the connector etc. disassembled during for placing Quick-release pin, spanner and installing car transhipment.Forward and backward
It is fixed with hoisting ring 9 also by standard connector, for carrying out vehicle lifting when transition is transported on longeron.
When using this utility model carrier belly antenna cover, movable bracket 2 is in extreme lower position, uses Quick-release pin 6
It is connected fixing with vehicle frame 1 longeron.When arriving appointment position installation antenna house, shake folding hand rocking handle 401 makes steel wire rope 5 receive
Volume, thus pull up a liter antenna house bracket 2.After antenna house installation, shake folding hand rocking handle 401 makes antenna house bracket 2 multiple
Position.
This utility model simple in construction, it is simple to manufacture, easy to use, safe and reliable, it is not necessary to electronic, hydraulic test, manually
Can realize placing, moving, dismount the function of aircraft belly antenna cover.
Claims (4)
1. car installed by an aircraft belly antenna cover, it is characterised in that: include the rectangular frame structure being made up of crossbeam and longeron
Vehicle frame (1) and across one group of antenna house bracket (2) on described vehicle frame (1), vehicle frame (1) two side girder has been arranged in pairs
Connection seat (201) one_to_one corresponding at one group of support post (3), described support post (3) and described antenna house bracket (2) two ends,
Support post (3) top is provided with fixed pulley (301), and antenna house bracket (2) connection seat (201) is installed with movable pulley (202),
Vehicle frame (1) surrounding is provided with directive wheel (101), from the upper a plurality of steel drawn of the Winder (4) being fixed on described vehicle frame (1)
Cord (5) is formed multiple around fixed pulley (301) and described movable pulley (202) below successively after described directive wheel (101)
Laborsaving assembly pulley；It is movably set with Quick-release pin (6) between described antenna house bracket (2) connection seat (201) and vehicle frame (1) longeron.
Car installed by aircraft belly antenna cover the most according to claim 1, it is characterised in that: described vehicle frame (1) crossbeam and sky
Irdome bracket (2) connects seat (201) surface configuration buffer protection layer.
Car installed by aircraft belly antenna cover the most according to claim 1 and 2, it is characterised in that: on described vehicle frame (1) longeron
It is provided with stretching structure.
Car installed by aircraft belly antenna cover the most according to claim 3, it is characterised in that: described vehicle frame is provided with on (1)
Folding arm rest (7), workbox (8) and hoisting ring (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620741297.1U CN205873767U (en) | 2016-07-15 | 2016-07-15 | Aircraft ventral antenna house installation car |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620741297.1U CN205873767U (en) | 2016-07-15 | 2016-07-15 | Aircraft ventral antenna house installation car |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205873767U true CN205873767U (en) | 2017-01-11 |
Family
ID=57694763
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620741297.1U Active CN205873767U (en) | 2016-07-15 | 2016-07-15 | Aircraft ventral antenna house installation car |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205873767U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271688A (en) * | 2019-05-17 | 2019-09-24 | 陕西飞机工业（集团）有限公司 | A kind of transporter large-scale antenna dome installation posture adjustment equipment |
-
2016
- 2016-07-15 CN CN201620741297.1U patent/CN205873767U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271688A (en) * | 2019-05-17 | 2019-09-24 | 陕西飞机工业（集团）有限公司 | A kind of transporter large-scale antenna dome installation posture adjustment equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 450005 mailbox 1084 in the middle section of South Third Ring Road, Zhengzhou City, Henan Province Co-patentee after: Zhengzhou Zhengfei Special Equipment Co.,Ltd. Patentee after: ZHENGZHOU AIRCRAFT EQUIPMENT Co.,Ltd. Address before: 450005 mailbox 1084 in the middle section of South Third Ring Road, Zhengzhou City, Henan Province Co-patentee before: AVIC ELECTRIC VEHICLES (ZHENGZHOU) CO.,LTD. Patentee before: ZHENGZHOU AIRCRAFT EQUIPMENT Co.,Ltd. |
|
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 451162 No. 20 Dongting Lake Road, Zhengzhou Airport District, Henan Province Co-patentee after: ZHENGZHOU AIRCRAFT EQUIPMENT Co.,Ltd. Patentee after: Zhengzhou Zhengfei Special Equipment Co.,Ltd. Address before: 450005 mailbox 1084 in the middle section of South Third Ring Road, Zhengzhou City, Henan Province Co-patentee before: Zhengzhou Zhengfei Special Equipment Co.,Ltd. Patentee before: ZHENGZHOU AIRCRAFT EQUIPMENT Co.,Ltd. |