CN206974290U - Guided missile changes the outfit docking facilities instrument - Google Patents
Guided missile changes the outfit docking facilities instrument Download PDFInfo
- Publication number
- CN206974290U CN206974290U CN201720677041.3U CN201720677041U CN206974290U CN 206974290 U CN206974290 U CN 206974290U CN 201720677041 U CN201720677041 U CN 201720677041U CN 206974290 U CN206974290 U CN 206974290U
- Authority
- CN
- China
- Prior art keywords
- moving jack
- jack horse
- guided missile
- platform
- outfit
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model discloses a kind of guided missile and changed the outfit docking facilities instrument, including organic frame, preceding Moving jack horse, lowering or hoisting gear, fixed rack and rear Moving jack horse；The frame has a platform, and the preceding Moving jack horse, lowering or hoisting gear, fixed rack and rear Moving jack horse are disposed side by side on platform successively.By the way that preceding Moving jack horse, lowering or hoisting gear, fixed rack and rear Moving jack horse are disposed side by side on platform successively, fixed rack is used for a bay section for fixing guided missile, preceding Moving jack horse and rear Moving jack horse fix other bay sections of guided missile, the lowering or hoisting gear is used for missile cabin support, rotation, lifting and locking, missile cabin is departed from or is placed on fixed rack, so that present apparatus instrument can be used for placing guided missile progress performance detection, it is easy to change the outfit simultaneously bay section before and after docking body, and convenient handling control flaps and aerofoil.
Description
Technical field
Docking facilities art is the utility model is related to, a kind of guided missile is referred in particular to and changes the outfit docking facilities instrument.
Background technology
Guided missile is placed on ammunition carrier when carrying out performance test, is both inconvenient to operate in energization detection performance, simultaneously
Also there is potential safety hazard.Thus pole needs a kind of special test table, places guided missile and carries out performance detection, while just
The bay section before and after the docking body that changes the outfit, and convenient handling control flaps and aerofoil.However, in the prior art, not this survey
Try workbench.
Utility model content
In view of this, in view of the existing deficiencies of the prior art, its main purpose is to provide a kind of guided missile and changed the utility model
Docking facilities instrument is filled, it, which can be used for placing guided missile, carries out performance detection, while bay section before and after docking body of being easy to change the outfit, Yi Jifang
Civilian dress unloads control flaps and aerofoil.
To achieve the above object, the utility model is using following technical scheme：
A kind of guided missile changes the outfit docking facilities instrument, including organic frame, preceding Moving jack horse, lowering or hoisting gear, fixed rack and after
Moving jack horse；The frame has a platform, and the preceding Moving jack horse, lowering or hoisting gear, fixed rack and rear Moving jack horse are successively side by side
It is arranged on platform.
Preferably, the preceding Moving jack horse can longitudinal direction and slide laterally adjustment be arranged on platform.
Preferably, Moving jack horse longitudinal direction and can be arranged on platform with sliding laterally adjustment after described.
Preferably, the bottom of the frame is provided with foundation bolt.
Preferably, the lowering or hoisting gear includes transmission mechanism, support and fixture, and the transmission mechanism is located under platform
Side, the support upwardly extend through platform, and support is arranged at transmission mechanism, and transmission mechanism drives support oscilaltion activity, should
Fixture is arranged at the upper end of support and positioned at the top of platform.
The utility model has clear advantage and beneficial effect compared with prior art, specifically, by above-mentioned technology
Scheme is understood：
By the way that preceding Moving jack horse, lowering or hoisting gear, fixed rack and rear Moving jack horse are disposed side by side on platform successively, Gu
Determine the bay section that stand is used to fix guided missile, preceding Moving jack horse and rear Moving jack horse fix other bay sections of guided missile, the lifting
Device is used to, to missile cabin support, rotation, lifting and locking, missile cabin is departed from or is placed on fixed rack, so as to
So that present apparatus instrument can be used for placing guided missile and carry out performance detection, while bay section before and after docking body of being easy to change the outfit, and conveniently
Load and unload control flaps and aerofoil.
More clearly to illustrate architectural feature and effect of the present utility model, come below in conjunction with the accompanying drawings with specific embodiment pair
The utility model is described in detail：
Brief description of the drawings
Fig. 1 is the front view of the preferred embodiment of the utility model.
Accompanying drawing identifier declaration：
10th, frame 11, platform
12nd, foundation bolt 20, preceding Moving jack horse
30th, lowering or hoisting gear 31, transmission mechanism
32nd, support 33, fixture
40th, fixed rack 50, rear Moving jack horse
60th, guided missile
Embodiment
It refer to shown in Fig. 1, that show the concrete structure of the preferred embodiment of the utility model, including organic frame
10th, preceding Moving jack horse 20, lowering or hoisting gear 30, fixed rack 40 and rear Moving jack horse 50.
The frame 10 has a platform 11, also, the bottom of the frame 10 is provided with foundation bolt 12.
Preceding Moving jack horse 20, lowering or hoisting gear 30, fixed rack 40 and the rear Moving jack horse 50 are disposed side by side on platform successively
On 11.In the present embodiment, the preceding Moving jack horse 20 can longitudinal direction and slide laterally adjustment be arranged on platform 11, after described
Moving jack horse 50 can longitudinal direction and slide laterally adjustment be arranged on platform 11.Specifically, the lowering or hoisting gear 30 includes
Transmission mechanism 31, support 32 and fixture 33, the transmission mechanism 31 are located at the lower section of platform 11, and the support 32 is upward through platform 11
Extension, support 32 are arranged at transmission mechanism 31, and transmission mechanism 31 drives the oscilaltion activity of support 32, and the fixture 33 is arranged at branch
The upper end of frame 32 and the top for being located at platform 11.
The operation principle that the present embodiment is described in detail is as follows：
In use, the fixed rack 40 is used for a bay section for fixing guided missile 60.Preceding Moving jack horse 20 and rear Moving jack horse
50 can slide along X, Y direction and make that fine position is whole, and other bay sections of fixed guided missile 60, the lowering or hoisting gear 30 is used for leading
The support of the bay section of bullet 60, rotation, lifting and locking, the bay section of guided missile 60 is departed from or is placed on fixed rack 40.Present apparatus load-bearing
Not less than 500kg, meet that guided missile 60 conveniently, safely, and quickly can be changed the outfit and docked to guided missile in performance test.
Technical principle of the present utility model is described above in association with specific embodiment.These descriptions are intended merely to explain this reality
With new principle, and the limitation to scope of protection of the utility model can not be construed in any way.Based on explanation herein,
Those skilled in the art, which would not require any inventive effort, can associate other embodiments of the present utility model,
These modes are fallen within the scope of protection of the utility model.
Claims (5)
- The docking facilities instrument 1. a kind of guided missile changes the outfit, it is characterised in that：Including organic frame, preceding Moving jack horse, lowering or hoisting gear, fixed station Frame and rear Moving jack horse；The frame has a platform, the preceding Moving jack horse, lowering or hoisting gear, fixed rack and rear Moving jack horse It is disposed side by side on successively on platform.
- The docking facilities instrument 2. guided missile as claimed in claim 1 changes the outfit, it is characterised in that：The preceding Moving jack horse can be longitudinally and horizontal It is arranged to sliding on platform with adjusting.
- The docking facilities instrument 3. guided missile as claimed in claim 1 changes the outfit, it is characterised in that：Moving jack horse can be longitudinally and horizontal after described It is arranged to sliding on platform with adjusting.
- The docking facilities instrument 4. guided missile as claimed in claim 1 changes the outfit, it is characterised in that：The bottom of the frame is provided with lower margin Bolt.
- The docking facilities instrument 5. guided missile as claimed in claim 1 changes the outfit, it is characterised in that：The lowering or hoisting gear includes driver Structure, support and fixture, the transmission mechanism are located at the lower section of platform, and the support upwardly extends through platform, and support is arranged at transmission Mechanism, transmission mechanism drive support oscilaltion activity, and the fixture is arranged at the upper end of support and positioned at the top of platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720677041.3U CN206974290U (en) | 2017-06-12 | 2017-06-12 | Guided missile changes the outfit docking facilities instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720677041.3U CN206974290U (en) | 2017-06-12 | 2017-06-12 | Guided missile changes the outfit docking facilities instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206974290U true CN206974290U (en) | 2018-02-06 |
Family
ID=61408023
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720677041.3U Expired - Fee Related CN206974290U (en) | 2017-06-12 | 2017-06-12 | Guided missile changes the outfit docking facilities instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206974290U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110877752A (en) * | 2019-12-05 | 2020-03-13 | 江西洪都航空工业集团有限责任公司 | Multifunctional butt-joint platform |
| CN112304170A (en) * | 2020-09-16 | 2021-02-02 | 北京航空航天大学 | Guided missile assembly transportation integration platform |
| CN114111467A (en) * | 2021-12-16 | 2022-03-01 | 北京惠众智通机器人科技股份有限公司 | Automatic butt joint system for projectile body cabin sections and operation method |
-
2017
- 2017-06-12 CN CN201720677041.3U patent/CN206974290U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110877752A (en) * | 2019-12-05 | 2020-03-13 | 江西洪都航空工业集团有限责任公司 | Multifunctional butt-joint platform |
| CN112304170A (en) * | 2020-09-16 | 2021-02-02 | 北京航空航天大学 | Guided missile assembly transportation integration platform |
| CN114111467A (en) * | 2021-12-16 | 2022-03-01 | 北京惠众智通机器人科技股份有限公司 | Automatic butt joint system for projectile body cabin sections and operation method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180206 Termination date: 20210612 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |