CN207018107U - A kind of carrier rocket ignition testing device - Google Patents
A kind of carrier rocket ignition testing device Download PDFInfo
- Publication number
- CN207018107U CN207018107U CN201720897702.3U CN201720897702U CN207018107U CN 207018107 U CN207018107 U CN 207018107U CN 201720897702 U CN201720897702 U CN 201720897702U CN 207018107 U CN207018107 U CN 207018107U
- Authority
- CN
- China
- Prior art keywords
- bearing frame
- rocket
- post
- trailer
- testing device
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- 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
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- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The utility model discloses a kind of carrier rocket ignition testing device,It is related to aerospace field,Including rocket body and trailer,The rocket body is above trailer,The trailer includes bearing frame,Some bearing bars being obliquely installed are hinged with the bearing frame,The bearing bar is provided with the retainer plate for being used for blocking rocket body,The retainer plate is divided to two valves,Bottom is hinged with iron,Top is fixedly connected using screw,The bottom of the bearing frame is provided with wheel,Limited block is provided with front of wheel,Limited block is articulated with the iron staff of bearing frame bottom,The side of the bearing frame and pass behind iron chains and be connected with locating pin,The locating pin includes post and shell,The post is socketed on enclosure,Post is provided with the head of a nail,The side of the head of a nail is provided with card article,The side top of the shell is provided with return-enclosure,Bottom is provided with some grooved bores,Rocket can effectively be fixed and avoid occurring surprisingly by the device.
Description
Technical field
It the utility model is related to aerospace field, and in particular to a kind of carrier rocket ignition testing device.
Background technology：
Carrier rocket is required for carrying out igniting test to rocket before formal transmitting, is happened suddenly when avoiding formally launching
Situation causes abortive launch, and needing to fix in rocket when lighting a fire and testing can not allow rocket really to be launched, otherwise consequence
Will be very serious, the effort of numerous personnel for a long time is not only wasted, property and life threat can be also brought to the people, because
This needs to design a kind of safe ignition testing device of comparison, such as application number：201510957793.0 disclose a kind of logical machine point
Firearm test device, including light-emitting window, light-emitting window include multiple runners of straight line arrangement, and rotation is provided with each runner and is driven
Dynamic device, different device of rotation driving can adjust different rotating speeds, and light-emitting window is arranged above the transmission along its axial movement
Band, the magnetic shoe being distributed along its axial strip is provided with each wheel surface, and each runner is connected with intelligent judging device.
In the course of the work, wheel drive means are opened, it is driven runner rotation, then place what is be detected on conveyer belt one end
Logical machine igniter, logical machine igniter is along transmission Tape movement and receives detection, because the velocity of rotation of runner is different, therefore when logical machine point
Firearm also just completes the survey for leading to the service behaviour of machine igniter under different rotating speeds after one section of transmission belt is moved to the other end
Examination, last each runner send the data detected to intelligent judging device, led to by what intelligent judging device judged to be detected
Whether machine igniter is qualified, and this kind of device obviously can not be applied on rocket.
Utility model content
The purpose of this utility model is to provide a kind of carrier rocket ignition testing device, to solve to cause in the prior art
Above-mentioned multinomial defect.
A kind of carrier rocket ignition testing device, including rocket body and trailer, the rocket body are provided with boost motor,
Boost motor and engine is equipped with the afterbody of rocket body, above trailer, the trailer includes holding the rocket body
Frame is weighed, some bearing bars being obliquely installed are hinged with the bearing frame, the bearing bar, which is provided with, to be used to block rocket body
Retainer plate, the retainer plate is divided to two valves, and bottom is hinged with iron, and top is fixedly connected using screw, the bottom of the bearing frame
Portion is provided with wheel, is provided with limited block in front of wheel, limited block is articulated with the iron staff of bearing frame bottom, the side of the bearing frame
And pass behind iron chains and be connected with locating pin, the locating pin includes post and shell, and the post is socketed on enclosure,
Post is provided with the head of a nail, and the side of the head of a nail is provided with card article, and the side top of the shell is provided with return-enclosure, and bottom is provided with some flutings
Hole.
Preferably, the bearing bar is connected by some springs with bearing frame.
Preferably, the bearing frame is reinforced by some poles being triangularly arranged.
Preferably, the internal layer of the retainer plate is provided with anti-slip rubber.
Preferably, the center-side of the post is provided with convex area.
The utility model has the advantage of：Ignition testing device in this, some be obliquely installed is hinged with the bearing frame
Bearing bar, inclined bearing bar can increase resistance, the side of the bearing frame and pass behind iron chains and be connected with positioning
Nail, locating pin is squeezed into ground and plays a part of fixed trailer, prevents trailer from being pushed by rocket, the locating pin include post and
Shell, the post are socketed on enclosure, and post is provided with the head of a nail, and the side of the head of a nail is provided with card article, the side of the shell
Top is provided with return-enclosure, and bottom is provided with some grooved bores, and card article can be caught in return-enclosure, plays firm effect, in the post
Heart end is provided with convex area, and while card article is caught in return-enclosure, fore-set down moves, and now convex area struts the bottom of shell,
Make contact of the shell with ground end even closer, connection is also just more firm, and the bearing bar passes through some springs and bearing frame connects
Connect, spring plays cushioning effect, makes vehicle body will not unexpected stress.
Brief description of the drawings
Fig. 1 is right view of the present utility model.
Fig. 2 is front view of the present utility model.
Fig. 3 is cross section view of the present utility model.
Fig. 4 is the structural representation of banking pin in the utility model.
Wherein：1-rocket body, 2-boost motor, 3-engine, 4-retainer plate, 5-spring, 6-pole, 7-hold
Weight bar, 8-iron staff, 9-limited block, 10-locating pin, 11-iron chains, 12-wheel, 13-anti-slip rubber, 14-iron,
15-screw, 16-grooved bore, 17-card article, 18-head of a nail, 19-shell, 20-post, 21-convex area, 22-return-enclosure,
23-trailer, 24-bearing frame.
Embodiment
Technological means, creation characteristic, reached purpose and effect to realize the utility model are easy to understand, below
With reference to embodiment, the utility model is expanded on further.
As shown in Figures 1 to 4, a kind of carrier rocket ignition testing device, including rocket body 1 and trailer 23, the fire
Arrow body 1 is provided with boost motor 2, boost motor 2 and is equipped with engine 3 with the afterbody of rocket body 1, and the rocket body 1 is set
Above trailer 23, the trailer 23 includes bearing frame 24, for carrying and moving rocket, if being hinged with the bearing frame 24
The dry bearing bar 7 being obliquely installed, inclined bearing bar 7 can increase resistance, and the bearing bar 7, which is provided with, to be used to block rocket sheet
The retainer plate 4 of body 1, the retainer plate 4 are divided to two valves, and bottom is hinged with iron 14, and top is fixedly connected using screw 15, for inciting somebody to action
Rocket body 1 is fixed up, and the bottom of the bearing frame 24 is provided with wheel 12, and the front of wheel 12 is provided with limited block 9, limited block 9
Be articulated with the iron staff 8 of the bottom of bearing frame 24, limited block 9 is desirable lower place with wheel 12 front, for stopping wheel 12
Rolling, the side of the bearing frame 24 and pass behind iron chains 11 and be connected with locating pin 10, locating pin 10 is squeezed into ground
Play a part of fixed trailer 23, prevent trailer 23 from being pushed by rocket, the locating pin 10 includes post 20 and shell 19, described
Post 20 is socketed on inside shell 19, and post 20 is provided with the head of a nail 18, and the side of the head of a nail 18 is provided with card article 17, the shell 19
Side top is provided with return-enclosure 22, and bottom is provided with some grooved bores 25, and card article 17 can be caught in return-enclosure 22, play firm effect.
It is worth noting that, the bearing bar 7 is connected by some springs 5 with bearing frame 24, spring plays cushioning effect,
Make vehicle body will not unexpected stress.
In the present embodiment, the bearing frame 24 is reinforced by some poles 6 being triangularly arranged, increase trailer 23
Stress intensity.
In the present embodiment, the internal layer of the retainer plate 4 is provided with anti-slip rubber 13, prevents rocket from sliding, anti-slip rubber 13
Retainer plate 4 can be enable further to clamp rocket body 1.
In addition, the center-side of the post 20 is provided with convex area 21, while card article 17 is caught in return-enclosure 22, fore-set 20 is past
Lower motion, now convex area 21 bottom of shell is strutted, make contact of the shell with ground end even closer, connection it is also just more firm
Gu.
Based on above-mentioned, ignition testing device in this, the rocket body 1 includes located at the top of trailer 23, the trailer 23
Bearing frame 24, for carrying and moving rocket, some bearing bars 7 being obliquely installed are hinged with the bearing frame 24, it is inclined
Bearing bar 7 can increase resistance, and the bottom of the bearing frame 24 is provided with wheel 12, and the front of wheel 12 is provided with limited block 9, limited block
9 are articulated with the iron staff 8 of the bottom of bearing frame 24, limited block 9 is desirable lower place with wheel 12 front, for stopping wheel 12
Rolling, the side of the bearing frame 24 and pass behind iron chains 11 and be connected with locating pin 10, locating pin 10 is squeezed into ground
Play a part of fixed trailer 23, prevent trailer 23 from being pushed by rocket, the locating pin 10 includes post 20 and shell 19, described
Post 20 is socketed on inside shell 19, and post 20 is provided with the head of a nail 18, and the side of the head of a nail 18 is provided with card article 17, the shell 19
Side top is provided with return-enclosure 22, and bottom is provided with some grooved bores 25, and card article 17 can be caught in return-enclosure 22, play firm effect,
The center-side of the post 20 is provided with convex area 21, and while card article 17 is caught in return-enclosure 22, fore-set 20 down moves, now convex
Play area 21 to strut the bottom of shell, make contact of the shell with ground end even closer, connection is also just more firm, the bearing bar
7 are connected by some springs 5 with bearing frame 24, and spring plays cushioning effect, make vehicle body will not unexpected stress.
As known by the technical knowledge, the utility model can pass through other essence without departing from its spirit or the reality of essential feature
Scheme is applied to realize.Therefore, embodiment disclosed above, for each side, all it is merely illustrative, is not only
's.It is all in the scope of the utility model or in the change being equal in the scope of the utility model by the utility model bag
Contain.
Claims (5)
1. a kind of carrier rocket ignition testing device, including rocket body (1) and trailer (23), it is characterised in that the rocket
Body (1) is provided with boost motor (2), and the afterbody of boost motor (2) and rocket body (1) is equipped with engine (3), the rocket sheet
For body (1) above the trailer (23), the trailer (23) includes bearing frame (24), is hinged with and some inclines on the bearing frame (24)
The bearing bar (7) tiltedly set, the bearing bar (7) are provided with the retainer plate (4) for being used for blocking rocket body (1), the fixation
Circle (4) is divided to two valves, and bottom is hinged with iron (14), and top is fixedly connected using screw (15), the bottom of the bearing frame (24)
Provided with wheel (12), limited block (9) is provided with front of wheel (12), limited block (9) is articulated with the iron staff (8) of bearing frame (24) bottom
On, the side of the bearing frame (24) and pass behind iron chains (11) and be connected with locating pin (10), locating pin (10) bag
Post (20) and shell (19) are included, the post (20) is socketed on shell (19) inside, and post (20) is provided with the head of a nail (18), follows closely
The side of cap (18) is provided with card article (17), and the side top of the shell (19) is provided with return-enclosure (22), and bottom is provided with some flutings
Hole (25).
A kind of 2. carrier rocket ignition testing device according to claim 1, it is characterised in that：The bearing bar (7) is logical
Some springs (5) are crossed to be connected with bearing frame (24).
A kind of 3. carrier rocket ignition testing device according to claim 2, it is characterised in that：The bearing frame (24) is logical
Some poles (6) being triangularly arranged are crossed to reinforce.
A kind of 4. carrier rocket ignition testing device according to claim 1, it is characterised in that：The retainer plate (4)
Internal layer is provided with anti-slip rubber (13).
A kind of 5. carrier rocket ignition testing device according to claim 1, it is characterised in that：In the post (20)
Heart end is provided with convex area (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720897702.3U CN207018107U (en) | 2017-07-24 | 2017-07-24 | A kind of carrier rocket ignition testing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720897702.3U CN207018107U (en) | 2017-07-24 | 2017-07-24 | A kind of carrier rocket ignition testing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207018107U true CN207018107U (en) | 2018-02-16 |
Family
ID=61481343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720897702.3U Expired - Fee Related CN207018107U (en) | 2017-07-24 | 2017-07-24 | A kind of carrier rocket ignition testing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207018107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112936202A (en) * | 2021-03-26 | 2021-06-11 | 北京中科宇航技术有限公司 | Solid carrier rocket final assembly frame vehicle |
-
2017
- 2017-07-24 CN CN201720897702.3U patent/CN207018107U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112936202A (en) * | 2021-03-26 | 2021-06-11 | 北京中科宇航技术有限公司 | Solid carrier rocket final assembly frame vehicle |
| CN112936202B (en) * | 2021-03-26 | 2023-06-23 | 北京中科宇航技术有限公司 | Solid carrier rocket assembly trolley |
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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: 20180216 Termination date: 20200724 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |