CN206974292U - A kind of safety instrumentation of rocket priming system - Google Patents
A kind of safety instrumentation of rocket priming system Download PDFInfo
- Publication number
- CN206974292U CN206974292U CN201720897759.3U CN201720897759U CN206974292U CN 206974292 U CN206974292 U CN 206974292U CN 201720897759 U CN201720897759 U CN 201720897759U CN 206974292 U CN206974292 U CN 206974292U
- Authority
- CN
- China
- Prior art keywords
- plate
- priming system
- front side
- bottom plate
- side board
- 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 safety instrumentation of rocket priming system,It is related to priming system technical field,Including explosion-proof tank and priming system fixed mechanism,Explosion-proof tank is by bottom plate,Top plate and side plate composition,Priming system fixed mechanism is located on the bottom plate in explosion-proof tank,Top plate is provided with the fairlead being used for through ignition fuse,Left plate,Right plate,Back side panel welds with bottom plate and top plate,Front side board is hinged with bottom plate,Anti whip device is installed on the inwall of side plate,Anti whip device includes steel plate,Guide rod,Back-moving spring and locking nut,Steel plate is provided with pilot hole and through hole,Guide rod one end is welded on the inwall of side plate and the other end passes through pilot hole,The end of guide rod is externally threaded,Acoustical panel is installed between steel plate and side plate,Priming system fixed mechanism includes column,Supporting plate,Support frame and pressing plate,The utility model is during testing priming system,Improve the security of test,It is easy to the positioning to priming system.
Description
Technical field
It the utility model is related to priming system technical field, and in particular to a kind of safety instrumentation of rocket priming system.
Background technology：
With being continuously increased for high density launch mission, priming system number practical on body armament systems and carrier rocket
Amount is also more and more, a critically important key element of the priming system as system transmitting success or failure, the fine or not direct shadow of its performance
The reliability to whole system work is rung, therefore its performance must be tested and considered before arrow on bullet on priming system.
In view of the particularity of fire attack articles for use, in order to prevent that generation accidental explosion accident causes unnecessary in test process
Loss tested, it is necessary to which priming system is placed in the environment of a safety, even if occur blast also will not be to surrounding
People and thing damage, therefore need when testing priming system to carry out full safeguard procedures.
Utility model content
The purpose of this utility model is to provide a kind of safety instrumentation of rocket priming system, in order to improves
Security of the priming system in test process.
A kind of safety instrumentation of rocket priming system, including explosion-proof tank and priming system fixed mechanism, the explosion-proof tank
It is made up of bottom plate, top plate and side plate, the side plate includes left plate, right plate, front side board and back side panel, and the priming system is fixed
Mechanism is located on the bottom plate in explosion-proof tank, and the top plate is provided with the fairlead being used for through ignition fuse, the left plate, the right side
Side plate, back side panel are welded with bottom plate and top plate, and the front side board is hinged with bottom plate, and erosion control is provided with the inwall of the side plate
Device is hit, the anti whip device includes steel plate, guide rod, back-moving spring and locking nut, and the steel plate is provided with pilot hole
And through hole, described guide rod one end is welded on the inwall of side plate and the other end passes through pilot hole, and the end of guide rod is tapped with outside
Screw thread, locking nut coordinate with guide rod thread, and acoustical panel, the acoustical panel fastening peace are provided between the steel plate and side plate
On the inwall of side plate, the acoustical panel is provided with bloop, and the side plate is provided with airflow hole, and airflow hole connects with bloop
Logical, the bottom plate is provided with chute, is provided with slide in chute, the glide direction of slide is vertical with front side board, and the priming system is consolidated
Determining mechanism includes column, supporting plate, support frame and pressing plate, and the column and support frame are arranged on the upper surface of slide, the branch
Fagging is horizontally arranged on column, and the upper surface of the pressing plate is provided with screw rod, and support frame as described above is provided with screwed hole one, screw rod with
Screwed hole one is engaged, and the top of screw rod is provided with adjusting handle.
Preferably, the lower end of the explosion-proof tank is provided with Moving caster.
Preferably, the bottom plate is provided with hinged seat, and the outer wall of the front side board is provided with support bar, support bar and front side
Plate is vertical, is provided with bolt hole on the top plate with the end face of front side board contact, and the upper end of front side board is real by clamping screw one
Existing fastening between top plate and front side board.
Preferably, the chute is T-slot, and the slide is arranged in T-slot, and T-slot is provided with perpendicular to bottom plate
Thread groove, slide are provided with screwed hole two, and fastening of the slide in chute is realized by clamping screw two.
The utility model has the advantage of：The utility model discloses a kind of safety instrumentation of rocket priming system,
When in use, front side board is opened, slide is slided towards close to the direction of front side board, priming system is placed on the supporting plate, turned
Dynamic adjusting handle makes pressing plate push down priming system, the positioning of priming system is so achieved that, then by slide away from front side
The direction movement of plate, when the thread groove of the screwed hole two on slide and chute bottom is located in same vertical straight line, utilize lock
Slide is positioned in chute by tight bolt two, then closes front side board, and the upper end of front side board is fastened into peace using clamping screw one
Mounted in the side of top plate, mobile explosion-proof tank to pilot region, fire-working article test is carried out.
When being tested, by ignition fuse from the fairlead of top plate upper end pass carry out fire trial, work as priming system
Generation explosion time, because the inwall in side plate is provided with anti whip device, priming system explosion time can produce shock wave, and steel plate is rushed
Hitting the effect of ripple can move away from the direction of priming system fixed mechanism, and back-moving spring produces deformation, is rushed caused by shock wave
Elastic potential energy can be partially converted into by hitting energy, reach the buffering effect of shock wave, in addition because sound caused by shock wave is gentle
Stream can sequentially pass through the through hole on steel plate, the sound attenuation hole on acoustical panel, finally be overflowed from the airflow hole of side plate.
The utility model improves the security of test, is easy to priming system during testing priming system
Positioning.
Brief description of the drawings
Fig. 1 is a kind of front view of the safety instrumentation of rocket priming system described in the utility model.
Fig. 2 is a kind of side view of the safety instrumentation of rocket priming system described in the utility model.
Fig. 3 is a kind of the partially schematic of side view of the safety instrumentation of rocket priming system described in the utility model
Figure.
Wherein：1-Moving caster, 2- bottom plates, 3- left plates, 4- acoustical panels, 5- airflow holes, 6- steel plates, 7- back side panels, 8-
Top plate, 9- guide rods, 10- right plates, 11- back-moving springs, 12- pressing plates, 13- supporting plates, 14- slides, 15- support frames, 16- locks
Tight bolt two, 17- chutes, 18- front side boards, 19- bolts hole, 20- support bars, 21- clamping screws one, 22- hinged seats, 23- are adjusted
Save handwheel.
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 Figure 1 to Figure 3, a kind of safety instrumentation of rocket priming system, including explosion-proof tank and priming system are fixed
Mechanism, the explosion-proof tank are made up of bottom plate 2, top plate 8 and side plate, and the side plate includes left plate 3, right plate 10, front side board 18
With back side panel 7, the priming system fixed mechanism is located on the bottom plate 2 in explosion-proof tank, and the top plate 8, which is provided with, to be used for through igniting
The fairlead (being not drawn into figure) of lead, the left plate 3, right plate 10, back side panel 7 weld with bottom plate 2 and top plate 8, institute
It is be hinged with bottom plate 2 to state front side board 18, anti whip device is installed, the anti whip device includes steel plate on the inwall of the side plate
6th, guide rod 9, back-moving spring 11 and locking nut, the steel plate 6 are provided with pilot hole and through hole, the one end of guide rod 9 weldering
It is connected on the inwall of side plate and the other end passes through pilot hole, the end of guide rod is externally threaded, locking nut and the spiral shell of guide rod 9
Line coordinates, and acoustical panel 4 is provided between the steel plate 6 and side plate, the acoustical panel 4 is securedly mounted on the inwall of side plate, institute
State acoustical panel 4 and be provided with bloop, the side plate is provided with airflow hole 5, and airflow hole 5 connects with bloop, is set on the bottom plate 2
There is chute 17, be provided with slide 14 in chute 17, the glide direction of slide 14 is vertical with front side board 18, the priming system fixed mechanism
Including column, supporting plate 13, support frame 15 and pressing plate 12, the column and support frame 15 are arranged on the upper surface of slide 14, institute
State supporting plate 13 to be horizontally arranged on column, the upper surface of the pressing plate 12 is provided with screw rod, and support frame as described above 15 is provided with screw thread
Kong Yi, screw rod are engaged with screwed hole one, and the top of screw rod is provided with adjusting handle 23.
In the present embodiment, the lower end of the explosion-proof tank is provided with Moving caster 1.
In the present embodiment, the bottom plate 2 is provided with hinged seat 22, and the outer wall of the front side board 18 is provided with support bar
20, support bar 20 is vertical with front side board 18, and when front side board 18 is opened, support bar 20 plays a part of support positioning, described
The end face contacted on top plate 8 with front side board 18 is provided with bolt hole 19, and the upper end of front side board 18 passes through clamping screw 1 and realized
Fastening between top plate 8 and front side board 18.
In the present embodiment, the chute 17 is T-slot, and the slide 14 is arranged in T-slot, and T-slot, which is provided with, hangs down
Screwed hole two directly is provided with the thread groove of bottom plate, slide 14, realizes slide 14 in chute 17 by clamping screw 2 16
Fastening.
In the utility model, the purpose of chute 17 and slide 14 is set to be in order to when being positioned to priming system, incite somebody to action
Priming system fixed mechanism is moved to close to the position of front side board 18, is slided after the completion of priming system is positioned by priming system fixed mechanism
Move to the center of bottom plate 2.
The utility model has the advantage of：The utility model discloses a kind of safety instrumentation of rocket priming system,
When in use, front side board 18 is opened, slide 14 is slided towards close to the direction of front side board 18, priming system is placed on supporting plate
On 13, rotating adjusting handle 23 makes pressing plate push down priming system, the positioning of priming system is so achieved that, then by the court of slide 14
The direction away from front side board 18 to move, when the thread groove of the screwed hole two on slide 14 and the bottom of chute 17 is positioned at same vertical
When on straight line, slide 14 is positioned in chute 17 using clamping screw 2 16, front side board 18 is then closed, utilizes clamping screw
One 21 are securedly mounted to the upper end of front side board 18 side of top plate 8, mobile explosion-proof tank to pilot region, to carry out priming system survey
Examination.
When being tested, by ignition fuse from the fairlead of top plate upper end pass carry out fire trial, work as priming system
Generation explosion time, due to being provided with anti whip device in the inwall of side plate, priming system explosion time can produce shock wave, steel plate 6 by
The effect of shock wave can move away from the direction of priming system fixed mechanism, and back-moving spring 11 produces deformation, and shock wave produces
Impact energy can be partially converted into elastic potential energy, reach the buffering effect of shock wave, in addition because of sound caused by shock wave
The through hole on steel plate 6, the sound attenuation hole on acoustical panel 4 can be sequentially passed through with air-flow, is finally overflowed from the airflow hole 5 of side plate.
The utility model improves the security of test, is easy to priming system during testing priming system
Positioning.
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 (4)
1. a kind of safety instrumentation of rocket priming system, including explosion-proof tank and priming system fixed mechanism, the explosion-proof tank by
Bottom plate (2), top plate (8) and side plate composition, the side plate include left plate (3), right plate (10), front side board (18) and back side panel
(7), the priming system fixed mechanism is located on the bottom plate (2) in explosion-proof tank, and the top plate (8), which is provided with, to be used to draw through igniting
The fairlead of line, it is characterised in that the left plate (3), right plate (10), back side panel (7) with bottom plate (2) and top plate (8)
Welding, the front side board (18) is be hinged with bottom plate (2), and anti whip device, the protecting against shock are provided with the inwall of the side plate
Device includes steel plate (6), guide rod (9), back-moving spring (11) and locking nut, and the steel plate (6) is provided with pilot hole and led to
Hole, described guide rod (9) one end is welded on the inwall of side plate and the other end passes through pilot hole, and the end of guide rod (9) is tapped with
External screw thread, locking nut coordinate with guide rod (9) screw thread, and the steel plate (6) is provided with acoustical panel (4) between side plate, described
Acoustical panel (4) is securedly mounted on the inwall of side plate, and the acoustical panel (4) is provided with bloop, and the side plate is provided with air-flow
Hole (5), airflow hole (5) connect with bloop, and the bottom plate (2) is provided with chute (17), and slide (14) is provided with chute (17),
The glide direction of slide (14) is vertical with front side board (18), and the priming system fixed mechanism includes column, supporting plate (13), support
Frame (15) and pressing plate (12), the column and support frame (15) are arranged on the upper surface of slide (14), supporting plate (13) water
Safety is on column, and the upper surface of the pressing plate (12) is provided with screw rod, and support frame as described above (15) is provided with screwed hole one, screw rod
It is engaged with screwed hole one, the top of screw rod is provided with adjusting handle (23).
A kind of 2. safety instrumentation of rocket priming system according to claim 1, it is characterised in that：The explosion-proof tank
Lower end be provided with Moving caster (1).
A kind of 3. safety instrumentation of rocket priming system according to claim 1, it is characterised in that：The bottom plate
(2) hinged seat (22) is provided with, the outer wall of the front side board (18) is provided with support bar (20), support bar (20) and front side board
(18) vertically, the end face on the top plate (8) with front side board (18) contact is provided with bolt hole (19), the upper end of front side board (18)
Fastening between top plate (8) and front side board (18) is realized by clamping screw one (21).
A kind of 4. safety instrumentation of rocket priming system according to claim 1, it is characterised in that：The chute
(17) it is T-slot, the slide (14) is arranged in T-slot, and T-slot is provided with the thread groove perpendicular to bottom plate (2), slide
(14) screwed hole two is provided with, fastening of the slide (14) in chute (17) is realized by clamping screw two (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720897759.3U CN206974292U (en) | 2017-07-24 | 2017-07-24 | A kind of safety instrumentation of rocket priming system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720897759.3U CN206974292U (en) | 2017-07-24 | 2017-07-24 | A kind of safety instrumentation of rocket priming system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206974292U true CN206974292U (en) | 2018-02-06 |
Family
ID=61397403
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720897759.3U Expired - Fee Related CN206974292U (en) | 2017-07-24 | 2017-07-24 | A kind of safety instrumentation of rocket priming system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206974292U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109459176A (en) * | 2018-10-30 | 2019-03-12 | 王少明 | There is the detection device of interim test power in firecracker production link |
-
2017
- 2017-07-24 CN CN201720897759.3U patent/CN206974292U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109459176A (en) * | 2018-10-30 | 2019-03-12 | 王少明 | There is the detection device of interim test power in firecracker production link |
| CN109459176B (en) * | 2018-10-30 | 2020-12-04 | 嘉兴尚坤科技有限公司 | Detection device with temporary testing power in firecracker production link |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Christiansen et al. | Mesh double-bumper shield: a low-weight alternative for spacecraft meteoroid and orbital debris protection | |
| CN206974292U (en) | A kind of safety instrumentation of rocket priming system | |
| CN108166779B (en) | Environmental bin for power battery | |
| CN110785036A (en) | Big data computer network safety device | |
| CN108894154A (en) | A kind of anti-rebound cushion guardail in tunnel | |
| CN109098693B (en) | Electromagnetic control's high pressure bubble source device under water | |
| CN207575615U (en) | A kind of superhigh pressure water jet fine water mist fire extinguishing equipment punctures spray gun | |
| CN106524843A (en) | Initiator testing safety device | |
| CN108548461B (en) | Fixing device convenient for fixing and hanging of ammunition in blast hole for engineering blasting | |
| CN206925901U (en) | A kind of impact protection apparatus for industrial robot | |
| CN219827969U (en) | Anti-smoke and anti-vibration support | |
| CN219641202U (en) | New energy automobile battery test platform with protective structure | |
| CN209994729U (en) | Hot runner control cabinet with vibration/noise reduction function | |
| CN106908338B (en) | A kind of high temperature and pressure hits the impact test platform of material more | |
| Zhao et al. | Experiment study of outburst pulverized coal-gas two-phase flow and characteristic analysis of outburst wave | |
| CN207556971U (en) | A kind of protective device of pendulum percussion instrument | |
| CN212964439U (en) | Low-speed penetration experimental device based on separated Hopkinson pressure bar | |
| CN213633016U (en) | Laboratory high strength crashproof material shock resistance testing arrangement | |
| CN206330493U (en) | A kind of fire-working article test safety device | |
| CN203783626U (en) | Explosion suppression device for gas transportation pipeline | |
| CN214067025U (en) | Bolt type strain clamp detection device | |
| CN110095299A (en) | A kind of fire disaster simulation device for testing fire water monitor | |
| CN219200839U (en) | A high strength test bed frame for aeroengine part test | |
| CN206660360U (en) | A kind of multifunctional fire-fighting shield | |
| CN206492123U (en) | Recoil multi-section type dismantling device |
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: 20200724 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |