CN207961404U - Damping device and sounding rocket emit transport vehicle - Google Patents
Damping device and sounding rocket emit transport vehicle Download PDFInfo
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- CN207961404U CN207961404U CN201820288333.2U CN201820288333U CN207961404U CN 207961404 U CN207961404 U CN 207961404U CN 201820288333 U CN201820288333 U CN 201820288333U CN 207961404 U CN207961404 U CN 207961404U
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Abstract
The utility model provides a kind of damping device and sounding rocket transmitting transport vehicle, belongs to vehicle-mounted sounding rocket lift-off technology field, which includes the first fixing piece, the second fixing piece, elastic element and locating rod；First fixing piece includes the first support plate and sleeve, second fixing piece includes the second support plate and inserted link, inserted link can be plugged in sleeve and can be moved axially along sleeve, and elastic element is socketed in sleeve and inserted link outer wall, and locating rod can extend into or be detached from sleeve inner.It in above-mentioned technical proposal, can be supported in the first support plate when inserted link extend into sleeve inner, make the first fixing piece that can not be moved towards the second fixing piece direction, the two forms rigid connection, to meet the mission need of rocket；When inserted link is detached from sleeve inner, the first fixing piece is enable to be moved towards the second fixing piece direction, the two forms elastic connection by elastic element, and free cushioning effect is played to meet rocket damping device in transportational process.
Description
Technical field
The utility model is related to vehicle-mounted sounding rocket lift-off technology fields, and in particular to a kind of damping device and sounding rocket
Transport car launcher.
Background technology
Sounding rocket is the rocket that terrestrial space carries out detection and scientific experimentation.The data obtained using sounding rocket is available
In weather forecast, the earth and astrophysics research, being provided for the aircraft development such as ballistic missile, carrier rocket, manned spaceship must
The environmental parameter wanted, sounding rocket can be additionally used in the experimental study of certain specific questions, the weightlessness such as provided using sounding rocket
The variation of state research living organism and adaptability carry out the proving test of new technology and instrument and equipment using sounding rocket
Deng.Sounding rocket flies high than sounding balloon, and the artificial satellite than low orbit operation flies low, is 30~200 kilometers of high-altitudes
Effective prospecting tools.
The general docking platform to carry rocket in the car launcher of sounding rocket is directly rigidly connected with vehicle frame at present,
Jerk is will produce in vehicle travels road, to be damaged to rocket, the transmitting of rocket is influenced whether or causes
Accidental launch brings security risk to indoor driver is driven, and therefore, how to eliminate this security risk is urgent need to resolve
The technical issues of.
Utility model content
The first of the utility model is designed to provide a kind of damping device, and when in use, manipulation positions the damping device
Bar makes the first fixing piece and the second fixing piece be in the unlocked position, and damping device is made to play free cushioning effect；It can also manipulate
Locating rod makes the first fixing piece and the second fixing piece be in the locked position, and damping device is made to play the role of rigid support, to make
Meet transport and the two different use environments of transmitting of rocket.
The second of the utility model is designed to provide a kind of sounding rocket transmitting transport vehicle, sounding rocket transmitting transport
Vehicle includes above-mentioned damping device, can make vehicle when driving using the damping device, to being used to support the general docking of rocket
Platform plays the role of cushioning effect, which can also make to play rigid support to general docking platform when rocket launching,
Rocket is avoided to be affected in transport or transmitting.
Based on above-mentioned first purpose, damping device provided by the utility model, including the first fixing piece, the second fixing piece,
Elastic element and locating rod；
First fixing piece includes the first support plate and sleeve, and the end face of first support plate connects the set
Cylinder；
Second fixing piece includes the second support plate and inserted link, and the end face connection of second support plate is described to insert
Bar,
The inserted link can be plugged in the sleeve and can be moved axially along the sleeve, the elastic element socket
In the sleeve and the inserted link outer wall, and the both ends of the elastic element are supported with the first support plate and described second respectively
Plate abuts against, and the inserted link, second support plate are coaxially disposed to accommodate the through-hole of the locating rod, the positioning respectively
Bar is arranged in the through-hole, and the locating rod can extend into or be detached from the sleeve inner.
In above-mentioned technical proposal, spring can make the first fixing piece be directed away from the second fixation under own resilient effect
It moves in the direction of part；Inserted link can be supported when extending into sleeve inner in the first support plate, make the first fixing piece can not court
It is moved to the second fixing piece direction, the two forms rigid connection, to meet the mission need of rocket；Inserted link is detached from sleeve inner
When, so that the first fixing piece is moved towards the second fixing piece direction, the two forms elastic connection by elastic element, to full
Final firing arrow damping device in transportational process plays free cushioning effect.
Further, the through-hole inside the inserted link is set as threaded hole, and the locating rod connects with the threaded hole screw thread
It connects.
In above-mentioned technical proposal, locating rod and inserted link interior bone are threadedly coupled, and adjusting locating rod is facilitated to stretch into or take off
From sleeve inner, to enable the first fixing piece and the second fixing piece to realize elastic connection or the two ways that is rigidly connected
Switching.
Further, the locating rod can be supported in the sleeve and be contacted with first support plate.
Using aforesaid way, locating rod can prevent that the first fixing piece is made to move towards the direction of the second fixing piece, to
Realize the rigid connection of the first fixing piece and the second fixing piece.
Further, the elastic element uses spring.
Further, further include pedestal, the pedestal is arranged in second support plate far from first fixing piece
End face, the pedestal have the through-hole for accommodating the locating rod.
In above-mentioned technical proposal, pedestal plays the supporting role to the second fixing piece.
Further, the pedestal of second support plate is detachably connected.
In above-mentioned technical proposal, the second support plate uses detachable connection with pedestal, is convenient for the second support plate and bottom
Assembly and replacement between seat.
Based on above-mentioned second purpose, a kind of sounding rocket transmitting transport vehicle provided by the utility model, including car body, guiding
Device, guider protective cover, regulating device, general docking platform and multiple above-mentioned damping devices；
The car body includes driver's cabin and vehicle frame, and the general docking platform bottom passes through the damping device and the vehicle
Frame connects, and the guider is arranged in the guider protective cover, the guider protective cover and the general docking platform
Flexible connection, the regulating device are separately connected the guider protective cover and the general docking platform.
In above-mentioned technical proposal, it is between general docking platform and vehicle frame using damping device, in rocket transportational process
In, manipulation locating rod makes the first fixing piece and the second fixing piece be in the unlocked position, and damping device is made to play the freedom to rocket
Cushioning effect；When rocket launching, manipulation locating rod makes the first fixing piece and the second fixing piece be in the locked position, and makes damping device
Play the role of rigid support, to make the transport for meeting rocket and the two different use environments of transmitting.
Further, the first support plate of the damping device is detachably connected with the general docking platform.Conveniently subtract
Shake the installation and replacement between device and general docking platform.
Further, sounding rocket transmitting transport vehicle further includes leveling support device, the leveling support device and institute
Vehicle frame connection is stated, the leveling support device has the telescopic supporting rod towards ground supports to carry out leveling to car body.
In above-mentioned technical proposal, using the leveling support device, facilitate the height for each position for adjusting car body, so that logical
It is in horizontality with docking platform, safety guarantee is provided for sounding rocket transmitting.
Further, sounding rocket transmitting transport vehicle further includes tool box, and the tool box is arranged at the vehicle frame bottom
End.
Using above-mentioned technical proposal, the technique effect of damping device provided by the utility model has：The damping device includes
First fixing piece, the second fixing piece, elastic element and locating rod；First fixing piece include the first support plate and sleeve, first
The end face branch sleeve of fagging；Second fixing piece includes the second support plate and inserted link, and the end face connection of the second support plate is inserted
Bar, inserted link can be plugged in sleeve and can be moved axially along sleeve, and elastic element is socketed in sleeve and inserted link outer wall, and
The both ends of elastic element are abutted against with the first support plate and the second support plate respectively, and inserted link, the second support plate are coaxially disposed respectively
To accommodate the through-hole of locating rod, locating rod is arranged in through-hole, and locating rod can extend into or be detached from sleeve inner.
In above-mentioned technical proposal, spring can make the first fixing piece be directed away from the second fixation under own resilient effect
It moves in the direction of part；Inserted link can be supported when extending into sleeve inner in the first support plate, make the first fixing piece can not court
It is moved to the second fixing piece direction, the two forms rigid connection, to meet the mission need of rocket；Inserted link is detached from sleeve inner
When, so that the first fixing piece is moved towards the second fixing piece direction, the two forms elastic connection by elastic element, to full
Final firing arrow damping device in transportational process plays free cushioning effect.
The technique effect of sounding rocket transmitting transport vehicle provided by the utility model has：The sounding rocket emits transport vehicle,
Including car body, guider, guider protective cover, regulating device, general docking platform and multiple above-mentioned damping devices；Car body
Including driver's cabin and vehicle frame, general docking platform bottom is connect by damping device with vehicle frame, and guider setting is anti-in guider
In shield, guider protective cover is flexibly connected with general docking platform, and regulating device is separately connected guider protective cover and general
Docking platform.
In above-mentioned technical proposal, it is between general docking platform and vehicle frame using damping device, in rocket transportational process
In, manipulation locating rod makes the first fixing piece and the second fixing piece be in the unlocked position, and damping device is made to play the freedom to rocket
Cushioning effect；When rocket launching, manipulation locating rod makes the first fixing piece and the second fixing piece be in the locked position, and makes damping device
Play the role of rigid support, to make the transport for meeting rocket and the two different use environments of transmitting.
Description of the drawings
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific implementation mode or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, other drawings may also be obtained based on these drawings.
Fig. 1 is the structural schematic diagram for the damping device that the utility model embodiment one provides；
Fig. 2 is the structural schematic diagram that the damping device that the utility model embodiment one provides is in the lock state；
Fig. 3 is the damping device of the offer of the utility model embodiment one structural schematic diagram in the unlocked state；
Fig. 4 is the structural schematic diagram that the sounding rocket that the utility model embodiment two provides emits transport vehicle.
Reference numeral：
The first fixing pieces of 100-；The second fixing pieces of 200-；300- elastic elements；400- locating rods；The first support plates of 110-；
120- sleeves；The second support plates of 210-；220- inserted links；500- pedestals；10- guider protective covers；20- regulating devices；30- is general
Docking platform；40- damping devices；50- driver's cabins；51- vehicle frames；60- leveling support devices；The tool boxes 70-.
Specific implementation mode
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally
The every other embodiment that field those of ordinary skill is obtained without making creative work, belongs to this practicality
Novel protected range.
It is in the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.In addition, term " the
One ", " second ", " third " are used for description purposes only, and are not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection；It can be mechanical connection, can also be electrical connection；Can be directly connected, can also indirectly connected through an intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, it can understand above-mentioned art with concrete condition
The concrete meaning of language in the present invention.
Fig. 1 shows the structural schematic diagram for the damping device that the utility model embodiment one provides；Fig. 2 shows this practicalities
The structural schematic diagram that the damping device that new embodiment one provides is in the lock state；Fig. 3 shows the utility model embodiment
The one damping device structural schematic diagram in the unlocked state provided；Fig. 4 shows the spy that the utility model embodiment two provides
The structural schematic diagram of empty rocket launching transport vehicle.
Embodiment one
It please refers to shown in Fig. 1-Fig. 3, damping device provided by the utility model, including the first fixing piece 100, second is fixed
Part 200, elastic element 300 and locating rod 400.
First fixing piece 100 includes the first support plate 110 and sleeve 120, the end face branch sleeve of the first support plate 110
120；
Second fixing piece 200 includes the second support plate 210 and inserted link 220, and the end face of the second support plate 210 connects inserted link
220,
Inserted link 220 can be plugged in sleeve 120 and can be moved axially along sleeve 120, and elastic element 300 is socketed in
Cylinder 120 and 220 outer wall of inserted link, and the both ends of elastic element 300 respectively with 210 phase of the first support plate 110 and the second support plate
It abuts, inserted link 220, the second support plate 210 are coaxially disposed to accommodate the through-hole of locating rod 400 respectively, and the setting of locating rod 400 exists
In through-hole, locating rod 400 be can extend into or be detached from inside sleeve 120.
In above-mentioned technical proposal, spring can make the first fixing piece 100 be directed away from second solid under own resilient effect
Determine the direction movement of part 200；Inserted link 220 can be supported when extending into 120 inside of sleeve in the first support plate 110, make first
Fixing piece 100 can not be moved towards 200 direction of the second fixing piece, and the two forms rigid connection, to meet the transmitting of rocket
Demand；When inserted link 220 is detached from 120 inside of sleeve, the first fixing piece 100 is enable to be moved towards 200 direction of the second fixing piece, two
Person forms elastic connection by elastic element 300, and free damping work is played to meet rocket damping device in transportational process
With.
In one preferred embodiment, the through-hole inside inserted link 220 is set as threaded hole, locating rod 400 and threaded hole spiral shell
Line connects.
In above-mentioned technical proposal, locating rod 400 and 220 interior bone of inserted link are threadedly coupled, and adjusting locating rod 400 is facilitated to stretch
Enter either be detached from sleeve 120 inside to enable the first fixing piece 100 and the second fixing piece 200 realize elastic connection or
The switching for the two ways that is rigidly connected.
It please refers to shown in Fig. 2 and Fig. 3, when it is implemented, rotating clockwise locating rod 400, locating rod 400 is made gradually to go deep into
To inside sleeve 120, until support to the first support plate 110, even if the first support plate 110 bears the gravity of rocket at this time, set
Cylinder 120 will not be moved towards inserted link 220, realized rigid connection, met the mission need of rocket.Rotate counterclockwise locating rod
400, make locating rod 400 far from sleeve 120 inside, sleeve 120 can overcome the elastic force of spring to be moved towards 220 direction of inserted link at this time
It is dynamic, it realizes elastic connection, meets the cushioning effect to rocket when transporting.
In one preferred embodiment, above-mentioned elastic element 300 uses spring.With simple in structure, low cost, it is convenient for
The characteristics of assembly.
In one preferred embodiment, which further includes pedestal 500, which is arranged in the second support plate
210 end faces far from the first fixing piece 100, pedestal 500 have the through-hole for accommodating locating rod 400.Above-mentioned technical proposal
In, pedestal 500 plays the supporting role to the second fixing piece 200.
In one preferred embodiment, the pedestal 500 of the second support plate 210 is detachably connected.
In above-mentioned technical proposal, the second support plate 210 uses detachable connection with pedestal 500, convenient for the second support
Assembly between plate 210 and pedestal 500 and replacement.When it is implemented, can be adopted between pedestal 500 and the second support plate 210
It is connected with mode.
Embodiment two
Shown in Fig. 1 and Fig. 4, a kind of sounding rocket provided by the utility model emits transport vehicle, including car body, leads
The damping provided into device, guider protective cover 10, regulating device 20, general docking platform 30 and multiple above-described embodiments one
Device 40.
Car body includes driver's cabin 50 and vehicle frame 51, and 30 bottom of general docking platform is connected by damping device 40 and vehicle frame 51
It connects, guider is arranged in guider protective cover 10, and guider protective cover 10 is flexibly connected with general docking platform 30, adjusts dress
It sets 20 and is separately connected guider protective cover 10 and general docking platform 30.
It in above-mentioned technical proposal, is between general docking platform 30 and vehicle frame 51 using damping device 40, is transported in rocket
During defeated, manipulation locating rod 400 makes the first fixing piece 100 and the second fixing piece 200 be in the unlocked position, and makes damping device 40
Play the free cushioning effect to rocket；When rocket launching, manipulation locating rod 400 makes the first fixing piece 100 and the second fixing piece
200 are in the locked position, and damping device 40 is made to play the role of rigid support, to make two kinds of the transport for meeting rocket and transmitting not
Same use environment.
One preferred embodiment, as shown in figure 4, two rows are arranged in damping device 40, two rows of damping devices are arranged at intervals on
The front side of general docking platform 30 and rear side, often row includes at least two damping devices, to be carried to general docking platform 30
For reliably supporting.
In one preferred embodiment, the first support plate 110 and the general docking platform 30 of damping device 40 detachably connect
It connects.Facilitate the installation and replacement between damping device 40 and general docking platform 30.
In one preferred real-time proposals, which may be used hydraulic telescopic rod, electric telescopic rod.
In one preferred embodiment, sounding rocket transmitting transport vehicle further includes leveling support device 60, leveling support
Device 60 is connect with vehicle frame 51, and leveling support device 60 has the telescopic supporting rod towards ground supports to be adjusted to car body
It is flat.
In above-mentioned technical proposal, facilitate the height for each position for adjusting car body using the leveling support device 60, so that
General docking platform 30 is in horizontality, and safety guarantee is provided for sounding rocket transmitting.
Hydraulic telescopic rod, electric telescopic rod or jack may be used in the leveling support device 60.Leveling support device can
With use above-mentioned each type, have the characteristics that it is simple in structure, be easily installed and regulate and control.
When it is implemented, at least four diagonal positions in vehicle frame 51 install an above-mentioned leveling support device respectively
60, when vehicle reaches transmitting destination, to general docking platform 30 and it is somebody's turn to do using the telescopic rod of four leveling support devices
Guider protective cover 10 on general docking platform 30 carries out leveling, to ensure the launch accuracy of sounding rocket.
In one preferred embodiment, sounding rocket transmitting transport vehicle further includes tool box 70, and the setting of tool box 70 exists
51 bottom end of vehicle frame.
It can be used for placing some common tools in tool box 70, tool box 70 is arranged in 51 bottom position of vehicle frame, will not
The space of driver's cabin 50 and the superjacent air space of vehicle frame 51 are occupied, use space is optimized.
Finally it should be noted that：The above various embodiments is only to illustrate the technical solution of the utility model, rather than limits it
System；Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should
Understand：It still can be with technical scheme described in the above embodiments is modified, either to which part or whole
Technical characteristic carries out equivalent replacement；And these modifications or replacements, this practicality that it does not separate the essence of the corresponding technical solution are new
The range of each embodiment technical solution of type.
Claims (10)
1. a kind of damping device, which is characterized in that including：First fixing piece, the second fixing piece, elastic element and locating rod；
First fixing piece includes the first support plate and sleeve, and the end face of first support plate connects the sleeve；
Second fixing piece includes the second support plate and inserted link, and the end face of second support plate connects the inserted link,
The inserted link can be plugged in the sleeve and can be moved axially along the sleeve, and the elastic element is socketed in institute
State sleeve and the inserted link outer wall, and the both ends of the elastic element respectively with the first support plate and the second support plate phase
It abuts, the inserted link, second support plate are coaxially disposed to accommodate the through-hole of the locating rod respectively, and the locating rod is set
It sets in the through-hole, the locating rod can extend into or be detached from the sleeve inner.
2. damping device according to claim 1, which is characterized in that the through-hole inside the inserted link is set as threaded hole,
The locating rod is threadedly coupled with the threaded hole.
3. damping device according to claim 1 or 2, which is characterized in that the locating rod can be supported in the sleeve
It is interior and contacted with first support plate.
4. damping device according to claim 1, which is characterized in that the elastic element uses spring.
5. damping device according to claim 1, which is characterized in that further include pedestal, pedestal setting is described the
End face of two support plates far from first fixing piece, the pedestal have the through-hole for accommodating the locating rod.
6. damping device according to claim 5, which is characterized in that the pedestal of second support plate detachably connects
It connects.
7. a kind of sounding rocket emits transport vehicle, which is characterized in that including car body, guider, guider protective cover, adjust dress
It sets, general docking platform and multiple claim 1-6 any one of them damping devices；
The car body includes driver's cabin and vehicle frame, and the general docking platform bottom is connected by the damping device and the vehicle frame
It connects, the guider is arranged in the guider protective cover, the guider protective cover and the general docking platform activity
Connection, the regulating device are separately connected the guider protective cover and the general docking platform.
8. sounding rocket according to claim 7 emits transport vehicle, which is characterized in that the first support of the damping device
Plate is detachably connected with the general docking platform.
9. sounding rocket according to claim 7 emits transport vehicle, which is characterized in that further include leveling support device, institute
It states leveling support device to connect with the vehicle frame, the leveling support device has the telescopic supporting rod towards ground supports with right
Car body carries out leveling.
10. sounding rocket according to claim 7 emits transport vehicle, which is characterized in that further include tool box, the tool
Case is arranged in the bottom end of vehicle frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820288333.2U CN207961404U (en) | 2018-03-01 | 2018-03-01 | Damping device and sounding rocket emit transport vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820288333.2U CN207961404U (en) | 2018-03-01 | 2018-03-01 | Damping device and sounding rocket emit transport vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207961404U true CN207961404U (en) | 2018-10-12 |
Family
ID=63740641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820288333.2U Active CN207961404U (en) | 2018-03-01 | 2018-03-01 | Damping device and sounding rocket emit transport vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207961404U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109681558A (en) * | 2018-12-26 | 2019-04-26 | 杭州程天科技发展有限公司 | Damping device and its wheel structure |
| CN115060122A (en) * | 2022-05-27 | 2022-09-16 | 火箭派(北京)航天科技有限公司 | Carrier rocket cabin section structure for modularized rapid assembly |
-
2018
- 2018-03-01 CN CN201820288333.2U patent/CN207961404U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109681558A (en) * | 2018-12-26 | 2019-04-26 | 杭州程天科技发展有限公司 | Damping device and its wheel structure |
| CN109681558B (en) * | 2018-12-26 | 2024-02-20 | 杭州程天科技发展有限公司 | Damping device and wheel structure thereof |
| CN115060122A (en) * | 2022-05-27 | 2022-09-16 | 火箭派(北京)航天科技有限公司 | Carrier rocket cabin section structure for modularized rapid assembly |
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