CN207922952U - Sounding rocket emits transport vehicle - Google Patents
Sounding rocket emits transport vehicle Download PDFInfo
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- CN207922952U CN207922952U CN201820288359.7U CN201820288359U CN207922952U CN 207922952 U CN207922952 U CN 207922952U CN 201820288359 U CN201820288359 U CN 201820288359U CN 207922952 U CN207922952 U CN 207922952U
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Abstract
The utility model provides a kind of sounding rocket transmitting transport vehicle, belongs to vehicle-mounted sounding rocket lift-off technology field, it includes car body, guider protective cover, regulating device, general docking platform, damping device and protective device which, which emits transport vehicle,；General docking platform is arranged by damping device on vehicle frame, damping device can be configured to resilient support pattern or rigid support pattern, guider protective cover is flexibly connected with general docking platform, regulating device is separately connected guider protective cover and general docking platform, the position close to driver's cabin in vehicle frame is arranged in protective device, also, protective device is located between driver's cabin and the guider protective cover being horizontal.It disclosure satisfy that rocket in the use demand transported or emitted using damping device; driver's cabin can be protected using protective device; it avoids the occurrence of accidental operation or security risk that other factors cause rocket to bring driver, protects the life security of driver.
Description
Technical field
The utility model is related to vehicle-mounted sounding rocket lift-off technology fields, and in particular to a kind of sounding rocket transmitting transport
Vehicle.
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；In addition, due to the sounding rocket face installed on car launcher
Driver's cabin, once security risk can be brought to indoor driver is driven by accidental operation or other factors occur, therefore, such as
What is the need remove the technical issues of above-mentioned security risk is urgent need to resolve.
Utility model content
The purpose of this utility model is to provide a kind of sounding rockets to emit transport vehicle, and sounding rocket transmitting transport vehicle exists
In use, can be configured to resilient support pattern or rigid support pattern using damping device, the transport of rocket can be met respectively
And launch requirements；Driver's cabin can be protected using protective device, avoiding the occurrence of accidental operation or other factors causes
The security risk that rocket brings driver protects the life security of driver.
Based on above-mentioned purpose, sounding rocket provided by the utility model emits transport vehicle, including：Car body, guider protection
Cover, regulating device, general docking platform, damping device and protective device；
The car body includes driver's cabin and vehicle frame, and the general docking platform is arranged by damping device in the vehicle frame
On, the damping device can be configured to resilient support pattern or rigid support pattern, the guider protective cover with it is described general
Docking platform is flexibly connected, and the regulating device is separately connected the guider protective cover and the general docking platform, described
Protective device is arranged in the vehicle frame close to the position of driver's cabin, also, the protective device is located at the driver's cabin and is in
Between the guider protective cover of horizontal position.
Further, the damping device includes 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.
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.
Further, sounding rocket transmitting transport vehicle further includes pedestal, and the pedestal is arranged in second support plate
End face far from first fixing piece, the pedestal have the through-hole for accommodating the locating rod.
Further, the protective device includes protective plate and protective base；The protective plate connects with the protective base
It connects.
Further, the protective plate is set as inclined surface close to the end face of guider protective cover, the inclined surface with
The horizontal plane has inclined angle alpha.
Further, sounding rocket transmitting transport vehicle further includes transmitting holder, the transmitting holder bottom end and the vehicle
Frame connects, and the transmitting upper end is to support guide protective cover.
Further, sounding rocket transmitting transport vehicle further includes heat preservation mechanism, and the heat preservation mechanism includes hair dryer dress
It sets and ventilation shaft；
The guider protective cover has air outlet and air inlet；The electric blower by ventilation shaft with it is described into
Air port is connected to, to convey hot gas into the guider protective cover.
Further, the electric blower includes shell and the air blower being arranged in the shell and electrical heating machine
The air outlet of the air blower described in face is arranged in structure, the electric heating mechanism, and the air of the air blower output is through electrical heating machine
It is delivered to inside guider protective cover by the ventilation shaft after structure heating.
Further, sounding rocket transmitting transport vehicle further includes controller, the controller and heat preservation mechanism electricity
Connection, the controller is controlling being turned on and off for the heat preservation mechanism.
Using above-mentioned technical proposal, the technique effect of sounding rocket transmitting transport vehicle provided by the utility model has：The spy
Empty rocket launching transport vehicle includes car body, guider protective cover, regulating device, general docking platform, damping device and protection dress
It sets；Car body includes driver's cabin and vehicle frame, and general docking platform is arranged by damping device on vehicle frame, and damping device can be configured to
Resilient support pattern or rigid support pattern, guider protective cover are flexibly connected with general docking platform, and regulating device connects respectively
Guider protective cover and the general docking platform are connect, the position close to driver's cabin in vehicle frame is arranged in protective device, also, protects
Device is located between driver's cabin and the guider protective cover being horizontal.
In above-mentioned technical proposal, general docking platform by damping device be arranged on vehicle frame, general docking platform to
Support guide protective cover, damping device can be configured to resilient support pattern or rigid support pattern, be configured to resilient support mould
When formula, it disclosure satisfy that and free cushioning effect is played to rocket in transportational process.When being configured to rigid support pattern, it disclosure satisfy that
The launch requirements of rocket；
Protective device is located between driver's cabin and the guider protective cover being horizontal, can be right using protective device
Driver's cabin is protected, and avoids the occurrence of accidental operation or security risk that other factors cause rocket to bring driver,
Protect the life security of driver.
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 that the sounding rocket that the utility model embodiment provides emits transport vehicle；
Fig. 2 is the structural schematic diagram for the damping device that the utility model embodiment provides；
Fig. 3 is the structural schematic diagram that the utility model embodiment provides that damping device is in rigid support pattern；
Fig. 4 is the structural schematic diagram that the damping device that the utility model embodiment provides is in resilient support pattern；
Fig. 5 is the structural schematic diagram for the protective device that the utility model embodiment provides；
Fig. 6 is the side view of Fig. 5；
Fig. 7 is the structural schematic diagram for the heat preservation mechanism that the utility model embodiment provides；
Fig. 8 is the structural schematic diagram for the electric blower that the utility model embodiment provides；
Fig. 9 is the control principle drawing for the heat preservation mechanism that the utility model embodiment provides.
Reference numeral：10- guider protective covers；11- driver's cabins；12- vehicle frames；13- air outlets；14- air inlets；20- tune
Regulating device；The general docking platforms of 30-；40- damping devices；The first fixing pieces of 41-；The second fixing pieces of 42-；43- elastic elements；
44- locating rods；The first support plates of 45-；46- sleeves；The second support plates of 47-；48- inserted links；49- pedestals；50- protective devices；51-
Protective plate；52- protective bases；The inclined surface 53-；60- emits holder；70- electric blowers；71- ventilation shafts；72- shells；
73- air blowers；74- electric heating mechanisms；80- is for electric installation.
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.
It please referring to shown in Fig. 1, sounding rocket provided by the utility model emits transport vehicle, including：Car body, guider protection
Cover 10, regulating device 20, general docking platform 30, damping device 40 and protective device 50.
Car body includes driver's cabin 11 and vehicle frame 12, and general docking platform 30 is arranged by damping device 40 on vehicle frame 12,
Damping device 40 can be configured to resilient support pattern or rigid support pattern, and guider protective cover 10 is lived with general docking platform 30
Dynamic connection, regulating device 20 are separately connected guider protective cover 10 and general docking platform 30, and protective device 50 is arranged in vehicle frame
12 close to the position of driver's cabin 11, also, the guider protective cover that protective device 50 is located at driver's cabin 11 and is horizontal
Between 10.
Two rows are arranged in one preferred embodiment, damping device 40, and two rows of damping devices 40 are arranged at intervals on general docking
The front side of platform 30 and rear side, often row includes at least two damping devices 40, to provide reliably general docking platform 30
Support.
It please refers to shown in Fig. 2 to Fig. 4, in a preferred embodiment, damping device 40 includes the first fixing piece 41, second
Fixing piece 42, elastic element 43 and locating rod 44.
First fixing piece 41 includes the first support plate 45 and sleeve 46, the end face branch sleeve 46 of the first support plate 45；
Second fixing piece 42 includes the second support plate 47 and inserted link 48, and the end face of the second support plate 47 connects inserted link 48；
Inserted link 48 can be plugged in sleeve 46 and can be moved axially along sleeve 46, and elastic element 43 is socketed in sleeve 46
With 48 outer wall of inserted link, and the both ends of elastic element 43 are abutted against with the first support plate 45 and the second support plate 47 respectively, inserted link
48, the second support plate 47 is coaxially disposed to accommodate the through-hole of locating rod 44 respectively, and locating rod 44 is arranged in through-hole, locating rod
44 can extend into or be detached from inside sleeve 46.
In one preferred embodiment, above-mentioned elastic element 43 uses spring.With simple in structure, low cost, it is convenient for
The characteristics of assembly.
Spring can be such that the direction that the first fixing piece 41 is directed away from the second fixing piece 42 moves under own resilient effect
It is dynamic；As shown in figure 3, inserted link 48 can be supported when extending into 46 inside of sleeve in the first support plate 45, make the first fixing piece 41
It can not be moved towards 42 direction of the second fixing piece, the two forms rigid connection, to meet the mission need of rocket；Such as Fig. 4
It is shown, when inserted link 48 is detached from 46 inside of sleeve, the first fixing piece 41 is enable to be moved towards 42 direction of the second fixing piece, the two is logical
It crosses elastic element 43 and forms elastic connection, free cushioning effect is played to meet rocket damping device 40 in transportational process.
In one preferred embodiment, the through-hole inside inserted link 48 is set as threaded hole, locating rod 44 and threaded hole screw thread
Connection.Locating rod 44 and 48 interior bone of inserted link are threadedly coupled, and adjusting locating rod 44 is facilitated to stretch into or be detached from inside sleeve 46,
To enable the first fixing piece 41 and the second fixing piece 42 to realize the switching of elastic connection or the two ways that is rigidly connected.
When it is implemented, rotating clockwise locating rod 44, locating rod 44 is made gradually to be deep into inside sleeve 46, until supporting
To the first support plate 45, even if the first support plate 45 bears the gravity of rocket at this time, sleeve 46 will not be moved towards inserted link 48,
Realization rigid connection (i.e. rigid support pattern, as shown in figure 3), meet the mission need of rocket.Rotate counterclockwise locating rod
44, make locating rod 44 far from sleeve 46 inside, sleeve 46 can overcome the elastic force of spring to be moved towards 48 direction of inserted link at this time, real
Existing elastic connection (flexibly supporting pattern, as shown in Figure 4), meets the cushioning effect to rocket when transporting.
In one preferred embodiment, sounding rocket transmitting transport vehicle further includes pedestal 49, and pedestal 49 is arranged second
End face of the support plate 47 far from the first fixing piece 41, pedestal 49 have the through-hole for accommodating locating rod 44.Pedestal 49 plays
Supporting role to the second fixing piece 42.
In one preferred embodiment, the pedestal 49 of the second support plate 47 is detachably connected.
In above-mentioned technical proposal, the second support plate 47 uses detachable connection with pedestal 49, is convenient for the second support plate
Assembly between 47 and pedestal 49 and replacement.When it is implemented, bolt may be used between pedestal 49 and the second support plate 47
Connection type.
In one preferred embodiment, the height on 50 top of protective device is higher than the guider protective cover being horizontal
The height on 10 top.
The height of protective device 50 and guider protective cover 10 uses above-mentioned set-up mode, and protective device 50 can be made along height
Direction covering guider protective cover 10 is spent, ensures the abundant protection to driver's cabin 11.
In one preferred embodiment, the width of protective device 50 is adapted to the width of driver's cabin 11.
The width of protective device 50 and guider protective cover 10 uses above-mentioned set-up mode, and protective device 50 can be made along vehicle
Width direction covering guider protective cover 10, ensures the abundant protection to driver's cabin 11.
As shown in Figure 5 and Figure 6, in a preferred embodiment, protective device 50 includes protective plate 51 and protective base 52；
Protective plate 51 is connect with protective base 52.
Protective base 52 is used for and vehicle frame 12 connects, and protective plate 51 plays the protective effect to driver's cabin 11.
The protective plate 51 preferably uses the steel plate of rectangle or square, has certain thickness, so that the steel plate
It can bear to be unlikely to damage driver's cabin 11 to rocket impact force.Protective base 52 is welded or is bolted
On the crossbeam on 12 chassis of vehicle frame, guarantee is capable of providing enough support strengths, can pass through welding between pedestal 49 and steel plate
Mode connect, can also use for example bolted detachable connection, above-mentioned protective plate 51 and protective base 52 can
Dismantling connection, convenient to protective plate 51, either protective base 52 is assembled or is replaced.
What needs to be explained here is that the height on 50 top of protective device of above-mentioned setting is higher than the guiding being horizontal
The height on the top of device protective cover 10 and the width of protective device 50 are adapted to the width of driver's cabin 11；Refer to protective plate
51 tip height and the width of protective plate 51.
In one preferred embodiment, protective plate 51 is set as inclined surface 53 close to the end face of guider protective cover 10,
Inclined surface 53 has inclined angle alpha with horizontal plane.
The inclined angle alpha is preferably arranged to 50 degree of -85 degree, and above-mentioned inclined surface 53 has inclined angle alpha with horizontal plane, it is therefore an objective to
At the inclined surface 53 of rocket crash plate 51, shock wave can be made to hoist pressure release along inclined surface 53, prevented to driver's cabin
11 damage, and reduce unnecessary loss.
In one preferred real-time proposals, which may be used hydraulic telescopic rod, electric telescopic rod.Using hydraulic pressure
Telescopic rod or electric telescopic rod are easier to be operated and be adjusted.
The effect of regulating device 20 is to adjust the raising or dropping action of guider protective cover 10, when guider protective cover
10 when being in raising state, and guider protective cover 10 and general docking platform 30 have certain inclination angle, can carry out rocket
Transmitting acts；When guider protective cover 10 is in landing state, guider protective cover 10 is in horizontality, can carry out fire
Arrow transports and storage.
In one preferred embodiment, sounding rocket transmitting transport vehicle further includes transmitting holder 60, please refers to Fig. 1, sends out
It penetrates 60 bottom end of holder to connect with vehicle frame 12, transmitting upper end is to support guide protective cover 10.Emit holder 60, plays to being oriented to
The Auxiliary support of device protective cover 10 acts on, and can share the pressure that regulating device 20 is subject to, and extend regulating device 20 uses the longevity
Life.
As shown in Figure 7 to 9, in a preferred embodiment, it further includes heat preservation mechanism which, which emits transport vehicle,
Heat preservation mechanism includes electric blower 70 and ventilation shaft 71；
Guider protective cover 10 has air outlet 13 and air inlet 14；Electric blower 70 passes through ventilation shaft 71 and air inlet
Mouth 14 is connected to, to convey hot gas into guider protective cover 10.Air outlet 13 is then being discharged in guider protective cover 10
Air.
In above-mentioned technical proposal, guider protective cover 10 plays the protective effect to guider and rocket, electric blower
70 can be passed through hot gas by ventilation shaft 71 into guider protective cover 10, the spy carried to rocket in guider protective cover 10
Empty instrument battery carries out heating and thermal insulation, it is ensured that sonde battery can work normally under low temperature environment.
In one preferred embodiment, ventilation shaft 71 is connected by the air inlet 14 of quick connector and guider protective cover 10
It connects, the purpose connected using quick connector is that being adjusted in guider protective cover 10 can be quickly by ventilation when vertical state is
Pipeline 71 disengages, to not interfere with the transmitting of rocket.
In one preferred embodiment, electric blower 70 includes shell 72 and the air blower 73 being arranged in shell 72
With electric heating mechanism 74, the air outlet 13 in face air blower 73 is arranged in electric heating mechanism 74, the air warp that air blower 73 exports
Electric heating mechanism 74 is delivered to by ventilation shaft 71 inside guider protective cover 10 after heating.
For air blower 73 to output gas flow, the air outlet 13 in air blower 73 is arranged in electric heating mechanism 74, and air blower 73 is defeated
The air-flow gone out is input to by ventilation shaft 71 in guider protective cover 10, by forming hot wind after air blower 73 to guider
Rocket carries out heating and thermal insulation in protective cover 10, it is ensured that sonde battery can work normally under low temperature environment.
In one preferred embodiment, electric heating mechanism 74 includes infrared electric heating tube.Infrared electric heating tube have it is simple in structure,
Fever is fast, the characteristics of being easily installed and safeguarding.
In one preferred embodiment, air outlet 13 is arranged in guider protective cover 10 by the position of front end, air inlet
Mouth 14 is arranged in the position close to middle rear end of guider protective cover 10.
In above-mentioned technical proposal, air outlet 13 and air inlet 14 be successively set on guider protective cover 10 by front end,
The position of middle rear end can ensure flowing stroke of the thermal current in guider protective cover 10, to guider protective cover 10
The sonde battery of interior rocket and its carrying is in stable temperature environment.
In one preferred embodiment, which further includes temperature-detecting device, temperature-detecting device
It is arranged in guider protective cover 10 and (does not illustrate in figure).
In above-mentioned technical proposal, temperature-detecting device can detect temperature in guider protective cover 10 in real time, and temperature is believed
Breath is supplied to staff.
In one preferred embodiment, it further includes controller, controller and heat preservation mechanism which, which emits transport vehicle,
Electrical connection, controller is controlling being turned on and off for heat preservation mechanism.
Specifically, the controller is electrically connected with the electric blower 70 in heat preservation mechanism, controller is controlling hair dryer
Device 70 is turned on and off.Also, the controller is also electrically connected with temperature-detecting device, is passed to receive temperature-detecting device
The temperature signal passed.
It can be realized using the controller and intelligent control is realized to the temperature in temperature guider protective cover 10.
Such as：When the temperature in guider protective cover 10 is too low, temperature signal is transferred to controller by temperature sensor,
There is preset temperature threshold, since temperature signal numerical value is less than the threshold value, controller output order makes air blower 73 in controller
It is powered with infrared electric heating tube, to make temperature in guider protective cover 10 be promoted.
When temperature is within the scope of preset temperature threshold in guider protective cover 10, air blower 73 and infrared electric heating tube not work
Make.
When temperature is excessively high in guider protective cover 10, is more than preset temperature threshold range in controller, controller output
Instruction control air blower 73 is powered, and infrared electric heating tube no power can increase the flowing of 10 interior air-flow of guider protective cover, rise at this time
To certain cooling effect.
In addition, as shown in Figure 1, sounding rocket transmitting transport vehicle further includes for electric installation 80, this includes for electric installation 80
Accumulator group and oil machine (diesel oil or gasoline engine generator).Accumulator group and oil machine are separately positioned on vehicle frame 12, accumulator and oil
Machine is electrically connected with infrared electric heating tube and air blower 73 respectively, in use, chance low temperature (- DEG C or less) weather, it should be before rocket launching
Hour, heating and thermal insulation measure is taken to rocket using oil start infrared electric heating tube and air blower 73, by transfer guard station to transmitting
In the driving process of position, it is readily modified as accumulator group and is powered.
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 sounding rocket emits transport vehicle, which is characterized in that including：It is car body, guider protective cover, regulating device, general
Docking platform, damping device and protective device；
The car body includes driver's cabin and vehicle frame, and the general docking platform is connect by damping device with the vehicle frame, described
Damping device can be configured to resilient support pattern or rigid support pattern, 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, the protective device
It is arranged in the vehicle frame close to the position of driver's cabin, also, the protective device is located at the driver's cabin and is horizontal
The guider protective cover between.
2. sounding rocket according to claim 1 emits transport vehicle, which is characterized in that the damping device includes first solid
Determine part, 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.
3. sounding rocket according to claim 2 emits transport vehicle, which is characterized in that the through-hole setting inside the inserted link
For threaded hole, the locating rod is threadedly coupled with the threaded hole.
4. sounding rocket according to claim 2 emits transport vehicle, which is characterized in that further include pedestal, the pedestal is set
It sets in end face of second support plate far from first fixing piece, the pedestal has for accommodating the locating rod
Through-hole.
5. sounding rocket according to claim 1 emits transport vehicle, which is characterized in that the protective device includes protective plate
And protective base；The protective plate is connect with the protective base.
6. sounding rocket according to claim 5 emits transport vehicle, which is characterized in that the protective plate is anti-close to guider
The end face of shield is set as inclined surface, and the inclined surface has inclined angle alpha with horizontal plane.
7. sounding rocket according to claim 1 emits transport vehicle, which is characterized in that further include transmitting holder, the hair
It penetrates holder bottom end to connect with the vehicle frame, the transmitting upper end is to support guide protective cover.
8. sounding rocket according to claim 1 emits transport vehicle, which is characterized in that further include heat preservation mechanism, the guarantor
Warm mechanism includes electric blower and ventilation shaft；
The guider protective cover has air outlet and air inlet；The electric blower passes through ventilation shaft and the air inlet
Connection, to convey hot gas into the guider protective cover.
9. sounding rocket according to claim 8 emits transport vehicle, which is characterized in that the electric blower includes shell
And the air blower described in face is arranged in the air blower and electric heating mechanism being arranged in the shell, the electric heating mechanism
The air of air outlet, the air blower output is delivered to guider protection after electric heating mechanism heats by the ventilation shaft
Cover is internal.
10. sounding rocket according to claim 8 emits transport vehicle, which is characterized in that further include controller, the control
Device is electrically connected with the heat preservation mechanism, and the controller is controlling being turned on and off for the heat preservation mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820288359.7U CN207922952U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket emits transport vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820288359.7U CN207922952U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket emits transport vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN207922952U true CN207922952U (en) | 2018-09-28 |
Family
ID=63601881
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820288359.7U Active CN207922952U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket emits transport vehicle |
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| CN (1) | CN207922952U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110949695A (en) * | 2018-12-20 | 2020-04-03 | 中国船舶重工集团应急预警与救援装备股份有限公司 | Booster and core-level rocket binding butt joint vertical direction adjusting system |
| CN110963421A (en) * | 2018-12-20 | 2020-04-07 | 中国人民解放军63921部队 | Multifunctional rocket transport erecting vehicle |
| CN112229270A (en) * | 2020-10-13 | 2021-01-15 | 北京航天发射技术研究所 | Can splice motor-driven carrier rocket launching platform |
| CN112343962A (en) * | 2020-11-03 | 2021-02-09 | 西安航天动力技术研究所 | Damping support of rocket launcher |
-
2018
- 2018-03-01 CN CN201820288359.7U patent/CN207922952U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110949695A (en) * | 2018-12-20 | 2020-04-03 | 中国船舶重工集团应急预警与救援装备股份有限公司 | Booster and core-level rocket binding butt joint vertical direction adjusting system |
| CN110963421A (en) * | 2018-12-20 | 2020-04-07 | 中国人民解放军63921部队 | Multifunctional rocket transport erecting vehicle |
| CN112229270A (en) * | 2020-10-13 | 2021-01-15 | 北京航天发射技术研究所 | Can splice motor-driven carrier rocket launching platform |
| CN112229270B (en) * | 2020-10-13 | 2023-04-25 | 北京航天发射技术研究所 | Can splice motor-driven carrier rocket launching platform |
| CN112343962A (en) * | 2020-11-03 | 2021-02-09 | 西安航天动力技术研究所 | Damping support of rocket launcher |
| CN112343962B (en) * | 2020-11-03 | 2022-08-19 | 西安航天动力技术研究所 | Damping support of rocket launcher |
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