CN207955443U - Sounding rocket attemperator and sounding rocket emit transport vehicle - Google Patents
Sounding rocket attemperator and sounding rocket emit transport vehicle Download PDFInfo
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- CN207955443U CN207955443U CN201820288150.0U CN201820288150U CN207955443U CN 207955443 U CN207955443 U CN 207955443U CN 201820288150 U CN201820288150 U CN 201820288150U CN 207955443 U CN207955443 U CN 207955443U
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- guider
- protective cover
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Abstract
The utility model provides a kind of sounding rocket attemperator and sounding rocket transmitting transport vehicle, belong to vehicle-mounted sounding rocket lift-off technology field, the sounding rocket attemperator includes shell and the air blower and electric heating mechanism that are arranged in the shell, the air outlet of the air blower described in face is arranged in the electric heating mechanism, and the air of the air blower output is delivered to by the ventilation shaft inside guider protective cover after electric heating mechanism heats.In above-mentioned technical proposal, air blower is to output gas flow, the air outlet in air blower is arranged in electric heating mechanism, the air-flow of air blower output after air blower by forming hot wind, it is input in guider protective cover by ventilation shaft, heating and thermal insulation is carried out to rocket in guider protective cover, it is ensured that sonde battery can work normally under low temperature environment.Sounding rocket transmitting transport vehicle uses above-mentioned sounding rocket attemperator, the These characteristics with the sounding rocket attemperator.
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 attemperator and
Sounding rocket emits 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.
At present the car launcher of sounding rocket carry out emission experiment environment it is generally relatively severe, rocket when the temperature is too low
Sonde battery then can not work normally, and make a big impact to experiment, therefore, how to eliminate this hidden danger is urgent need to resolve
Technical problem.
Utility model content
The first of the utility model is designed to provide a kind of sounding rocket attemperator, which exists
In use, into guider protective cover hot gas is conveyed by ventilation shaft using electric blower, to the sonde to rocket
Battery carries out heating and thermal insulation, it is ensured that sonde battery can work normally under low temperature environment.
The second of the utility model is designed to provide a kind of sounding rocket transmitting transport vehicle, sounding rocket transmitting transport
Vehicle uses above-mentioned sounding rocket attemperator.
Based on above-mentioned first purpose, sounding rocket attemperator provided by the utility model, including electric blower and logical
Wind pipeline；
The electric blower includes shell and the air blower and electric heating mechanism that are arranged in the shell, the electricity
The air outlet of the air blower described in face is arranged in heating mechanism, and the air of the air blower output leads to after electric heating mechanism heats
The ventilation shaft is crossed to be delivered to inside guider protective cover.
In above-mentioned technical proposal, for air blower to output gas flow, the air outlet in air blower, air blast is arranged in electric heating mechanism
The air-flow of machine output is input to by ventilation shaft in guider protective cover by forming hot wind after air blower, anti-to guider
Rocket carries out heating and thermal insulation in shield, it is ensured that sonde battery can work normally under low temperature environment.
Further, to load guider and rocket, the guider protective cover has the guider protective cover
Air port and air inlet；The electric blower is connected to by ventilation shaft with the air inlet, to be protected to the guider
Hot gas is conveyed in cover.
In above-mentioned technical proposal, guider protective cover plays the protective effect to guider, and electric blower passes through ventilation
Pipeline can be passed through hot gas into guider protective cover, carry out heating and thermal insulation to rocket in guider protective cover, it is ensured that low temperature ring
Sonde battery can work normally under border.
Further, the electric heating mechanism includes infrared electric heating tube.
In above-mentioned technical proposal, electric heating mechanism using infrared electric heating tube have simple in structure, fever is fast, be easily installed and
The characteristics of safeguarding.
Further, the air outlet is arranged in the guider protective cover by the position of front end, the air inlet
It is arranged in the position close to middle rear end of the guider protective cover.
In above-mentioned technical proposal, air outlet and air inlet be successively set on guider protective cover by front end, middle rear end
Position, can ensure flowing stroke of the thermal current in guider protective cover, to in guider protective cover rocket and
Its sonde battery carried is in stable temperature environment.
Further, guider protective cover upper end has debugging operations hole.
The debugging operations hole, which is played, facilitates technical staff to switch or tie up the devices such as power supply in guider protective cover
Nurse makees.
Further, further include debugging operations frame, the debugging operations frame is arranged on the guider protective cover, described
Debugging operations frame can be moved along guider protective cover length direction.
In above-mentioned technical proposal, debugging operations erect carrying staff's effect, convenient for staff to debugging operations
The equipment such as hole interior power are manipulated.
Further, which further includes temperature-detecting device, and the temperature-detecting device setting exists
In the guider protective cover.
In above-mentioned technical proposal, temperature-detecting device can detect guider protection case temperature in real time, by temperature information
It is supplied to staff.
Further, which further includes controller, the controller and electric blower electricity
Connection, the controller is controlling being turned on and off for the electric blower.
Based on above-mentioned second purpose, a kind of sounding rocket provided by the utility model emits transport vehicle, including car body, general
Docking platform, regulating device, guider, guider protective cover and at least one above-mentioned sounding rocket attemperator；
The car body includes driver's cabin and vehicle frame, and the general docking platform is arranged on the vehicle frame, the guider
It is arranged in the guider protective cover, the guider protective cover is flexibly connected with the general docking platform, the adjusting
Device is separately connected the guider protective cover and the general docking platform, and guider protection can be adjusted by regulating device
The lifting action of cover, the electric blower are arranged on the vehicle frame.
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.
In above-mentioned technical proposal, transmitting holder plays the role of the Auxiliary support to guider protective cover, can share adjusting
The pressure that device is subject to extends the service life of regulating device.
Using above-mentioned technical proposal, sounding rocket attemperator provided by the utility model has the characteristics that：
Electric blower includes shell and the air blower and electric heating mechanism that are arranged in the shell, the electrical heating
The air outlet of the air blower described in face is arranged in mechanism, and the air of the air blower output passes through institute after electric heating mechanism heats
Ventilation shaft is stated to be delivered to inside guider protective cover.
In above-mentioned technical proposal, for air blower to output gas flow, the air outlet in air blower, air blast is arranged in electric heating mechanism
The air-flow of machine output is input to by ventilation shaft in guider protective cover by forming hot wind after air blower, anti-to guider
Rocket carries out heating and thermal insulation in shield, it is ensured that sonde battery can work normally under low temperature environment.
Sounding rocket transmitting transport vehicle provided by the utility model uses above-mentioned sounding rocket attemperator, and having should
The These characteristics of sounding rocket attemperator.
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 sounding rocket attemperator that the utility model embodiment one provides；
Fig. 2 is the structural representation of electric blower in the sounding rocket attemperator that the utility model embodiment one provides
Figure.
Fig. 3 is the control principle drawing for the sounding rocket attemperator that the utility model embodiment one provides；
Fig. 4 is the structural schematic diagram that the sounding rocket that the utility model embodiment two provides emits transport vehicle.
Reference numeral：
100- guider protective covers；110- air outlets；120- air inlets；130- debugging operations hole；140- debugging operations framves；
200- electric blowers；300- ventilation shafts；210- shells；220- air blowers；230- electric heating mechanisms；10- driver's cabins；20-
Vehicle frame；The general docking platforms of 30-；40- regulating devices；50- sounding rocket attemperators；60- is for electric installation；70- emits holder.
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 sounding rocket attemperator that the utility model embodiment provides；Fig. 2 shows
In the sounding rocket attemperator that the utility model embodiment provides, the structural schematic diagram of protective device；Fig. 3 shows the sides Fig. 2
View；Fig. 4 show the utility model embodiment provide sounding rocket attemperator in, the structural representation of leveling support device
Figure.
Embodiment one
Referring to Fig.1 and 2, sounding rocket attemperator provided by the utility model, including electric blower 200 and logical
Wind pipeline 300.
Electric blower 200 includes shell 210 and the air blower 220 and electric heating mechanism that are arranged in shell 210
230, the air outlet in face air blower 220 is arranged in electric heating mechanism 230, and the air that air blower 220 exports is through electric heating mechanism
It is delivered to inside guider protective cover 100 by ventilation shaft 300 after 230 heating.
In above-mentioned technical proposal, going out in air blower 220 is arranged to output gas flow, electric heating mechanism 230 in air blower 220
Air port, the air-flow that air blower 220 exports is input to guider by forming hot wind after air blower 220, by ventilation shaft 300 to be prevented
In shield 100, heating and thermal insulation is carried out to rocket in guider protective cover 100, it is ensured that sonde battery can be just under low temperature environment
Often work.
In one preferred embodiment, guider protective cover 100 is loading guider and rocket, guider protective cover
100 preferably use wave transparent thermal insulation material to manufacture, for example, it may be the materials such as fiberglass.
Guider protective cover 100 has air outlet 110 and air inlet 120；Electric blower 200 passes through ventilation shaft 300
It is connected to air inlet 120, to convey hot gas into guider protective cover 100, air outlet 110 then protects guider is discharged
Air in cover 100.
In above-mentioned technical proposal, guider protective cover 100 plays the protective effect to guider and rocket, electric blower
200 can be passed through hot gas by ventilation shaft 300 into guider protective cover 100, be carried to rocket in guider protective cover 100
Sonde battery carry out heating and thermal insulation, it is ensured that sonde battery can work normally under low temperature environment.
In one preferred embodiment, air inlet that ventilation shaft 300 passes through quick connector and guider protective cover 100
120 connections, the purpose connected using quick connector is that being adjusted in guider protective cover 100 can be quickly when vertical state is
Ventilation shaft 300 is disengaged, to not interfere with the transmitting of rocket.
In one preferred embodiment, electric heating mechanism 230 includes infrared electric heating tube.Infrared electric heating tube has structure letter
It is single, fever is fast, the characteristics of being easily installed and safeguarding.
In one preferred embodiment, air outlet 110 is arranged in guider protective cover 100 by the position of front end, into
Air port 120 is arranged in the position close to middle rear end of guider protective cover 100.
In above-mentioned technical proposal, air outlet 110 and air inlet 120 are successively set on leaning on nearby for guider protective cover 100
It holds, the position of middle rear end, can ensure flowing stroke of the thermal current in guider protective cover 100, to protect guider
The sonde battery of rocket and its carrying in cover 100 is in stable temperature environment.
In one preferred embodiment, 100 upper end of guider protective cover has debugging operations hole 130.The debugging operations hole
130 play technical staff are facilitated to be switched to devices such as power supplys in guider protective cover 100 or maintenance work.
Further include debugging operations frame 140 in one preferred embodiment, the setting of debugging operations frame 140 is protected in guider
On cover 100, debugging operations frame 140 can be moved along 100 length direction of guider protective cover.
In above-mentioned technical proposal, debugging operations frame 140 plays the role of carrying staff, is grasped to debugging convenient for staff
Make the equipment such as 130 interior power of hole to be manipulated.
Please refer to Fig. 3, in a preferred embodiment, which further includes temperature-detecting device, temperature
Detection device is spent to be arranged in guider protective cover 100 and (in figure do not illustrate).
In above-mentioned technical proposal, temperature-detecting device can detect temperature in guider protective cover 100 in real time, and temperature is believed
Breath is supplied to staff.
Please refer to Fig. 3, in a preferred embodiment, which further includes controller, controller with
Electric blower 200 is electrically connected, and controller is controlling being turned on and off for electric blower 200.Also, the controller also with
Temperature-detecting device is electrically connected, to receive the temperature signal of temperature-detecting device transmission.
Intelligence is realized to the temperature in temperature guider protective cover 100 when it is implemented, can be realized using the controller
Control.
Such as：When the temperature in guider protective cover 100 is too low, temperature signal is transferred to control by temperature sensor
Device, controller is interior to have preset temperature threshold, and since temperature signal numerical value is less than the threshold value, controller output order makes air blower
220 and infrared electric heating tube be powered, to make in guider protective cover 100 temperature be promoted.
When temperature is within the scope of preset temperature threshold in guider protective cover 100, air blower 220 and infrared electric heating tube are not
Work.
When temperature is excessively high in guider protective cover 100, is more than preset temperature threshold range in controller, controller output
Instruction control air blower 220 is powered, and infrared electric heating tube no power can increase the flowing of 100 interior air-flow of guider protective cover at this time,
Play certain cooling effect.
Embodiment two
Fig. 4 is please referred to, a kind of sounding rocket transmitting transport vehicle is present embodiments provided comprising car body, general docking are flat
The sounding rocket that platform 30, regulating device 40, guider, guider protective cover 100 and at least one above-described embodiment one provide
Attemperator 50.
Car body includes driver's cabin 10 and vehicle frame 20, and general docking platform 30 is arranged on vehicle frame 20, and guider setting is being led
Into device protective cover 100, guider protective cover 100 is flexibly connected with general docking platform 30, and regulating device 40, which is separately connected, to be led
To device protective cover 100 and general docking platform 30, the lifting that guider protective cover 100 can be adjusted by regulating device 40 is dynamic
Make, electric blower 200 is arranged on vehicle frame 20.
Further include for electric installation 60, this includes accumulator group and oil machine (bavin Water Oil Or Gas hair for electric installation when concrete application
Motor).Accumulator group and oil machine are separately positioned on vehicle frame 20, accumulator and oil machine respectively with infrared electric heating tube and air blower
220 electrical connections, in use, low temperature (- 10 DEG C or less) weather is met, it should be infrared using oil start 12 hours before rocket launching
Electrothermal tube and air blower 220 take heating and thermal insulation measure to rocket, by transfer guard station to launching site driving process, Ke Yigai
It is powered for accumulator group.
In one preferred embodiment, sounding rocket transmitting transport vehicle further includes transmitting holder 70,70 bottom of transmitting holder
End is connect with vehicle frame 20, and transmitting upper end is to support guide protective cover 100.
In above-mentioned technical proposal, transmitting holder 70 plays the role of the Auxiliary support to guider protective cover 100, can share
The pressure that regulating device 40 is subject to extends the service life of regulating device 40.
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 attemperator, which is characterized in that including：Electric blower and ventilation shaft；The hair dryer dress
It sets including shell and the air blower and electric heating mechanism that are arranged in the shell, the electric heating mechanism is arranged in face institute
The air outlet of air blower is stated, the air of the air blower output is delivered to after electric heating mechanism heats by the ventilation shaft
Inside guider protective cover.
2. sounding rocket attemperator according to claim 1, which is characterized in that the guider protective cover is loading
Guider and rocket, the guider protective cover have air outlet and air inlet；The electric blower by ventilation shaft with
The air inlet connection, to convey hot gas into the guider protective cover.
3. sounding rocket attemperator according to claim 2, which is characterized in that the electric heating mechanism includes infrared electricity
Heat pipe.
4. sounding rocket attemperator according to claim 2, which is characterized in that the air outlet is arranged in the guiding
Device protective cover by the position of front end, the position close to middle rear end in the guider protective cover is arranged in the air inlet.
5. sounding rocket attemperator according to claim 2, which is characterized in that guider protective cover upper end has
Debugging operations hole.
6. sounding rocket attemperator according to claim 2, which is characterized in that further include debugging operations frame, the tune
It tries crosshead to be arranged on the guider protective cover, the debugging operations frame can be moved along guider protective cover length direction
It is dynamic.
7. according to claim 2-6 any one of them sounding rocket attemperators, which is characterized in that further include temperature detection dress
It sets, the temperature-detecting device is arranged in the guider protective cover.
8. sounding rocket attemperator according to claim 7, which is characterized in that further include controller, the controller
It is electrically connected with the electric blower, the controller is controlling being turned on and off for the electric blower.
9. a kind of sounding rocket emits transport vehicle, which is characterized in that including car body, general docking platform, regulating device, guiding
Device, guider protective cover and at least one claim 1-8 any one of them sounding rocket attemperator；
The car body includes driver's cabin and vehicle frame, and the general docking platform is arranged on the vehicle frame, the guider setting
In the guider protective cover, the guider protective cover is flexibly connected with the general docking platform, the regulating device
It is separately connected the guider protective cover and the general docking platform, the electric blower is arranged on the vehicle frame.
10. sounding rocket according to claim 9 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.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820288150.0U CN207955443U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket attemperator and sounding rocket emit transport vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820288150.0U CN207955443U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket attemperator and sounding rocket emit transport vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN207955443U true CN207955443U (en) | 2018-10-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820288150.0U Active CN207955443U (en) | 2018-03-01 | 2018-03-01 | Sounding rocket attemperator and sounding rocket emit transport vehicle |
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| Country | Link |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111077818A (en) * | 2019-12-05 | 2020-04-28 | 江西洪都航空工业集团有限责任公司 | Control box for aircraft data forwarding and transmitting control |
| CN112082435A (en) * | 2020-09-21 | 2020-12-15 | 北京中科宇航技术有限公司 | Rocket final repair heat preservation device |
-
2018
- 2018-03-01 CN CN201820288150.0U patent/CN207955443U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111077818A (en) * | 2019-12-05 | 2020-04-28 | 江西洪都航空工业集团有限责任公司 | Control box for aircraft data forwarding and transmitting control |
| CN112082435A (en) * | 2020-09-21 | 2020-12-15 | 北京中科宇航技术有限公司 | Rocket final repair heat preservation device |
| CN112082435B (en) * | 2020-09-21 | 2022-02-08 | 北京中科宇航技术有限公司 | Rocket final repair heat preservation device |
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