CN205615733U - A fixed wing uavs jettison device for low temperature environment - Google Patents
A fixed wing uavs jettison device for low temperature environment Download PDFInfo
- Publication number
- CN205615733U CN205615733U CN201620355024.3U CN201620355024U CN205615733U CN 205615733 U CN205615733 U CN 205615733U CN 201620355024 U CN201620355024 U CN 201620355024U CN 205615733 U CN205615733 U CN 205615733U
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- Prior art keywords
- hot
- hot blast
- aerial vehicle
- unmanned aerial
- blast
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- 230000005540 biological transmission Effects 0.000 claims abstract description 14
- 230000001681 protective effect Effects 0.000 claims description 3
- 235000017166 Bambusa arundinacea Nutrition 0.000 abstract 3
- 235000017491 Bambusa tulda Nutrition 0.000 abstract 3
- 241001330002 Bambuseae Species 0.000 abstract 3
- 235000015334 Phyllostachys viridis Nutrition 0.000 abstract 3
- 239000011425 bamboo Substances 0.000 abstract 3
- 238000009423 ventilation Methods 0.000 abstract 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 210000003205 muscle Anatomy 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model relates to a fixed wing uavs jettison device for low temperature environment, including support frame and launching cradle, be equipped with the rubber rubber band on the launching cradle, be equipped with the hot -blast device that blows below the launching cradle, the hot -blast device that blows includes generator, air heater, hot -blast transmission pipe, the hot -blast section of thick bamboo of dispersing, the air heater is connected to the generator, and the air heater is connected through a hot -blast transmission pipe and the hot -blast section of thick bamboo of dispersing, and the hot -blast section of thick bamboo of dispersing sets up in the rubber rubber band below of launching cradle, a hot -blast last interval setting ventilation holes that disperses. The utility model is suitable for a low temperatures in the winter uses down, has solved the problem that unmanned aerial vehicle can't take off winter. Optimize the unmanned aerial vehicle utilization ratio, improve unmanned aerial vehicle operation level.
Description
Technical field
This utility model relates to a kind of fixed-wing unmanned aerial vehicle ejecting device for low temperature environment.
Background technology
The mode of taking off that fixed-wing unmanned plane uses at present is catapult-assisted take-off, and it is that rubber rubber band launches that ejection system uses, but
In the environment of high and cold, rubber rubber band is stretched to routine when launching length, launches strength and can weaken, along with the reduction of temperature, bullet
Power attenuation degree can be deepened.Liaoning Area winter is cold, temperature on average below-10 DEG C, under such environment fixed-wing without
Man-machine cannot use at all.Now need to study a kind of low temperature environment fixed-wing unmanned aerial vehicle ejecting device to solve fixed-wing unmanned plane
The problem that cannot use in the winter time.
Summary of the invention
Technical problem to be solved in the utility model is to provide a kind of fixed-wing unmanned aerial vehicle ejecting device for low temperature environment,
The problem solving to use unmanned plane winter.
For achieving the above object, this utility model realizes by the following technical solutions:
A kind of fixed-wing unmanned aerial vehicle ejecting device for low temperature environment, including bracing frame and launching cradle, launching cradle is provided with rubber
Rubber muscle, is provided with heater blower unit below launching cradle, and described heater blower unit includes electromotor, hot-air blower, hot blast
Transmission pipe, hot blast dissipate cylinder, and described electromotor connects hot-air blower, and hot-air blower dissipates cylinder by hot blast transmission pipe with hot blast and is connected,
Hot blast dissipates cylinder and is arranged on below the rubber rubber band of launching cradle, and hot blast dissipates interval on cylinder and arranges transmission air holes.
It is cylinder or square tube that described hot blast dissipates cylinder.
Described hot blast transmission pipe is hot blast flexible pipe.
Described fixed-wing unmanned aerial vehicle ejecting device also includes the protective cover setting launching cradle for cover.
Compared with prior art, the beneficial effects of the utility model are:
This utility model is applicable under winter low temperature use, and solves the problem that winter, unmanned plane cannot take off.Optimize unmanned plane
Utilization rate, improves unmanned plane level of operation.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
In figure: 1-bracing frame, 2-launching cradle, 3-rubber rubber band, 4-electromotor, 5-hot-air blower, 6-hot blast transmission pipe,
7-hot blast dissipates cylinder, 8-sends air holes
Detailed description of the invention
Below in conjunction with the accompanying drawings detailed description of the invention of the present utility model is further illustrated:
Such as Fig. 1, a kind of fixed-wing unmanned aerial vehicle ejecting device for low temperature environment, including bracing frame 1 and launching cradle 2, bullet
Penetrating frame 2 and be provided with rubber rubber band 3, be provided with heater blower unit below launching cradle 2, described heater blower unit includes sending out
Motor 4, hot-air blower 5, hot blast transmission pipe 6, hot blast dissipate cylinder 7, and described electromotor 4 connects hot-air blower 5, hot-air blower 5
Dissipating cylinder 7 by hot blast transmission pipe 6 with hot blast to be connected, hot blast transmission pipe 6 is hot blast flexible pipe.Hot blast dissipates cylinder 7 and is arranged on
Below the rubber rubber band 3 of launching cradle 2, it is cylinder or square tube that hot blast dissipates cylinder 7, and hot blast dissipates interval on cylinder 7 and arranges transmission
Air holes 8.
Fixed-wing unmanned aerial vehicle ejecting device also includes the protective cover setting launching cradle for cover.
Described above is only ultimate principle of the present utility model, not imposes any restrictions this utility model, every according to this reality
It is carried out equivalent variations and modification, all within the category of the art of this patent protection scheme with novel.
Claims (4)
1., for a fixed-wing unmanned aerial vehicle ejecting device for low temperature environment, including bracing frame and launching cradle, launching cradle sets
Having rubber rubber band, it is characterised in that be provided with heater blower unit below launching cradle, described heater blower unit includes generating
Machine, hot-air blower, hot blast transmission pipe, hot blast dissipate cylinder, and described electromotor connects hot-air blower, and hot-air blower is by hot blast transmission pipe
Dissipating cylinder with hot blast to be connected, hot blast dissipates cylinder and is arranged on below the rubber rubber band of launching cradle, and hot blast dissipates interval setting on cylinder and sends out
Wind pushing hole.
A kind of fixed-wing unmanned aerial vehicle ejecting device for low temperature environment the most according to claim 1, it is characterised in that
It is cylinder or square tube that described hot blast dissipates cylinder.
A kind of fixed-wing unmanned aerial vehicle ejecting device for low temperature environment the most according to claim 1, it is characterised in that
Described hot blast transmission pipe is hot blast flexible pipe.
A kind of fixed-wing unmanned aerial vehicle ejecting device for low temperature environment the most according to claim 1, it is characterised in that
Described fixed-wing unmanned aerial vehicle ejecting device also includes the protective cover setting launching cradle for cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620355024.3U CN205615733U (en) | 2016-04-22 | 2016-04-22 | A fixed wing uavs jettison device for low temperature environment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620355024.3U CN205615733U (en) | 2016-04-22 | 2016-04-22 | A fixed wing uavs jettison device for low temperature environment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205615733U true CN205615733U (en) | 2016-10-05 |
Family
ID=57028078
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620355024.3U Active CN205615733U (en) | 2016-04-22 | 2016-04-22 | A fixed wing uavs jettison device for low temperature environment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205615733U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005467A (en) * | 2016-08-01 | 2016-10-12 | 天峋（常州）智能科技有限公司 | Small fixed wing unmanned aerial vehicle ejector rack |
-
2016
- 2016-04-22 CN CN201620355024.3U patent/CN205615733U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005467A (en) * | 2016-08-01 | 2016-10-12 | 天峋（常州）智能科技有限公司 | Small fixed wing unmanned aerial vehicle ejector rack |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |