CN207748015U - A kind of double unmanned planes promoting cruising ability - Google Patents
A kind of double unmanned planes promoting cruising ability Download PDFInfo
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- CN207748015U CN207748015U CN201721841323.9U CN201721841323U CN207748015U CN 207748015 U CN207748015 U CN 207748015U CN 201721841323 U CN201721841323 U CN 201721841323U CN 207748015 U CN207748015 U CN 207748015U
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- cycle engine
- variable cycle
- double
- inner shaft
- shaft lever
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Abstract
The utility model discloses a kind of double unmanned planes promoting cruising ability, structure includes：Variable cycle engine,Wireless Transmitter the cover,Rotor wing bracket arm,Propeller aircraft cap,Rotor inner shaft lever,Double-axis transmission wheel,Shock-proof spring pipe,Support heel slab,Aerial camera,Proximity sensor,Propeller aircraft cap is horizontally installed on rotor inner shaft lever and using mechanical connection,Double-axis transmission wheel,Shock-proof spring pipe is all provided with there are two and is vertically arranged to respectively at left and right sides of variable cycle engine,Wireless Transmitter the cover is horizontally installed to variable cycle engine both sides up and down respectively with proximity sensor,The utility model variable cycle engine is equipped with wireless transmission plate,Variable cycle engine body,Motor distribution geosynclinal block,Become circulation rotating kettle,Realize the change loop structure high efficient and flexible for the double unmanned planes for promoting cruising ability,The cruising ability of engine changes with tactic pattern,Coordinate the body most efficient degree that efficiently continuation of the journey and real-time guarantees fly.
Description
Technical field
The utility model is a kind of double unmanned planes promoting cruising ability, belongs to unmanned plane equipment technical field.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer.Compared with manned aircraft, nobody
Machine is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane press application field, can be divided into it is military with it is civilian.
Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application, which is unmanned plane, really just have been needed；
At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping,
The application in news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded unmanned plane itself
Purposes, developed country also actively extension sector application with development unmanned air vehicle technique.
But the flight performance height of prior art unmanned plane is not enough to cope with various climatic conditions, and stability is poor, flight
Pattern fix and can not flexible cooperation flight, be not achieved promoted continuation of the journey effect again can not real-time high-efficiency fly.
Utility model content
In view of the deficienciess of the prior art, the utility model aim be to provide it is a kind of promoted cruising ability it is double nobody
Machine, the flight performance height to solve unmanned plane are but not enough to cope with various climatic conditions, and stability is poor, offline mode fix and
Can not flexible cooperation flight, be not achieved promoted continuation of the journey effect again can not real-time high-efficiency flight the problem of.
To achieve the goals above, the utility model is to realize by the following technical solutions：A kind of promotion continuation of the journey energy
Double unmanned planes of power, structure include：Variable cycle engine, Wireless Transmitter the cover, rotor wing bracket arm, propeller aircraft cap,
Rotor inner shaft lever, Double-axis transmission wheel, shock-proof spring pipe, support heel slab, aerial camera, proximity sensor, the rotor spiral shell
Rotation spinner is horizontally installed on rotor inner shaft lever and using mechanical connection, the Double-axis transmission wheel, shock-proof spring pipe are equipped with
It two and is vertically arranged to respectively at left and right sides of variable cycle engine, the Wireless Transmitter the cover is distinguished with proximity sensor
Variable cycle engine both sides up and down are horizontally installed to, the variable cycle engine is horizontally installed to Wireless Transmitter the cover and approaches
It is connect by Double-axis transmission wheel mechanical between sensor and with propeller aircraft cap, rotor inner shaft lever, the support heel slab
Under rotor wing bracket arm, the rotor wing bracket arm is equipped with two or more with support heel slab and is sent out with cycle is become oblique weld
Motivation is around connection, and the aerial camera is vertically arranged between two support heel slabs, and the variable cycle engine is equipped with
It is wirelessly transferred plate, variable cycle engine body, motor distribution geosynclinal block, becomes circulation rotating kettle, the wireless transmission plate level is tightly attached to
It is electrically connected on variable cycle engine body and with motor distribution geosynclinal block by conducting wire, the motor distribution geosynclinal block is welded on change vertically
On the right side of cycle engine body, the change circulation rotating kettle is installed vertically under variable cycle engine body and uses mechanical connection,
The variable cycle engine body be horizontally installed between Wireless Transmitter the cover and proximity sensor and with propeller aircraft cap,
Rotor inner shaft lever is connected by Double-axis transmission wheel mechanical.
Further, the propeller aircraft cap is conllinear with the axle center of rotor inner shaft lever.
Further, the aerial camera is connect with proximity sensor by conductor signal.
Further, the rotor inner shaft lever is mutually parallel with shock-proof spring pipe.
Further, the convex block of the groove and rotor inner shaft lever of the propeller aircraft cap is gap-matched.
Further, the variable cycle engine is mechanical part, and transformation different mode structure is continued a journey and coordinated various
Situation is efficiently flown.
Further, the shock-proof spring pipe is spring members, and elasticity is big, and buffering is strong, and shock-absorbing is efficient.
Advantageous effect
The utility model variable cycle engine is equipped with wireless transmission plate, variable cycle engine body, motor distribution geosynclinal block, becomes
Circulation rotating kettle realizes the change loop structure high efficient and flexible for the double unmanned planes for promoting cruising ability, the cruising ability of engine
As tactic pattern changes, the cooperation body most efficient degree that efficiently continuation of the journey and real-time guarantees fly.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram for the double unmanned planes promoting cruising ability of the utility model.
Fig. 2 is a kind of cross-sectional view for the double unmanned planes promoting cruising ability of the utility model.
Fig. 3 is a kind of cross-section structure signal of double unmanned plane variable cycle engines promoting cruising ability of the utility model
Figure.
In figure：Variable cycle engine -1, Wireless Transmitter the cover -2, rotor wing bracket arm -3, propeller aircraft cap -4, rotor
Inner shaft lever -5, Double-axis transmission wheel -6, shock-proof spring pipe -7, support heel slab -8, aerial camera -9, proximity sensor -10, nothing
Line transmission board -100, motor distribution geosynclinal block -102, becomes circulation rotating kettle -103 at variable cycle engine body -101.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below
In conjunction with specific implementation mode, the utility model is expanded on further.
- Fig. 3 is please referred to Fig.1, the utility model provides a kind of double unmanned planes promoting cruising ability：Its structure includes：Become
Cycle engine 1, Wireless Transmitter the cover 2, rotor wing bracket arm 3, propeller aircraft cap 4, rotor inner shaft lever 5, Double-axis transmission wheel
6, shock-proof spring pipe 7, support heel slab 8, aerial camera 9, proximity sensor 10, the propeller aircraft cap 4 are horizontally mounted
In on rotor inner shaft lever 5 and using mechanical connection, the Double-axis transmission wheel 6, shock-proof spring pipe 7 are all provided with there are two and distinguish
It is vertically arranged to 1 left and right sides of variable cycle engine, the Wireless Transmitter the cover 2 is horizontally mounted respectively with proximity sensor 10
In about 1 both sides of variable cycle engine, the variable cycle engine 1 is horizontally installed to Wireless Transmitter the cover 2 and close sensing
It is mechanically connected by Double-axis transmission wheel 6 between device 10 and with propeller aircraft cap 4, rotor inner shaft lever 5, the support heel slab
Under rotor wing bracket arm 3, the rotor wing bracket arm 3 is equipped with two or more with support heel slab 8 and is followed with change 8 oblique welds
Around connection, the aerial camera 9 is vertically arranged between two support heel slabs 8 ring engine 1, and the change cycle is started
Machine 1 is equipped with wireless transmission plate 100, variable cycle engine body 101, motor distribution geosynclinal block 102, becomes circulation rotating kettle 103, the nothing
100 level of line transmission board is tightly attached on variable cycle engine body 101 and is electrically connected by conducting wire with motor distribution geosynclinal block 102,
The motor distribution geosynclinal block 102 is welded on 101 right side of variable cycle engine body vertically, and the change circulation rotating kettle 103 is vertically pacified
Loaded on variable cycle engine body 101 times and using mechanical connection, the variable cycle engine body 101 is horizontally installed to wirelessly pass
Pass through 6 machinery of Double-axis transmission wheel between defeated device the cover 2 and proximity sensor 10 and with propeller aircraft cap 4, rotor inner shaft lever 5
Connection, the propeller aircraft cap 4 is conllinear with the axle center of rotor inner shaft lever 5, and the aerial camera 9 is logical with proximity sensor 10
Cross conductor signal connection, the rotor inner shaft lever 5 is mutually parallel with shock-proof spring pipe 7, the groove of the propeller aircraft cap 4 and
The convex block of rotor inner shaft lever 5 is gap-matched, and the variable cycle engine 1 is mechanical part, and transformation different mode structure is continuous
It navigates and various situations is coordinated efficiently to fly, the shock-proof spring pipe 7 is spring members, and elasticity is big, and buffering is strong, and shock-absorbing is efficient.
During promoting the use of double unmanned planes of cruising ability, pass through the wireless transmission plate of variable cycle engine 1
100, variable cycle engine body 101, motor distribution geosynclinal block 102, change circulation rotating kettle 103 coordinate during wireless transmission adjusts
Whole propeller aircraft cap 4, rotor inner shaft lever 5, Double-axis transmission wheel 6, shock-proof spring pipe 7 act pattern conversion continuation of the journey cycle high efficiency flying
Row, the change loop structure high efficient and flexible for the double unmanned planes for promoting cruising ability is reached by variable cycle engine 1, and engine continues
Boat ability changes with tactic pattern, the cooperation body most efficient degree that efficiently continuation of the journey and real-time guarantees fly.
Variable cycle engine 1 described in the utility model refers to passing through some of change engine on an engine
Geometry, size or the position of component utilize change varying cyclically to realize the gas-turbine unit of different thermodynamic cycles
Cycle of engine parameter can make engine in various work shapes such as pressure ratio, turbine inlet temperature, air mass flow and bypass ratio
It is all with good performance under state.
Its structure and principle, which are all this technology personnel, can be learnt by technical manual or be known by routine experiment method,
The utility model solves the problems, such as it is that the flight performance height of unmanned plane is but not enough to cope with various climatic conditions, and stability is poor,
Offline mode fix and can not flexible cooperation flight, be not achieved promoted continuation of the journey effect again can not real-time high-efficiency fly,
The utility model is combined with each other by above-mentioned component, and the change loop structure that can reach the double unmanned planes for promoting cruising ability is high
Effect is flexible, and the cruising ability of engine changes with tactic pattern, the efficiently continuation of the journey and real-time guarantees flight is most of cooperation body
Efficient degree, it is described in detail below：
100 level of wireless transmission plate is tightly attached on variable cycle engine body 101 and is led to motor distribution geosynclinal block 102
Conducting wire electrical connection is crossed, the motor distribution geosynclinal block 102 is welded on 101 right side of variable cycle engine body, the change cycle rotation vertically
Turn kettle 103 and is installed vertically on variable cycle engine body 101 times and using mechanical connection, 101 water of variable cycle engine body
Safety is loaded between Wireless Transmitter the cover 2 and proximity sensor 10 and passes through with propeller aircraft cap 4, rotor inner shaft lever 5
Double-axis transmission wheel 6 is mechanically connected.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (5)
1. a kind of double unmanned planes promoting cruising ability, structure include：Variable cycle engine（1）, Wireless Transmitter the cover
（2）, rotor wing bracket arm（3）, propeller aircraft cap（4）, rotor inner shaft lever（5）, Double-axis transmission wheel（6）, shock-proof spring pipe（7）、
Support heel slab（8）, aerial camera（9）, proximity sensor（10）, the propeller aircraft cap（4）It is horizontally installed to rotor
Inner shaft lever（5）Above and using mechanical connection, the Double-axis transmission wheel（6）, shock-proof spring pipe（7）There are two being all provided with and respectively
It is vertically arranged to variable cycle engine（1）The left and right sides, the Wireless Transmitter the cover（2）With proximity sensor（10）Water respectively
Safety is loaded on variable cycle engine（1）Upper and lower both sides, it is characterised in that：
The variable cycle engine（1）It is horizontally installed to Wireless Transmitter the cover（2）With proximity sensor（10）Between and with
Propeller aircraft cap（4）, rotor inner shaft lever（5）Pass through Double-axis transmission wheel（6）Mechanical connection, the support heel slab（8）It tilts
It is welded on rotor wing bracket arm（3）Under, the rotor wing bracket arm（3）With support heel slab（8）Be equipped with two or more and with change
Cycle engine（1）Around connection, the aerial camera（9）It is vertically arranged to two support heel slabs（8）Between；
The variable cycle engine（1）Equipped with wireless transmission plate（100）, variable cycle engine body（101）, motor distribution geosynclinal block
（102）, become circulation rotating kettle（103）, the wireless transmission plate（100）Level is tightly attached to variable cycle engine body（101）On simultaneously
And with motor distribution geosynclinal block（102）It is electrically connected by conducting wire, the motor distribution geosynclinal block（102）The vertical change cycle that is welded on is started
Body（101）Right side, the change circulation rotating kettle（103）It is installed vertically on variable cycle engine body（101）Down and use machine
Tool connects, the variable cycle engine body（101）It is horizontally installed to Wireless Transmitter the cover（2）With proximity sensor（10）Between
And with propeller aircraft cap（4）, rotor inner shaft lever（5）Pass through Double-axis transmission wheel（6）Mechanical connection.
2. a kind of double unmanned planes promoting cruising ability according to claim 1, it is characterised in that：The propeller aircraft
Cap（4）With rotor inner shaft lever（5）Axle center it is conllinear.
3. a kind of double unmanned planes promoting cruising ability according to claim 1, it is characterised in that：The aerial camera
（9）With proximity sensor（10）It is connected by conductor signal.
4. a kind of double unmanned planes promoting cruising ability according to claim 1, it is characterised in that：The rotor inner shaft lever
（5）With shock-proof spring pipe（7）It is mutually parallel.
5. a kind of double unmanned planes promoting cruising ability according to claim 1, it is characterised in that：The propeller aircraft
Cap（4）Groove and rotor inner shaft lever（5）Convex block be gap-matched.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721841323.9U CN207748015U (en) | 2017-12-24 | 2017-12-24 | A kind of double unmanned planes promoting cruising ability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721841323.9U CN207748015U (en) | 2017-12-24 | 2017-12-24 | A kind of double unmanned planes promoting cruising ability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207748015U true CN207748015U (en) | 2018-08-21 |
Family
ID=63150543
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721841323.9U Expired - Fee Related CN207748015U (en) | 2017-12-24 | 2017-12-24 | A kind of double unmanned planes promoting cruising ability |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207748015U (en) |
-
2017
- 2017-12-24 CN CN201721841323.9U patent/CN207748015U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190426 Address after: Pavement No.1 and No.2 on the second floor of the house north of No.5 Changhu Road, Qingxiu District, Nanning City, Guangxi Zhuang Autonomous Region Patentee after: Guangxi Daxiong Eagle Technology Co., Ltd. Address before: 311300 Science and Technology Business Incubation Base B Building 337, No. 1079 Wusu Street, Jinbei Street, Linan District, Hangzhou City, Zhejiang Province Patentee before: Know and (Hangzhou) Technology Co., Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180821 Termination date: 20191224 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |