CN108116651A - It is a kind of that there is the unmanned plane of Anti-bumping protection - Google Patents
It is a kind of that there is the unmanned plane of Anti-bumping protection Download PDFInfo
- Publication number
- CN108116651A CN108116651A CN201711498119.6A CN201711498119A CN108116651A CN 108116651 A CN108116651 A CN 108116651A CN 201711498119 A CN201711498119 A CN 201711498119A CN 108116651 A CN108116651 A CN 108116651A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- supporting rod
- casing
- wing
- energy dissipating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000013016 damping Methods 0.000 claims description 16
- 230000007246 mechanism Effects 0.000 claims description 6
- 230000006870 function Effects 0.000 abstract description 6
- 230000009286 beneficial effect Effects 0.000 abstract description 3
- 230000035939 shock Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 208000027418 Wounds and injury Diseases 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 208000014674 injury Diseases 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
There is the unmanned plane of Anti-bumping protection the invention discloses a kind of; including unmanned plane body, supporting rod and wing; unmanned plane casing is packaged on the outside of the unmanned plane body; and it is provided with anticollision device, collision-prevention device on the outside of unmanned plane casing; the unmanned plane body is internally provided with radiator; and the upper and lower ends of unmanned plane body offer air outlet and air inlet respectively, the supporting rod is connected by folding support member with unmanned plane casing, and the wing is connected by hinge component with unmanned plane casing.This has the function of the unmanned plane of Anti-bumping protection; supporting rod and wing can be folded by folding support member and hinge component; the memory space of the unmanned plane can be reduced; and it is carried convenient for user; radiator is mounted on the inside of unmanned plane body; beneficial to the heat generated when distributing this body running of unmanned plane, anticollision device, collision-prevention device is arranged on the outside of unmanned plane casing, is conducive to buffer the shock strength between external object and unmanned plane body and energy dissipating.
Description
Technical field
It is specially a kind of that there is the unmanned plane of Anti-bumping protection the present invention relates to unmanned air vehicle technique field.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned vehicle that presetting apparatus manipulates, unmanned plane is actually the general designation of unmanned vehicle, with manned aircraft
It compares, it has many advantages, such as small, low cost, easy to use, low to operational environment requirement, battlefield survival is stronger, because
Utilization of this unmanned plane in modern development is extremely wide, but the unmanned plane used at present does not possess the function of folding, inconvenient
In storage of the user to unmanned plane, while do not possess collision prevention function, be unfavorable for increasing the service life of unmanned plane.
The content of the invention
There is the unmanned plane of Anti-bumping protection it is an object of the invention to provide a kind of, to solve in above-mentioned background technology
The unmanned plane used at present proposed does not possess the function of folding, storage of the person of being not convenient to use to unmanned plane, while does not possess
Collision prevention function, the problem of being unfavorable for increasing the service life of unmanned plane.
To achieve the above object, the present invention provides following technical solution：It is a kind of that there is the unmanned plane of Anti-bumping protection, bag
Unmanned plane body, supporting rod and wing are included, is packaged with unmanned plane casing on the outside of the unmanned plane body, and unmanned plane casing
Outside is provided with anticollision device, collision-prevention device, and the unmanned plane body is internally provided with radiator, and the upper and lower ends of unmanned plane body
Air outlet and air inlet are offered respectively, and the supporting rod is connected by folding support member with unmanned plane casing, and the wing leads to
Hinge component is crossed to be connected with unmanned plane casing.
Preferably, the anticollision device, collision-prevention device includes the first elastic energy dissipating layer, the first damping spring, the second elastic energy dissipating layer and the
Two damping springs, and the inside of the first elastic energy dissipating layer is equipped with the first damping spring, the inner ring of the first elastic energy dissipating layer is set
There is the second elastic energy dissipating layer, the inside of the second elastic energy dissipating layer is equipped with the second damping spring.
Preferably, the radiator includes heat-dissipating pipe, the first radiating fin and the second radiating fin, and the one of heat-dissipating pipe
End is equipped with the first radiating fin, and the other end of the first radiating fin is connected with the second radiating fin.
Preferably, the supporting rod and folding support member form fold mechanism, and supporting rod is mounted on nobody at equal intervals
The downside of machine casing.
Preferably, the supporting rod is arc-shaped structure, and post upper curved bend curvature is less than supporting rod lower end arc
Shape curvature.
Preferably, the wing and hinge component form fold mechanism, and are flexible connection between wing and hinge component.
Compared with prior art, the beneficial effects of the invention are as follows：This has the function of the unmanned plane of Anti-bumping protection, passes through folding
Supporting item and hinge component can fold supporting rod and wing, can reduce the memory space of the unmanned plane, and be convenient for
User carries, and radiator is mounted on the inside of unmanned plane body, is conducive to distribute the heat generated during this body running of unmanned plane
Amount, avoids impacting because of the excessive parts to unmanned plane body interior of heat, is conducive to increase the use year of the unmanned plane
Limit, anticollision device, collision-prevention device is arranged on the outside of unmanned plane casing, when extraneous object is bumped against on the unmanned plane, is conducive to extraneous object
The injury of body and unmanned plane is preferably minimized, and is conducive to buffer the shock strength between external object and unmanned plane body
And energy dissipating, the exchange being provided with beneficial to air of air inlet and air outlet can avoid the inside of unmanned plane body from high temperature occur
Situation.
Description of the drawings
Fig. 1 is positive structure diagram of the present invention；
Fig. 2 is supporting rod of the present invention and folding support member attachment structure schematic diagram；
Fig. 3 is anticollision device, collision-prevention device structure diagram of the present invention
Fig. 4 is construction for heat radiating device schematic diagram of the present invention.
In figure：1st, unmanned plane body, 2, unmanned plane casing, 3, anticollision device, collision-prevention device, the 301, first elastic energy dissipating layer, 302, first
Damping spring, the 303, second elastic energy dissipating layer, the 304, second damping spring, 4, radiator, 401, heat-dissipating pipe, 402, first dissipates
Hot fin, the 403, second radiating fin, 5, air inlet, 6, air outlet, 7, supporting rod, 8, folding support member, 9, wing, 10, hinge
Chain component.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other without making creative work
Embodiment belongs to the scope of protection of the invention.
- 4 are please referred to Fig.1, the present invention provides a kind of technical solution：It is a kind of that there is the unmanned plane of Anti-bumping protection, including
Unmanned plane body 1, unmanned plane casing 2, anticollision device, collision-prevention device 3, radiator 4, air inlet 5, air outlet 6, supporting rod 7, folding support
Part 8, wing 9 and hinge component 10, the outside of unmanned plane body 1 are packaged with unmanned plane casing 2, and the outside of unmanned plane casing 2
Anticollision device, collision-prevention device 3 is provided with, anticollision device, collision-prevention device 3 includes the first elastic energy dissipating layer 301, first the 302, second elastic energy dissipating layer of damping spring
303 and second damping spring 304, and the inside of the first elastic energy dissipating layer 301 is equipped with the first damping spring 302, the first elasticity
The inner ring of energy dissipating layer 301 is provided with the second elastic energy dissipating layer 303, and the inside of the second elastic energy dissipating layer 303 is equipped with the second damping
Spring 304 when extraneous object is bumped against on unmanned plane body 1, is conducive to hitting between external object and unmanned plane body 1
Strength is hit into row buffering and energy dissipating, unmanned plane body 1 is internally provided with radiator 4, and the upper and lower ends of unmanned plane body 1
Air outlet 6 and air inlet 5 are offered respectively, and radiator 4 includes heat-dissipating pipe 401, the first radiating fin 402 and the second heat radiating fin
Piece 403, and one end of heat-dissipating pipe 401 is equipped with the first radiating fin 402, the other end of the first radiating fin 402 is connected with
Two radiating fins 403 are conducive to distribute the heat generated when unmanned plane body 1 works, and heat dissipation effect is splendid, and supporting rod 7 is logical
Folding support member 8 to be crossed to be connected with unmanned plane casing 2, supporting rod 7 and folding support member 8 form fold mechanism, and between 7 grade of supporting rod
Away from mounted on the downside of unmanned plane casing 2, convenient for folding of the user to supporting rod 7, be conducive to reduce unmanned plane body 1
Placement space, supporting rod 7 is arc-shaped structure, and 7 upper end curved bend curvature of supporting rod is less than 7 lower end arc-shaped bend of supporting rod
Degree plays an important role of to guide air-flow, be conducive to keep stability during unmanned plane 1 flight of body, wing 9 passes through hinge component 10
It is connected with unmanned plane casing 2, wing 9 and hinge component 10 form fold mechanism, and are activity between wing 9 and hinge component 10
Connection, convenient for folding and placement of the user to wing 9, in order to the carrying of user.
Operation principle：When using this that there is the unmanned plane of Anti-bumping protection, pass through folding support member 8 and hinge first
Component 10 by supporting rod 7 and wing 9 be separately folded to the lower end of unmanned plane body 1 and with 1 parallel place of unmanned plane body, then beat
Switch power supply, at this time unmanned plane body 1 start to work, unmanned plane body 1 starts to fly up under the drive of wing 9, in unmanned plane sheet
During body 1 flies, air-flow enters the inside of heat-dissipating pipe 401 by air inlet 5, then in the first radiating fin 402 and second
Cool down under the action of radiating fin 403 to the inside of unmanned plane body 1, be conducive to distribute the heat inside unmanned plane body 1
Amount, next treats that extraneous object is accidentally bumped against on unmanned plane body 1, at this time the first damping spring 302 and the second damping spring
304 in the states shunk, at the same the first elastic 301 and second elastic energy dissipating layer 303 of energy dissipating layer can consume external object and
Impact force between unmanned plane body 1 is conducive to the injury of extraneous object and unmanned plane body 1 being preferably minimized, finally treat
Unmanned plane body 1 after hours, closes power supply, and unmanned plane body 1 is stopped at this time, is not described in detail in this specification
Content belong to the prior art well known to professional and technical personnel in the field.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of have the function of the unmanned plane of Anti-bumping protection, special including unmanned plane body (1), supporting rod (7) and wing (9)
Sign is：Unmanned plane casing (2) is packaged on the outside of the unmanned plane body (1), and is provided on the outside of unmanned plane casing (2)
Anticollision device, collision-prevention device (3), the unmanned plane body (1) are internally provided with radiator (4), and up and down the two of unmanned plane body (1)
End offers air outlet (6) and air inlet (5) respectively, and the supporting rod (7) passes through folding support member (8) and unmanned plane casing
(2) connect, the wing (9) is connected by hinge component (10) with unmanned plane casing (2).
A kind of there is the unmanned plane of Anti-bumping protection 2. according to claim 1, it is characterised in that：The anticollision device, collision-prevention device
(3) the first elastic energy dissipating layer (301), the first damping spring (302), the second elastic energy dissipating layer (303) and the second damping bullet are included
Spring (304), and the inside of the first elastic energy dissipating layer (301) is equipped with the first damping spring (302), the first elastic energy dissipating layer
(301) inner ring is provided with the second elastic energy dissipating layer (303), and the inside of the second elastic energy dissipating layer (303) is equipped with the second damping
Spring (304).
A kind of there is the unmanned plane of Anti-bumping protection 3. according to claim 1, it is characterised in that：The radiator
(4) heat-dissipating pipe (401), the first radiating fin (402) and the second radiating fin (403), and one end peace of heat-dissipating pipe (401) are included
Equipped with the first radiating fin (402), the other end of the first radiating fin (402) is connected with the second radiating fin (403).
A kind of there is the unmanned plane of Anti-bumping protection 4. according to claim 1, it is characterised in that：The supporting rod
(7) and folding support member (8) forms fold mechanism, and supporting rod (7) is mounted on the downside of unmanned plane casing (2) at equal intervals.
A kind of there is the unmanned plane of Anti-bumping protection 5. according to claim 1, it is characterised in that：The supporting rod
(7) it is arc-shaped structure, and supporting rod (7) upper end curved bend curvature is less than supporting rod (7) lower end curved bend curvature.
A kind of there is the unmanned plane of Anti-bumping protection 6. according to claim 1, it is characterised in that：The wing (9)
Fold mechanism is formed with hinge component (10), and is flexible connection between wing (9) and hinge component (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711498119.6A CN108116651A (en) | 2017-12-31 | 2017-12-31 | It is a kind of that there is the unmanned plane of Anti-bumping protection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711498119.6A CN108116651A (en) | 2017-12-31 | 2017-12-31 | It is a kind of that there is the unmanned plane of Anti-bumping protection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108116651A true CN108116651A (en) | 2018-06-05 |
Family
ID=62232556
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711498119.6A Pending CN108116651A (en) | 2017-12-31 | 2017-12-31 | It is a kind of that there is the unmanned plane of Anti-bumping protection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108116651A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112678156A (en) * | 2021-01-13 | 2021-04-20 | 徐艳 | Unmanned aerial vehicle flight anti-collision device |
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|---|---|---|---|---|
| CN104590556A (en) * | 2014-10-31 | 2015-05-06 | 湖北易瓦特科技有限公司 | Foldable unmanned aerial vehicle |
| CN205632998U (en) * | 2016-05-25 | 2016-10-12 | 黄健强 | Unmanned aerial vehicle heat abstractor of high -efficient rain -proof snow |
| CN106005384A (en) * | 2016-06-20 | 2016-10-12 | 深圳市勤新科技有限公司 | Unmanned aerial vehicle with high protection performance |
| CN206087338U (en) * | 2016-10-12 | 2017-04-12 | 中交遥感载荷（北京）科技有限公司 | Agricultural plant protection unmanned aerial vehicle collision resistance device |
| CN206273035U (en) * | 2016-12-07 | 2017-06-20 | 深圳市加贝智能科技有限公司 | One kind retinue unmanned plane radiator |
| US20170247098A1 (en) * | 2016-02-25 | 2017-08-31 | Parrot Drones | Drone with folding linking arms |
| CN107323655A (en) * | 2017-07-13 | 2017-11-07 | 厦门九星天翔航空科技有限公司 | A kind of shatter-resistant unmanned plane |
| CN107472535A (en) * | 2017-09-20 | 2017-12-15 | 王月娟 | A kind of unmanned plane hood of shatter-resistant |
| CN206807953U (en) * | 2016-12-29 | 2017-12-26 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane enclosed radiation ducting system and unmanned plane |
-
2017
- 2017-12-31 CN CN201711498119.6A patent/CN108116651A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104590556A (en) * | 2014-10-31 | 2015-05-06 | 湖北易瓦特科技有限公司 | Foldable unmanned aerial vehicle |
| US20170247098A1 (en) * | 2016-02-25 | 2017-08-31 | Parrot Drones | Drone with folding linking arms |
| CN205632998U (en) * | 2016-05-25 | 2016-10-12 | 黄健强 | Unmanned aerial vehicle heat abstractor of high -efficient rain -proof snow |
| CN106005384A (en) * | 2016-06-20 | 2016-10-12 | 深圳市勤新科技有限公司 | Unmanned aerial vehicle with high protection performance |
| CN206087338U (en) * | 2016-10-12 | 2017-04-12 | 中交遥感载荷（北京）科技有限公司 | Agricultural plant protection unmanned aerial vehicle collision resistance device |
| CN206273035U (en) * | 2016-12-07 | 2017-06-20 | 深圳市加贝智能科技有限公司 | One kind retinue unmanned plane radiator |
| CN206807953U (en) * | 2016-12-29 | 2017-12-26 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane enclosed radiation ducting system and unmanned plane |
| CN107323655A (en) * | 2017-07-13 | 2017-11-07 | 厦门九星天翔航空科技有限公司 | A kind of shatter-resistant unmanned plane |
| CN107472535A (en) * | 2017-09-20 | 2017-12-15 | 王月娟 | A kind of unmanned plane hood of shatter-resistant |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112678156A (en) * | 2021-01-13 | 2021-04-20 | 徐艳 | Unmanned aerial vehicle flight anti-collision device |
| CN112678156B (en) * | 2021-01-13 | 2022-08-30 | 国鹄航空科技(杭州)股份有限公司 | Anti-collision device for unmanned aerial vehicle flight |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180605 |