CN106081077A - A kind of can the shockproof flight instruments of multiple-effect of flying for long time - Google Patents
A kind of can the shockproof flight instruments of multiple-effect of flying for long time Download PDFInfo
- Publication number
- CN106081077A CN106081077A CN201610706090.5A CN201610706090A CN106081077A CN 106081077 A CN106081077 A CN 106081077A CN 201610706090 A CN201610706090 A CN 201610706090A CN 106081077 A CN106081077 A CN 106081077A
- Authority
- CN
- China
- Prior art keywords
- foot rest
- bracing frame
- straight tube
- aircraft body
- guard rail
- 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 abstract description 39
- 229920001971 elastomer Polymers 0.000 claims description 8
- 239000005060 rubber Substances 0.000 claims description 8
- 239000000463 material Substances 0.000 claims description 6
- 230000005611 electricity Effects 0.000 claims description 3
- 230000006378 damage Effects 0.000 abstract description 7
- 230000008901 benefit Effects 0.000 abstract description 4
- 210000003128 head Anatomy 0.000 description 9
- 230000006835 compression Effects 0.000 description 5
- 238000007906 compression Methods 0.000 description 5
- 239000002699 waste material Substances 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000009514 concussion Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000523 sample Substances 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229920003051 synthetic elastomer Polymers 0.000 description 2
- 239000005061 synthetic rubber Substances 0.000 description 2
- 244000043261 Hevea brasiliensis Species 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 241000607479 Yersinia pestis Species 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000005684 electric field Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000002372 labelling Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000004899 motility Effects 0.000 description 1
- 229920003052 natural elastomer Polymers 0.000 description 1
- 229920001194 natural rubber Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000002341 toxic gas Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a kind of can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body, connecting on aircraft body has two to land foot rest, each foot rest that lands includes that two support straight tube and a bracing frame, are provided with a damping spring between each support straight tube and bracing frame；Damping straight tube it is additionally provided with inside damping spring；Also including that extends a foot rest on foot rest each landing, described prolongation foot rest is fixed on bracing frame by two buckles；Landing at two and be additionally provided with a guard rail between foot rest, the two ends of guard rail are connected with two bracing frames landed on foot rest respectively；Aircraft body is additionally provided with a solar battery sheet.Advantages of the present invention: solve land vibrations bring photographic head, The Cloud Terrace and land foot rest easily collide with damage problem；Solve land foot rest be weak to mill and be easily damaged when landing, aircraft can not maintain the problems such as flying for long time.
Description
Technical field
The present invention relates to minute vehicle field, relate in particular to a kind of can the multiple-effect of flying for long time shockproof flight dress
Put.
Background technology
Minute vehicle receives much attention owing to having special purposes.One important application is military surveillance, is equipped with
To soldier class, carry out enemy's situation scouting and supervision.Can be additionally used in war danger estimation, target search, communication relay, monitoring chemistry,
Nuclear or biological weapons, scouts interior of building situation.It is applicable to the multiple war environment such as city, jungle.Because it is easy to take
Band, simple to operate, advantage that safety is good, can equip in a large number in army.In non-military field, it is configured with respective sensor
Minute vehicle can be used to search disaster survivor, toxic gas or chemical substance source, eliminate crop pests etc..In reality
In the life of border, the minute vehicle with photography function uses the most universal, but this minute vehicle land foot rest one
As be made up of rigid, hard plastics or rustless steel, material is harder, the most wear-resisting, yielding, when landing, lands foot rest, photographic head
Very big with the concussion impact that The Cloud Terrace is subject to, damage of easily being collided with.Even if landing on smooth ground, always can exist and taking the photograph
The unclear problem of picture shot when landing as head.It addition, existing minute vehicle typically uses battery to power, at any time
May not have electricity, cause aircraft can not maintain flying for long time, use dry cell power supply to be unfavorable for environmental conservation, wave simultaneously yet
Take the energy.
Summary of the invention
It is an object of the invention to provide a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solve existing miniature
Aircraft when landing, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem；Solve existing
When minute vehicle falls on uneven ground, the photographic head of minute vehicle and The Cloud Terrace easily collide with damage, the picture of shooting
Face is ambiguous problem because being given a shock；Solve existing minute vehicle can not automatic power, cause the aircraft can not
Maintain flying for long time, change battery trouble, the waste energy, the most durable problem.
The present invention is achieved through the following technical solutions:
A kind of can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body, aircraft body connects and has two
The individual foot rest that lands, each foot rest that lands includes that two support straight tube and a bracing frame, are provided with two on each bracing frame (3)
Individual slotted eye, is provided with a damping spring between each support straight tube and bracing frame；One end of described damping spring and support
Straight tube is fixed, and the other end is fixed with bracing frame；Inside damping spring, be additionally provided with damping straight tube, one end of damping straight tube with
Support is fixed, and the other end is placed in inside support straight tube；Also include that one extends foot rest, described prolongation foot on foot rest each landing
Frame is fixed on bracing frame by two buckles；
Landing at two and be additionally provided with a guard rail between foot rest, what the two ends of guard rail were landed on foot rest with two respectively props up
Support connects；Described guard rail be one by the bar pad having certain thickness rubber to make, be provided with at the two ends of guard rail
Groove, the notch size of groove and the shaft diameter matches of bracing frame；Each groove is additionally provided with two circular holes, described circle
The diameter in hole is equal with the diameter of slotted eye on bracing frame, uses the mode that screw bolt and nut is connected by guard rail
It is fixed on bracing frame；
Aircraft body is additionally provided with a solar battery sheet, solar battery sheet and the charging within aircraft body
Battery connects；Described solar battery sheet is positioned at the top of aircraft body, uses the mode that draw-in groove connects by solaode
Sheet is fixed on aircraft body.
Further, arranging a damping straight tube inside damping spring, one end of damping straight tube is fixed with bracing frame, subtracts
One end and the bracing frame of shake straight tube are fixing has been a supporting role, it is to avoid damping spring bending shifts, and causes landing foot rest
Deformation.Additionally the other end of damping straight tube be placed in support straight tube inside, when designing simultaneously, it is desirable to damping straight tube not with support straight tube
Being connected and also have a certain distance with supporting straight tube, such damping straight tube can move along with the compression of damping spring and past
Support straight tube is internal mobile.Flight controller has constant weight, so flight controller is when landing, is positioned on flight controller
The foot rest that lands can produce an active force over the ground, meanwhile, landing foot rest also can be by the opposition on ground.Because being subject to
To the opposition on ground, the damping spring on foot rest that lands will be produced a thrust by compression, and damping spring produces
The opposition on thrust and ground can be cancelled out each other, meanwhile, be placed in support one end of the damping straight tube within straight tube can be along with
The compression of damping spring and more probe into inside support straight tube.The damping spring and the damping straight tube that arrange on foot rest solve existing
Minute vehicle when landing, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem.
Also include that extends a foot rest on foot rest each landing, one prolongation foot rest is fixed on by two buckles
Add on support and land the height of foot rest, both can ensure that the original-pack foot rest that lands was not dirty, and be not scraped off, fall can be reduced again
The probability that camera lens when falling, The Cloud Terrace are injured.
Landing at two and arrange a guard rail between foot rest, guard rail is had certain thickness rubber blanket to make by one,
For example with synthetic rubber.The top view of guard rail is a rectangle, and the width of guard rail can be with more slightly wider, as far as possible will shooting
Head base and The Cloud Terrace surround, and when falling rough local time, the effect of camera head protecting can be more preferably.The two ends of guard rail are recessed
Groove, groove has two apertures, is stuck on bracing frame by groove, and bolt passes aperture, uses nut by guard rail and bracing frame
Fix.
Being additionally provided with inverter and transformator in aircraft body, solar battery sheet is arranged on the top of aircraft body
Portion can be conducive to shining upon, in order to obtains luminous energy.The principle that solar battery sheet is powered is: solar irradiation is at quasiconductor P-
N ties, and forms new hole-electron pair, and under the effect of P-N junction electric field, hole is flowed to P district by N district, and electronics is flowed to N by P district
District, is formed for electric current after connecting circuit.The electric current that solaode produces is unidirectional current, and unidirectional current is transformed into after inverter
Alternating current, then the voltage of the alternating current transmitted by inverter through transformator drops in the rechargeable battery range of nominal tension, then
It is transmitted further to rechargeable battery.Using solar energy is that aircraft is powered, and solving existing minute vehicle can not automatic power, more
Change battery trouble, the waste energy, the most durable problem.Backlight device that the present invention uses and transformator and solaode
Sheet is all existing conventional.
Being additionally provided with the connecting hole of an annular on each support straight tube, the foot rest that lands is threaded connection part and passes
Connecting hole is fixed with aircraft body.Further, each support straight tube is additionally provided with the connecting hole of an annular, falls
Ground foot rest is threaded connection part and fixes with aircraft body through connecting hole.Supporting the connecting hole that annular is set on straight tube
The foot rest that lands for convenience is threaded connection fixing with aircraft body, uses threaded connector through the such connection of connecting hole
Fixed form has motility, and the foot rest that lands can take off at any time, does not occupies, it is simple to transport.
Described prolongation foot rest uses abrasion-resistive hard quality of rubber materials to make.Use the prolongation foot that abrasion-resistive hard quality of rubber materials is made
Frame can be more resistant to mill, and service life is longer.
The present invention compared with prior art, has such advantages as and beneficial effect:
1, the present invention a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solve existing minute vehicle and landing
Time, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem；
2, the present invention a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solve existing minute vehicle and fall in injustice
Time on smooth ground, the photographic head of minute vehicle and The Cloud Terrace easily collide with damage, and the picture of shooting obscures because being given a shock
Unclear problem；
3, the present invention a kind of can the shockproof flight instruments of multiple-effect of flying for long time, solving existing minute vehicle can not be automatic
Power supply, causes aircraft can not maintain flying for long time, changes battery trouble, the waste energy, the most durable problem.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing being further appreciated by the embodiment of the present invention, constitutes of the application
Point, it is not intended that the restriction to the embodiment of the present invention.In the accompanying drawings:
Fig. 1 is the structural representation of the present invention；
Fig. 2 is that the present invention lands the structural representation of foot rest；
Fig. 3 is the structural representation of guard rail of the present invention.
Labelling in accompanying drawing and the component names of correspondence:
1-aircraft body, 2-supports straight tube, 3-bracing frame, 4-damping spring, 5-damping straight tube, and 6-extends foot rest, 7-card
Button, 8-connecting hole, 9-guard rail, 10-groove, 11-circular hole, 12-solar battery sheet.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with embodiment and accompanying drawing, to this
Invention is described in further detail, and the exemplary embodiment of the present invention and explanation thereof are only used for explaining the present invention, do not make
For limitation of the invention.
Embodiment 1:
As shown in Figure 1, Figure 2, Figure 3 shows a kind of can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body 1,
Connecting on aircraft body 1 has two to land foot rest, it is characterised in that each foot rest that lands includes that two support straight tubes 2 and
Individual bracing frame 3, is provided with two slotted eyes on each bracing frame 3, is provided with one between each support straight tube 2 and bracing frame 3
Individual damping spring 4；One end of described damping spring 4 is fixed with supporting straight tube 2, and the other end is fixed with bracing frame 3；At damping spring
The 4 internal damping straight tubes 5 that are additionally provided with, one end of damping straight tube 5 is fixing with bracing frame 3, and it is internal that the other end is placed in support straight tube 2；
Also including that extends a foot rest 6 on foot rest each landing, described prolongation foot rest 6 is fixed on bracing frame 3 by two buckles 7
On；
Landing at two and be additionally provided with a guard rail 9 between foot rest, the two ends of guard rail 9 are landed on foot rest with two respectively
Bracing frame 3 connects；Described guard rail 9 be one by the bar pad having certain thickness rubber to make, set at the two ends of guard rail 9
It is equipped with groove 10, the notch size of groove 10 and the shaft diameter matches of bracing frame 3；Each groove 10 is additionally provided with two
Circular hole 11, the diameter of described circular hole 11 is equal with the diameter of slotted eye on bracing frame 3, uses screw bolt and nut to coordinate even
Guard rail 9 is fixed on bracing frame 3 by the mode connect；
Being additionally provided with a solar battery sheet 12 on aircraft body 1, the electric energy of acquisition is flown by solar battery sheet 12
Rechargeable battery charging within row device body 1；Described solar battery sheet 12 is positioned at the top of aircraft body 1, uses draw-in groove
Solar battery sheet 12 is fixed on aircraft body 1 by the mode connected.
Being additionally provided with the connecting hole 8 of an annular on each support straight tube 2, the foot rest that lands is threaded connection part and wears
Cross connecting hole to fix with aircraft body 1.Described prolongation foot rest 6 uses abrasion-resistive hard quality of rubber materials to make.
A kind of can the design principle of the shockproof flight instruments of multiple-effect of flying for long time: flight controller has constant weight,
So flight controller is when landing, the foot rest that lands being positioned on flight controller can produce an active force over the ground, meanwhile,
Landing foot rest also can be by the opposition on ground.Because by the opposition on ground, land the damping bullet on foot rest
Spring 4 will be produced a thrust by compression, and the thrust of damping spring 4 generation can be cancelled out each other with the opposition on ground, with
Time, the one end being placed in support damping straight tube 5 within straight tube 2 more can probe into along with the compression of damping spring 4 in support straight tube 2
Portion.Land on foot rest arrange damping spring 4 and damping straight tube 5 solve existing minute vehicle and be easily subject to when landing
To concussion, the float causing shooting is unclear, and lands foot rest and be easily subject to impact and the problem damaged.
Also include that extends a foot rest 6 on foot rest each landing, by two buckles 7, a prolongation foot rest 6 is fixed
Bracing frame 3 adds and lands the height of foot rest, both can ensure that the original-pack foot rest that lands was not dirty, and be not scraped off, again can
The probability that when reducing landing, camera lens, The Cloud Terrace are injured.Additionally extending foot rest 6 uses natural rubber material to make, and more resistant to mill, uses the longevity
Order longer.
Landing at two and arrange a guard rail 9 between foot rest, guard rail 9 uses synthetic rubber to make.When falling in injustice
The local time in of sliding, there are this guard rail 9, photographic head and The Cloud Terrace can avoid colliding with below photographic head, photographic head and The Cloud Terrace
A good protection can be obtained.
In aircraft body 1, it is additionally provided with inverter and transformator, uses monocrystaline silicon solar cell sheet 12 to be arranged on
The top of aircraft body 1 can be conducive to shining upon, in order to obtains luminous energy.The electric current that solaode 12 produces is direct current
Electricity, unidirectional current is transformed into alternating current after inverter, then the voltage of the alternating current transmitted by inverter through transformator drops to
In the rechargeable battery range of nominal tension, then it is transmitted further to rechargeable battery.Using solar energy is that aircraft is powered, and solves existing
Minute vehicle can not automatic power, change battery trouble, waste the energy, the most durable problem.
Above-described detailed description of the invention, has been carried out the purpose of the present invention, technical scheme and beneficial effect further
Describe in detail, be it should be understood that the detailed description of the invention that the foregoing is only the present invention, be not intended to limit the present invention
Protection domain, all within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, all should comprise
Within protection scope of the present invention.
Claims (3)
1. can the shockproof flight instruments of multiple-effect of flying for long time, including aircraft body (1), on aircraft body (1)
Connect and have two to land foot rest, it is characterised in that each foot rest that lands includes that two support straight tube (2) and a bracing frame (3),
Each bracing frame (3) is provided with two slotted eyes, between each support straight tube (2) and bracing frame (3), is provided with one subtracts
Shake spring (4)；One end of described damping spring (4) is fixed with supporting straight tube (2), and the other end is fixed with bracing frame (3)；In damping
The internal damping straight tube (5) that is additionally provided with of spring (4), one end of damping straight tube (5) is fixing with bracing frame (3), and the other end is placed in and props up
Support straight tube (2) is internal；Also including that extends a foot rest (6) on foot rest each landing, described prolongation foot rest (6) passes through two cards
Button (7) is fixed on bracing frame (3)；
Landing at two and be additionally provided with a guard rail (9) between foot rest, land foot rest respectively with two at the two ends of guard rail (9)
On bracing frame (3) connect；Described guard rail (9) be one by the bar pad having certain thickness rubber to make, at guard rail
(9) two ends are provided with the shaft diameter matches of groove (10), the notch size of groove (10) and bracing frame (3)；Each recessed
Being additionally provided with two circular holes (11) on groove (10), the diameter of the diameter of described circular hole (11) slotted eye upper with bracing frame (3) is big
Little equal, guard rail (9) is fixed on bracing frame (3) by the mode using screw bolt and nut to be connected；
Aircraft body (1) is additionally provided with a solar battery sheet (12), the electricity that solar battery sheet (12) will obtain
The rechargeable battery charging that aircraft body (1) is internal can be given；Described solar battery sheet (12) is positioned at the top of aircraft body (1)
Portion, solar battery sheet (12) is fixed on aircraft body (1) by the mode using draw-in groove to connect.
The most according to claim 1 a kind of can the shockproof flight instruments of multiple-effect of flying for long time, it is characterised in that each
Support the connecting hole (8) being additionally provided with an annular on straight tube (2), the foot rest that lands be threaded connection part through connecting hole with
Aircraft body (1) is fixed.
The most according to claim 1 a kind of can the shockproof flight instruments of multiple-effect of flying for long time, it is characterised in that described in prolong
Long foot rest (6) uses abrasion-resistive hard quality of rubber materials to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706090.5A CN106081077A (en) | 2016-08-23 | 2016-08-23 | A kind of can the shockproof flight instruments of multiple-effect of flying for long time |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706090.5A CN106081077A (en) | 2016-08-23 | 2016-08-23 | A kind of can the shockproof flight instruments of multiple-effect of flying for long time |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106081077A true CN106081077A (en) | 2016-11-09 |
Family
ID=57226245
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610706090.5A Pending CN106081077A (en) | 2016-08-23 | 2016-08-23 | A kind of can the shockproof flight instruments of multiple-effect of flying for long time |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106081077A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107883927A (en) * | 2017-11-09 | 2018-04-06 | 陕西科技大学 | Quadrotor plant growth inspection system |
| CN108069023A (en) * | 2016-11-17 | 2018-05-25 | 深圳光启空间技术有限公司 | Aircraft damping undercarriage and aircraft |
| CN108545206A (en) * | 2018-04-03 | 2018-09-18 | 芜湖超科机电设备有限公司 | A kind of aerophotography unmanned plane |
| CN110550217A (en) * | 2019-09-21 | 2019-12-10 | 浙江驭云航空科技有限公司 | Unmanned aerial vehicle's extension continuation of journey device |
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| EP2607232A1 (en) * | 2011-12-21 | 2013-06-26 | Eurocopter Deutschland GmbH | Landing gear vibration absorber for a helicopter and method of operating said landing gear vibration absorber |
| CN104044731A (en) * | 2014-06-26 | 2014-09-17 | 深圳市哈博森科技有限公司 | Aircraft landing device and aircraft |
| CN205150253U (en) * | 2015-11-26 | 2016-04-13 | 江西天祥通用航空股份有限公司 | Novel helicopter joins externally pesticide spraying machine |
| CN205327398U (en) * | 2015-12-27 | 2016-06-22 | 北京航空航天大学 | Small -size many rotor crafts shock attenuation undercarriage |
| CN205418094U (en) * | 2016-03-18 | 2016-08-03 | 天际智控成都科技有限责任公司 | Push -button aircraft |
| CN206087275U (en) * | 2016-08-23 | 2017-04-12 | 成都翼高九天科技有限公司 | But jar -proof flying device of solar energy power supply multiple -effect |
-
2016
- 2016-08-23 CN CN201610706090.5A patent/CN106081077A/en active Pending
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|---|---|---|---|---|
| EP2607232A1 (en) * | 2011-12-21 | 2013-06-26 | Eurocopter Deutschland GmbH | Landing gear vibration absorber for a helicopter and method of operating said landing gear vibration absorber |
| CN104044731A (en) * | 2014-06-26 | 2014-09-17 | 深圳市哈博森科技有限公司 | Aircraft landing device and aircraft |
| CN205150253U (en) * | 2015-11-26 | 2016-04-13 | 江西天祥通用航空股份有限公司 | Novel helicopter joins externally pesticide spraying machine |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108069023A (en) * | 2016-11-17 | 2018-05-25 | 深圳光启空间技术有限公司 | Aircraft damping undercarriage and aircraft |
| CN107883927A (en) * | 2017-11-09 | 2018-04-06 | 陕西科技大学 | Quadrotor plant growth inspection system |
| CN108545206A (en) * | 2018-04-03 | 2018-09-18 | 芜湖超科机电设备有限公司 | A kind of aerophotography unmanned plane |
| CN108545206B (en) * | 2018-04-03 | 2020-09-01 | 山东昊盾警用装备有限公司 | Unmanned aerial vehicle for aerial photography |
| CN110550217A (en) * | 2019-09-21 | 2019-12-10 | 浙江驭云航空科技有限公司 | Unmanned aerial vehicle's extension continuation of journey device |
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Application publication date: 20161109 |