CN207225643U - The multi-functional unmanned plane undercarriage of horizontal - Google Patents
The multi-functional unmanned plane undercarriage of horizontal Download PDFInfo
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- CN207225643U CN207225643U CN201720903261.3U CN201720903261U CN207225643U CN 207225643 U CN207225643 U CN 207225643U CN 201720903261 U CN201720903261 U CN 201720903261U CN 207225643 U CN207225643 U CN 207225643U
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- unmanned plane
- undercarriage
- telescopic rod
- frame body
- power supply
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Abstract
The utility model discloses a kind of multi-functional unmanned plane undercarriage of horizontal, it is made of left the undercarriage frame body and right landing gear frame body for being located at left and right ends below unmanned aerial vehicle body, camera or video camera is arranged below in holder among below unmanned aerial vehicle body, and the equipment such as the first magnechuck, the second magnechuck, storage battery, power supply adaptor, flash lamp lamp cap, searchlight lamp cap, telescopic rod and screw type annulus are additionally arranged on left undercarriage frame body and right landing gear frame body.The utility model has to be connected by outdoor charging conductor with the power supply on ground, realize the purpose long lasting for power supply for unmanned plane, so as to add the skyborne cruising ability of unmanned plane, so that unmanned function is from restriction ground follow-on mission and completes work of taking photo by plane, and unmanned plane is breached because of the limited bottleneck in fuselage interior space, the advantage of unmanned plane has more efficiently been played, has improved unmanned plane Multifunction horizontal, the advantages of electric wire pins down can be broken away from any time again when there is emergency case.
Description
Technical field
Unmanned plane is the utility model is related to, more particularly, to a kind of multi-functional unmanned plane undercarriage of horizontal.
Background technology
UAV abbreviation unmanned plane, unmanned plane are to utilize wireless remotecontrol and the presetting apparatus provided for oneself manipulation
Not manned aircraft.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed.
In recent years, with the rise of unmanned plane and the fast development of unmanned plane field technology, the application field of unmanned plane
Rapidly extended, since one of main function of unmanned plane is exactly to take photo by plane, height is installed on the holder under unmanned plane ventral
Therefore the camera or video camera of clarity, unmanned plane have also entered into civil field from simple military affairs, scientific research field, increasingly
More ordinary peoples starts to contact unmanned plane.In numerous civilian unmanned planes, it is exactly take photo by plane four axis, six axis etc. of taking photo by plane to occur more
Unmanned plane.Since unmanned plane is to fly in the air, under the remote control of ground staff, flying speed, height, the angle of unmanned plane are equal
It is adjustable, thus from the excellent for taking a crane shot, capturing in the air, tourist is very suitable at some special sight spots of Scenic Spots
（Such as extremely difficult overhanging cliff climbed up and over, Grand Canyon glass bridge, isolated island or river center sight spot, towering tower upright stone tablet statue）Take pictures
Or self-timer souvenir, the deficiency of single-lens reflex camera and mobile phone self-shooting bar self-timer ability is made up, ginseng of the tourist in visit is greatly improved
Feel with sense, substitution, scenic spot enterprise can lift customer satisfaction and scenic spot reputation whereby, create more consumption values.
For power used in the unmanned plane of civil to rechargeable battery, unmanned plane follow-on mission and carries out phase in the air
Close need of work and consume more electric energy.Due to the finite capacity of battery, correlation technique can not be broken through, therefore unmanned plane
Cruising ability wretched insufficiency, flight can only continue 10-20 minutes, must then return to the new battery of replaced on ground and continue to fly
Or continue charging wait and fly next time, this has just seriously affected the use of unmanned plane；Further, since the inside of unmanned aerial vehicle body
Space is limited, can not install the electronic equipments such as searchlight, flash lamp additional, and the electronic equipment installed additional is also required to consume more electricity
Can, these defects cause the function of unmanned plane more effectively to play.
The content of the invention
The purpose of this utility model is to provide a kind of multi-functional unmanned plane undercarriage of horizontal, it is led by outdoor charging
Line is connected with the power supply on ground, realizes the purpose long lasting for power supply for unmanned plane, so as to add unmanned plane in sky
In cruising ability so that unmanned function breaches unmanned plane because of machine from restricting ground follow-on mission and complete to take photo by plane work
The limited bottleneck in body inner space, has more efficiently played the advantage of unmanned plane, improves unmanned plane Multifunction horizontal, is going out
Electric wire can be broken away from any time during existing emergency case again to pin down.
What the purpose of this utility model was realized in：
A kind of multi-functional unmanned plane undercarriage of horizontal, by the left undercarriage frame for being located at left and right ends below unmanned aerial vehicle body
Body and right landing gear frame body composition, left undercarriage frame body by be connected as a single entity left front load supporting tube, left back load supporting tube and
Horizontal left landing pipe is formed, right landing gear frame body by load supporting tube before the right side that is connected as a single entity, it is right after load supporting tube and horizontal stroke
To right landing pipe form, be equipped with holder between middle, left undercarriage frame body and right landing gear frame body below unmanned aerial vehicle body,
Camera or video camera are equipped with below holder, is characterized in：It is equipped with the front end mouth of pipe of right landing pipe with positive and negative anodes contact
First magnechuck, the first magnechuck can produce magnetic force in the case of energization and hold the preceding iron plate with positive and negative anodes contact, preceding
Iron plate is connected by outdoor charging conductor with ground power supply box, and the close ground surface end of outdoor charging conductor is wound on spool；
Middle part in right landing pipe is equipped with storage battery and power supply adaptor, is equipped with load supporting tube behind the right side and connects with undercarriage inside conductor
What is connect passes through the positive and negative anodes on undercarriage inside conductor and the first magnechuck to fuselage power supply interface, the input terminal of power supply adaptor
Contact connects, and the output terminal of power supply adaptor is connected with storage battery and to fuselage power supply interface respectively by undercarriage inside conductor,
It is plugged on to fuselage power supply interface on the power interface on the bottom of unmanned aerial vehicle body side, passes through undercarriage to fuselage power supply interface
Inside conductor is connected with the power circuit in unmanned aerial vehicle body.
On the front side wall of the left front load supporting tube of left undercarriage frame body, load supporting tube before the right side of right landing gear frame body
Front side wall on be respectively equipped with several flash lamp lamp caps being serially connected, in the left back load pillar of left undercarriage frame body
Photoflash controller is equipped with pipe, these flash lamp lamp caps connect the output terminal of photoflash controller by undercarriage inside conductor, dodge
The output terminal connection of master controller in the input terminal and unmanned aerial vehicle body of light lamp controller, storage battery supply for flash lamp lamp cap
Electricity.
Searchlight lamp cap is equipped with the front end of the left landing pipe of left undercarriage frame body, storage battery is powered for searchlight lamp cap.
Rear portion in the left landing pipe of left undercarriage frame body is equipped with telescopic rod sleeve, and more piece has been included in flexible rod sleeve
The telescopic rod that can be pulled out or retract, is equipped with the telescopic rod retraction for preventing from stretching out or is easy on the bottom outer wall of every section telescopic rod
The wedge-shaped Spring Card that the telescopic rod of retraction pulls out, wedge-shaped Spring Card can be fixed when each section telescopic rod can be caused to extend, respectively
Section telescopic rod does not bounce back.
The top that telescopic rod is saved in outermost one is spiral equipped with the telescopic rod top circular hole for being used to hang screw type annulus, suspension
One end of type annulus be hooked in outermost one save telescopic rod telescopic rod top circular hole in, suspension screw type annulus the other end hook for
Another outdoor charging conductor of another frame unmanned plane power supply, works and provides support, screw type in the air for another frame unmanned plane
The rotation of outdoor charging conductor can be put into not easily to fall off by annulus.
External screw thread is equipped with the rear end outer wall of the left landing pipe of left undercarriage frame body, is equipped with the inner wall of telescopic rod pole cap
The internal thread coordinated with external screw thread, when telescopic rod is in contraction state, telescopic rod pole cap passes through screw thread and left landing pipe
Rear end outer wall connection, covers telescopic rod.
The second magnechuck is equipped with the rear end mouth of pipe of right landing pipe, the second magnechuck can produce in the case of energization
Magnetic force holds the rear iron plate with hook, some rescues of extension field trapped person, the goods and materials of emergency can be selected on hook（Mineral spring
Water, bread, medicine, GPS transmitters, laser pen, small oxygen uptake bottle, rope, flashlight, battery of mobile phone, pull inflatable life jacket
Deng）, easy to unmanned plane materials needed are dropped when reaching trapped person overhead.
The utility model is added on left the undercarriage frame body and right landing gear frame body of the civilian unmanned plane of conventional horizontal
First magnechuck, the second magnechuck, storage battery, power supply adaptor, flash lamp lamp cap, searchlight lamp cap, telescopic rod and
The equipment such as screw type annulus, the power supply that so can not only allow in ground power supply box pass sequentially through outdoor charging conductor, band positive and negative anodes
Connected after the preceding iron plate of contact, the first magnechuck with power supply adaptor, the external power supply electric current that power supply adaptor can will turn on
Unmanned aerial vehicle body is transported to after rectification, is charged a battery at the same time, storage battery can be to the left in undercarriage frame body and right landing gear frame body
Equipment power supply, also breach unmanned plane because of the limited bottleneck in fuselage interior space, possess flash lamp, searchlight, launch smallclothes
Article etc. is multi-functional, has more efficiently played the advantage of unmanned plane.
Therefore, the utility model has the following advantages that：
1st, the utility model is connected by the outdoor charging conductor of endless with the power supply on ground so that ground power supply energy
Directly it is without interruption in sky through power supply adaptor, to the power interface on fuselage power supply interface, unmanned aerial vehicle body side bottom
The unmanned plane of middle flight is long lasting for power supply, charging, so as to add the skyborne cruising ability of unmanned plane so that unmanned plane
Can be from restricting ground follow-on mission and complete to take photo by plane work, so as to repack common unmanned plane into unmanned plane that live line is tethered at；
2nd, there is emergency case（It is possible to influence unmanned plane during flying as outdoor charging conductor is snarled by foreign object）Or no longer
When needing surface power supply, it can power off the first magnechuck, preceding iron plate is no longer held by the first magnechuck, in self gravitation
Under the action of depart from unmanned plane, unmanned plane can break away from outdoor charging conductor at any time and pin down, freely circle in the air, and skyborne room of floaing
Outer charging conductor is quickly pulled back on spool under the action of spool, is waited and being powered next time for unmanned plane；
3rd, flash lamp, searchlight can daytime light it is bad or at night send strong light, illuminate by bat personnel or object, for shine
Camera or video camera provide floodlight, and the good photo or image of clarity is taken easy to camera or video camera；
4th, some rescues of extension field trapped person, the goods and materials of emergency can be selected on the hook of rear iron plate（Mineral water, face
Bag, medicine, GPS transmitters, laser pen, small oxygen uptake bottle, rope, flashlight, battery of mobile phone, pull inflatable life jacket etc.）, just
Materials needed are dropped when unmanned plane reaches trapped person overhead, to win the rescue time of preciousness；
5th, a wide range of horizontal maneuver is carried out in high-altitude using other live lines can be helped to be tethered at unmanned plane during telescopic rod；
6th, when multi-functional unmanned plane undercarriage is not required in user, can easily dismount by hand, it is rapid to restore to the original state.
Brief description of the drawings
Fig. 1 is the structure diagram that the utility model is installed on unmanned aerial vehicle body；
Fig. 2 is the structure diagram of the utility model；
Fig. 3 is structure diagram when telescopic rod extends；
Fig. 4 is the structure diagram that the multi-functional unmanned plane undercarriage of horizontal carries out surface power supply；
Fig. 5 helps other live lines to be tethered at unmanned plane level when being extended for the multi-functional unmanned plane undercarriage telescopic rod of horizontal
Motor-driven schematic diagram；
Fig. 6 is the schematic diagram of the multi-functional unmanned plane undercarriage dedicated remote control of horizontal.
Embodiment
With reference to embodiment and compare attached drawing the utility model is described in further detail.
A kind of multi-functional unmanned plane undercarriage of horizontal, by the left undercarriage for being located at 1 lower section left and right ends of unmanned aerial vehicle body
Frame body 4 and right landing gear frame body 3 form, left undercarriage frame body 4 by be connected as a single entity left front load supporting tube 13, left back load branch
Column tube 14 and horizontal left landing pipe 6 are formed, right landing gear frame body 3 by load supporting tube 11 before the right side that is connected as a single entity, it is right after hold
Power supporting tube 12 and horizontal right landing pipe 5 are formed, middle below unmanned aerial vehicle body 1, left undercarriage frame body 4 and right landing gear
Holder 2 is equipped between frame body 3, camera or video camera 17 are equipped with below holder 2, is set in the front end mouth of pipe of right landing pipe 5
There is the first magnechuck 7 with positive and negative anodes contact 8, the first magnechuck 7 can produce magnetic force in the case of energization and hold band just
The preceding iron plate 23 of anode contact 29, preceding iron plate 23 are connected by outdoor charging conductor 22 with ground power supply box 27, and outdoor charging is led
The close ground surface end of line 22 is wound on spool 30；Middle part in right landing pipe 5 is equipped with storage battery 28 and power supply adaptor 18,
Be equipped with behind the right side on load supporting tube 12 be connected with undercarriage inside conductor 21 to fuselage power supply interface 16, power supply adaptor 18
Input terminal is connected by undercarriage inside conductor 21 with the positive and negative anodes contact 8 on the first magnechuck 7, the output of power supply adaptor 18
End is connected with storage battery 28 and to fuselage power supply interface 16 respectively by undercarriage inside conductor 21, to 16 grafting of fuselage power supply interface
On power interface on 1 side bottom of unmanned aerial vehicle body, pass through undercarriage inside conductor 21 and nobody to fuselage power supply interface 16
Power circuit connection in machine fuselage 1.
On the front side wall of the left front load supporting tube 13 of left undercarriage frame body 4, load branch before the right side of right landing gear frame body 3
Several flash lamp lamp caps 15 being serially connected are respectively equipped with the front side wall of column tube 11, in the left back of left undercarriage frame body 4
Photoflash controller 20 is equipped with load supporting tube 14, these flash lamp lamp caps 15 connect flash lamp control by undercarriage inside conductor 21
The output terminal of device 20 processed, the input terminal of photoflash controller 20 are connected with the output terminal of the master controller in unmanned aerial vehicle body 1, are stored
Battery 28 is powered for flash lamp lamp cap 15.
Searchlight lamp cap 10 is equipped with the front end of the left landing pipe 6 of left undercarriage frame body 4, storage battery 28 is searchlight lamp cap
10 power supplies.
Rear portion in the left landing pipe 6 of left undercarriage frame body 4 is equipped with telescopic rod sleeve 19, is included in flexible rod sleeve 19
There is the telescopic rod 25 that more piece can pull out or retract, the telescopic rod for preventing stretching out is equipped with the bottom outer wall of every section telescopic rod 25
25 retraction or easy to retraction telescopic rod 25 pull out wedge-shaped Spring Card 35, wedge-shaped Spring Card 35 can so that it is each save telescopic rod 25 stretch
Fixed when long, each telescopic rod 25 that saves does not bounce back.
On the top that outermost one saves telescopic rod 25 equipped with the telescopic rod top circular hole 31 for being used to hang screw type annulus 32, hang
The one end for hanging screw type annulus 32 is hooked in the telescopic rod top circular hole 31 that outermost one saves telescopic rod 25, suspension screw type annulus 32
The other end hook another outdoor charging conductor 36 for the power supply of another frame unmanned plane 37, be another frame unmanned plane 37 in the air
Work provides support, and another outdoor rotation of charging conductor 36 can be put into not easily to fall off by screw type annulus 32.
External screw thread 34 is equipped with the rear end outer wall of the left landing pipe 6 of left undercarriage frame body 4, in telescopic rod pole cap 26
Wall is equipped with the internal thread 33 coordinated with external screw thread 34, and when telescopic rod 25 is in contraction state, telescopic rod pole cap 26 passes through screw thread
It is connected with the rear end outer wall of left landing pipe 6, covers telescopic rod 25.
The second magnechuck 9 is equipped with the rear end mouth of pipe of right landing pipe 5, the second magnechuck 9 can be in the case of energization
Produce magnetic force and hold the rear iron plate 24 with hook 38, some rescues of extension field trapped person, emergency can be selected on hook 38
Goods and materials（Mineral water, bread, medicine, GPS transmitters, laser pen, small oxygen uptake bottle, rope, flashlight, battery of mobile phone, pull and fill
Gas formula life vest etc.）, easy to unmanned plane materials needed are dropped when reaching by rescuer overhead.
Remote controler used by a user on ground is multi-functional undercarriage dedicated remote control 44, special in multi-functional undercarriage
Remote controler antenna 39, the first magnechuck remote control switch 40, the second magnechuck remote control switch 41, spy are equipped with remote controler 44
Illuminator remote control switch 42 and flash lamp remote control switch 43.
Embodiment 1：Unmanned plane electromagnet is long lasting for power supply.
When needing unmanned plane flying for long time in the air, user is first by the electricity of positive and negative anodes contact 29 and first of preceding iron plate 23
The positive and negative anodes contact 8 of magnetic-disc 7 contacts well, then presses the first electricity on multi-functional undercarriage dedicated remote control 44
Magnetic-disc remote control switch 40, storage battery 28 power to the first magnechuck 7 and produce magnetic force, iron plate 23 before holding, ground power supply
The electric current of box 27 reaches the power supply adaptor 18 in right landing pipe 5 by preceding 23 and first magnechuck 7 of iron plate, then pass through to
Fuselage power supply interface 16 is powered for unmanned aerial vehicle body 1, while is charged to the storage battery 28 in right landing pipe 5.User manipulates nothing again
Control key on man-machine fuselage remote controler, unmanned plane start with outdoor charging conductor 22 to it is predetermined it is aerial fly to, ground electricity
The unmanned plane that source can directly fly in the air without interruption is long lasting for power supply, charging.When there is emergency case（Such as outdoor
Charging conductor is snarled by foreign object to be possible to influence unmanned plane during flying）Or no longer need surface power supply constantly, press the suction of the first electromagnetism
Disk remote control switch 40, the first magnechuck 7 power off magnetic at once, and preceding iron plate 23 comes off naturally, and unmanned plane terminates externally fed, cuts
Fuselage battery powered is changed to freely to fly away.
Embodiment 2：Unmanned plane electromagnet launches small article.
When needing unmanned plane to be dropped in designated position, user first connects rear 24 and second magnechuck 9 of iron plate well
Touch together, then press the second magnechuck remote control switch 41 on multi-functional undercarriage dedicated remote control 44, storage battery 28 to
Second magnechuck 9 powers and produces magnetic force, holds the rear iron plate 24 with hook 38, small article can be hung on hook 38.Nothing
It is man-machine to take off when reaching predetermined release position, press the second magnechuck remote control switch 41, the disconnected magnetic of the second magnechuck 9 power-off, band
The rear iron plate 24 and small article of hook 38 invest destination.
Embodiment 3：Help other live lines to be tethered at unmanned plane and move horizontally that (live line is tethered at unmanned plane due to by electric wire
Restrict, can only be vertically moved up and down under the more environment of barrier).
Live line is tethered at unmanned plane 37 and takes off vertically in advance, and tall barrier（Such as high building, great Shu）Locking hovering afterwards
State.User rotatably unscrews the telescopic rod pole cap 26 on the telescopic rod sleeve 19 in the left landing pipe 6 on the second frame unmanned plane, draws
Go out telescopic rod 25, screw type annulus 32 is fixed on telescopic rod top circular hole 31, live line is tethered to the outdoor of unmanned plane 37
Charging conductor 36 pierces into screw type annulus 32, and the second frame unmanned plane, which takes off vertically to live line, is tethered at the lower orientation of unmanned plane 37
Put, lock floating state.Afterwards, live line is tethered at unmanned plane 37 under the support of outdoor charging conductor 36, can with the second frame without
It is man-machine to do remote, a wide range of motor-driven, flying for long time in the air in the horizontal direction for fulcrum.After task, live line
Be tethered at unmanned plane 37 fly back the second frame unmanned plane horizontal level nearby and hover, the second frame unmanned plane vertically falls back to ground
Face, outdoor charging conductor 36 is taken out from screw type annulus 32, live line, which is tethered at unmanned plane 37, can then land.
Embodiment 4：Unmanned plane searchlight, flash lamp use.
When needing to use unmanned plane searchlight function, the searchlight pressed on multi-functional undercarriage dedicated remote control 44 is distant
Control switch 42, the searchlight lamp cap 10 of storage battery 28 in right landing pipe 5 to the left in landing pipe 6 are powered and are lighted, press again
Searchlight remote control switch 42, the power-off of searchlight lamp cap 10 are extinguished.When needing to use unmanned plane flash lamp function, press multi-functional
Flash lamp remote control switch 43 on undercarriage dedicated remote control 44, the photoflash controller 20 in left back load supporting tube 14 are in
Armed state, when unmanned plane shooting shutter is pressed, on the front side wall of left front load supporting tube 13, it is right before before load supporting tube 11
The activation of flash lamp lamp cap 15 on side wall sends strong flash of light.
Claims (10)
- A kind of 1. multi-functional unmanned plane undercarriage of horizontal, by the left undercarriage frame body for being located at left and right ends below unmanned aerial vehicle body Formed with right landing gear frame body, left undercarriage frame body is by the left front load supporting tube, left back load supporting tube and horizontal stroke that are connected as a single entity To left landing pipe form, right landing gear frame body by load supporting tube before the right side that is connected as a single entity, it is right after load supporting tube and transverse direction Right landing pipe form, be equipped with holder between middle, left undercarriage frame body and right landing gear frame body below unmanned aerial vehicle body, Camera or video camera are equipped with below holder, it is characterised in that：Band positive and negative anodes contact is equipped with the front end mouth of pipe of right landing pipe The first magnechuck, the first magnechuck can produce magnetic force in the case of energization and hold the preceding iron plate with positive and negative anodes contact, Preceding iron plate is connected by outdoor charging conductor with ground power supply box, and the close ground surface end of outdoor charging conductor is wound on spool； Middle part in right landing pipe is equipped with storage battery and power supply adaptor, is equipped with and undercarriage inside conductor on load supporting tube behind the right side Connection to fuselage power supply interface, the input terminal of power supply adaptor by undercarriage inside conductor with it is positive and negative on the first magnechuck Pole contact connection, the output terminal of power supply adaptor are connected with storage battery and to fuselage power supply interface respectively by undercarriage inside conductor Connect, be plugged on to fuselage power supply interface on the power interface on the bottom of unmanned aerial vehicle body side, to fuselage power supply interface by rising Fall frame inside conductor to be connected with the power circuit in unmanned aerial vehicle body.
- 2. the multi-functional unmanned plane undercarriage of horizontal according to claim 1, it is characterised in that：In left undercarriage frame body On the front side wall of left front load supporting tube, before the right side of right landing gear frame body several are respectively equipped with the front side wall of load supporting tube The flash lamp lamp cap being serially connected, photoflash controller is equipped with the left back load supporting tube of left undercarriage frame body, these Flash lamp lamp cap connects the output terminal of photoflash controller, the input terminal and unmanned plane of photoflash controller by undercarriage inside conductor The output terminal connection of master controller in fuselage, storage battery are powered for flash lamp lamp cap.
- 3. the multi-functional unmanned plane undercarriage of horizontal according to claim 1 or 2, it is characterised in that：In left undercarriage frame The front end of the left landing pipe of body is equipped with searchlight lamp cap, and storage battery is powered for searchlight lamp cap.
- 4. the multi-functional unmanned plane undercarriage of horizontal according to claim 3, it is characterised in that：In left undercarriage frame body Rear portion in left landing pipe is equipped with telescopic rod sleeve, and the telescopic rod that more piece can pull out or retract is included in flexible rod sleeve, The wedge shape pulled out on the bottom outer wall of every section telescopic rod equipped with the telescopic rod retraction for preventing from stretching out or easy to the telescopic rod of retraction Spring Card.
- 5. the multi-functional unmanned plane undercarriage of horizontal according to claim 4, it is characterised in that：Telescopic rod is saved in outermost one Top be equipped with and be used to hang the telescopic rod top circular hole of screw type annulus, one end of suspension screw type annulus is hooked in outermost one and saves In the telescopic rod top circular hole of telescopic rod, the other end of suspension screw type annulus hooks another for the power supply of another frame unmanned plane Outdoor charging conductor.
- 6. the multi-functional unmanned plane undercarriage of horizontal according to claim 5, it is characterised in that：In left undercarriage frame body The rear end outer wall of left landing pipe is equipped with external screw thread, and the internal thread coordinated with external screw thread is equipped with the inner wall of telescopic rod pole cap.
- 7. the multi-functional unmanned plane undercarriage of horizontal according to claim 6, it is characterised in that：In the rear end of right landing pipe The mouth of pipe is equipped with the second magnechuck.
- 8. the multi-functional unmanned plane undercarriage of horizontal according to claim 1 or 2, it is characterised in that：In left undercarriage frame Rear portion in the left landing pipe of body is equipped with telescopic rod sleeve, flexible rod sleeve include more piece can pull out or retract it is flexible Pole, the wedge pulled out on the bottom outer wall of every section telescopic rod equipped with the telescopic rod retraction for preventing from stretching out or easy to the telescopic rod of retraction Shape Spring Card.
- 9. the multi-functional unmanned plane undercarriage of horizontal according to claim 8, it is characterised in that：In the rear end of right landing pipe The mouth of pipe is equipped with the second magnechuck.
- 10. the multi-functional unmanned plane undercarriage of horizontal according to claim 1 or 2, it is characterised in that：In right landing pipe The rear end mouth of pipe is equipped with the second magnechuck.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720903261.3U CN207225643U (en) | 2017-07-25 | 2017-07-25 | The multi-functional unmanned plane undercarriage of horizontal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720903261.3U CN207225643U (en) | 2017-07-25 | 2017-07-25 | The multi-functional unmanned plane undercarriage of horizontal |
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| Publication Number | Publication Date |
|---|---|
| CN207225643U true CN207225643U (en) | 2018-04-13 |
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ID=61853624
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720903261.3U Expired - Fee Related CN207225643U (en) | 2017-07-25 | 2017-07-25 | The multi-functional unmanned plane undercarriage of horizontal |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423158A (en) * | 2018-05-11 | 2018-08-21 | 福建中量智汇科技有限公司 | A kind of luminous undercarriage of unmanned plane |
| CN112912310A (en) * | 2018-09-11 | 2021-06-04 | 马克·霍尔布洛克·汉纳 | Unmanned transport aircraft with distributed batteries and power supply method thereof |
| CN113460315A (en) * | 2020-03-30 | 2021-10-01 | 古洛布莱株式会社 | Telescopic wire guiding tool |
| CN113697102A (en) * | 2020-05-22 | 2021-11-26 | 古洛布莱株式会社 | Telescopic wire guide device with drop-preventing member |
-
2017
- 2017-07-25 CN CN201720903261.3U patent/CN207225643U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423158A (en) * | 2018-05-11 | 2018-08-21 | 福建中量智汇科技有限公司 | A kind of luminous undercarriage of unmanned plane |
| CN112912310A (en) * | 2018-09-11 | 2021-06-04 | 马克·霍尔布洛克·汉纳 | Unmanned transport aircraft with distributed batteries and power supply method thereof |
| CN113460315A (en) * | 2020-03-30 | 2021-10-01 | 古洛布莱株式会社 | Telescopic wire guiding tool |
| CN113697102A (en) * | 2020-05-22 | 2021-11-26 | 古洛布莱株式会社 | Telescopic wire guide device with drop-preventing member |
| CN113697102B (en) * | 2020-05-22 | 2024-03-26 | 古洛布莱株式会社 | Telescopic wire guide with drop-preventing member |
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