CN108725821A - A kind of dual-purpose portable unmanned plane launching platform - Google Patents
A kind of dual-purpose portable unmanned plane launching platform Download PDFInfo
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- CN108725821A CN108725821A CN201810405950.0A CN201810405950A CN108725821A CN 108725821 A CN108725821 A CN 108725821A CN 201810405950 A CN201810405950 A CN 201810405950A CN 108725821 A CN108725821 A CN 108725821A
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- platform
- dual
- hinged
- slot
- unmanned plane
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- 210000001015 abdomen Anatomy 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000000354 decomposition reaction Methods 0.000 description 2
- 206010044565 Tremor Diseases 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The present invention discloses a kind of dual-purpose portable unmanned plane launching platform,Including supporting rack,Support frame as described above lower end edge central shaft be hinged with it is multiple can be by supporting rack with respect to ground fixed folding supporting legs vertically,The dual-purpose apparatus that can be taken off for unmanned plane and can be used for fixing unmanned controller is screwed on support frame as described above top,The locking device of remote controler can be fixed by being symmetrically hinged on the dual-purpose apparatus,The object of the present invention is to provide a kind of using the platform that is screwed on portable support frame,Folding supporting legs ensure in the case of the out-of-flatness of ground platform remain unchanged can holding level be that multi-rotor unmanned aerial vehicle takes off and provides suitable condition,Dual-purpose platform can regard the auxiliary fixing device of unmanned controller when platform is used alone,Still user's body can be kept away to avoid falling or remote controler overturning touches caused by user's body control lever and accidentally touches phenomenon even if both hands can be provided and decontroled,The device of safe ready is in-flight provided for unmanned plane fan.
Description
Technical field
The present invention relates to kind of a dual-purpose portable unmanned plane launching platforms.
Background technology
Unmanned plane is more and more in life now sees, and increases with the fan of unmanned plane, and many places are all done
The policy that limitation unmanned plane flies in city is gone out, place can only be chosen some human footmarks by many multi-rotor unmanned aerial vehicle fans
Seldom mountain area extremely goes flight to shoot, but because multi-rotor unmanned aerial vehicle limiting so that on the ground of mountain area out-of-flatness because of takeoff condition
Can not safe take-off, or even because air-flow shakiness causes to fall when ground out-of-flatness or takeoff point nearby have shelter to cause to take off
Machine hurts user and surrounding people, and unmanned plane many times needs one-handed performance remote controler another in landing
Hand connects aircraft or closes aircraft power supply so that often will appear one hand and holds and holds that remote controler is unstable to cause remote controler to fall or be remotely controlled
Device overturning touches control lever caused by user's body and accidentally touches phenomenon to cause aircraft is out of control to hurt user and surrounding
Personnel cause a hidden trouble to flight safety.
Invention content
Place that purpose of the invention is to overcome the shortcomings in the prior art, provides kind of a dual-purpose portable unmanned plane and takes off
Platform.
In order to achieve the above object, the present invention uses following scheme：
A kind of dual-purpose portable unmanned plane launching platform, it is characterised in that：Including supporting rack, in support frame as described above lower end edge
Central shaft, which is hinged with, multiple can be screwed with by supporting rack with respect to ground fixed folding supporting legs vertically on support frame as described above top
The dual-purpose apparatus that can take off and can be used for fixing unmanned controller for unmanned plane, energy is symmetrically hinged on the dual-purpose apparatus
The locking device of fixed remote controler.
A kind of dual-purpose portable unmanned plane launching platform as described above, it is characterised in that：The dual-purpose apparatus includes rotation
It is connected on the energy landing on supporting rack top and places the platform of unmanned controller, the locking device is respectively hinged at platform two
End, is arranged with T-type sliding slot in the mesa base, T-type sliding block is movably equipped in the T-type sliding slot, in the T-type sliding block
It is upper to be arranged with hinged ear positioned at T-type sliding slot opening one end, it is hinged with connecting tube in the hinged ear, in the connecting tube
It is inside plugged with the telescopic rod of the opposite connecting tube collapsing length of energy, the telescopic rod passes through curved support with another telescopic rod end
Plate is connected, and curved support plate side, which is equipped with, can make curved support plate top pressure prevent curved support plate in operator's abdomen
The fixation band of landing is equipped with the lanyard that can be hung on operator's neck in described platform one end.
A kind of dual-purpose portable unmanned plane launching platform as described above, it is characterised in that：The locking device includes hinge
Open folded sheet can be overturn by being connected on platform left and right ends, and pull slot is equipped on the folded sheet, grafting in the pull slot
There is the card pressing plate that can push locking unmanned controller to prevent remote controler from skidding off platform, is located at pull slot in the card pressing plate
Interior bottom both ends are respectively equipped with anti-off board, and the guide groove being connected with pull slot is respectively equipped at the folded sheet both ends,
Guide post is equipped in the guide groove, the anti-off board is set in guide post, and card can be kept by being arranged in the guide post
The resetting spring of pressure under pressing plate, the resetting spring are arranged between anticreep plate top surface and guide groove side inner wall.
A kind of dual-purpose portable unmanned plane launching platform as described above, it is characterised in that：In the platform left and right ends
It is arranged with axle bed, articulated shaft is equipped in described folded sheet one end, card slot is equipped in described articulated shaft one end, in the axle bed one
End is equipped with deck, and the folded sheet is hinged on by articulated shaft in axle bed, and articulated shaft can be locked by being equipped with to be plugged in the card slot
The fixture block of rotation is connected with card column in described fixture block one end, and described card column one end passes through deck side and stretches out outside deck, in institute
It states card column and is located at the end of the outer side of deck and be connected with adjusting block, the limitation that can prevent card column from rotating is equipped in the card column
Block, runs through in the deck side and is equipped with limiting slot, and the confinement block is arranged in limiting slot.
A kind of dual-purpose portable unmanned plane launching platform as described above, it is characterised in that：It is equipped in the connecting tube
Straight slot is hinged with locking buckle in age straight slot side, is equipped with lock slots, described locking buckle one end card successively on the telescopic rod
It is pressed in lock slots, in the locking buckle side, top pressure, which has, can make locking buckle be maintained at the top pressure spring in lock slots.
In conclusion advantage is the present invention compared with the existing technology：
The present invention is using the platform of be screwed on portable support frame energy landing and placement unmanned controller, folding supporting legs guarantee
On mountain area ground in the case of out-of-flatness platform remain unchanged can holding level be that multi-rotor unmanned aerial vehicle takes off and provides the suitable item that takes off
Part reduces the hidden danger that the air crash caused by taking off injures user or left side personnel, and dual-purpose platform can when platform is used alone
As the auxiliary fixing device of unmanned controller, though can provide both hands decontrol still can be kept away from user's body from
And avoid falling or remote controler overturning touches control lever caused by user's body and accidentally touches phenomenon, it flies for unmanned plane fan
The middle device that safe ready is provided.
Description of the drawings
Fig. 1 is one of the stereoscopic schematic diagram of the present invention；
Fig. 2 is the two of the stereoscopic schematic diagram of the present invention；
Fig. 3 is one of the decomposition diagram of the present invention；
Fig. 4 is the two of the enlargement decomposition of the present invention；
Fig. 5 is enlarged drawing at A in Fig. 3.
Specific implementation mode
The invention will be further described with specific implementation mode for explanation below in conjunction with the accompanying drawings：
A kind of dual-purpose portable unmanned plane launching platform as shown in Fig. 1 to 5, including supporting rack 1, in support frame as described above 1
Lower end edge central shaft be hinged with it is multiple can be by supporting rack 1 with respect to ground fixed folding supporting legs 4 vertically, in support frame as described above 1
Top is screwed with the dual-purpose apparatus 2 that can be taken off for unmanned plane and can be used for fixing unmanned controller, on the dual-purpose apparatus 2
It symmetrically is hinged with the locking device 3 that can fix remote controler, folding supporting legs ensure the platform in the case of out-of-flatness of mountain area ground
It can still keep plateau levels to take off for multi-rotor unmanned aerial vehicle and suitable takeoff condition is provided, the conduct when taking off of dual-purpose apparatus 2
Platform is taken off, the auxiliary device of fixed remote controler is usually can be used as, remote controler smoothly can be fixed on two by locking device 3
With on device 2.
Heretofore described dual-purpose apparatus 2 includes being screwed in the energy landing on 1 top of supporting rack and placing no-manned machine distant control
The platform 4 of device, the locking device 3 are respectively hinged at 4 both ends of platform, and T-type sliding slot 5 is equipped in 4 bottom symmetrical of the platform,
It is movably equipped with T-type sliding block 51 in the T-type sliding slot 5, is symmetrically set positioned at 5 opening one end of T-type sliding slot on the T-type sliding block 51
There is hinged ear 52, connecting tube 21 is hinged in the hinged ear 52, being plugged in the connecting tube 21 can opposite connecting tube
The telescopic rod 22 of 21 collapsing lengths, the telescopic rod 22 are connected with another 22 end of telescopic rod by curved support plate 23,
23 side of curved support plate, which is equipped with, can make 23 top pressure of curved support plate prevent curved support plate 23 from sliding in operator's abdomen
The fixation band 24 fallen is equipped with the lanyard 25 that can be hung on operator's neck in 4 one end of the platform, and 4 one end of platform passes through lanyard
25 hang over platform 4 on user's neck, and curved support plate 23 is coordinated fixed band 24 by the other end by the telescopic rod 22 of bottom
Before platform 4 is stably fixed to user's body, opening telescopic rod allows platform 4 to be kept away from user's body, ensures distant
The distant bar of control device will not accidentally touch user's body and cause aircraft out of control.
Heretofore described locking device 3 includes being hinged on 4 left and right ends of platform to overturn open folded sheet 31,
The folded sheet 31 is equipped with pull slot 32, and locking unmanned controller can be pushed to prevent by being plugged in the pull slot 32
Remote controler skids off the card pressing plate 33 of platform 4, and being located at the bottom both ends in pull slot 32 in the card pressing plate 33 is respectively equipped with anticreep
Plate 34 is respectively equipped with the guide groove 35 being connected with pull slot 32 at 31 both ends of the folded sheet, is set in the guide groove 35
There are guide post 36, the anti-off board 34 to be set in guide post 36, card pressing plate 33 can be kept by being arranged in the guide post 36
The resetting spring 37 of lower pressure, the resetting spring 37 are arranged between 35 side inner wall of 34 top surface of anti-off board and guide groove, need
By 31 opposed platforms of folded sheet, 4 tipped upright when fixing remote controler, 33 clamping remote controler both ends of card pressing plate are pulled open.
Heretofore described 4 left and right ends of platform are arranged with axle bed 41, are equipped in 31 one end of the folded sheet hinged
Axis 42 is equipped with card slot 421 in 42 one end of the articulated shaft, is equipped with deck 43 in 41 one end of the axle bed, the folded sheet 31 is logical
It crosses articulated shaft 42 to be hinged in axle bed 41, the fixture block 44 for being plugged with and capable of locking articulated shaft rotation is equipped in the card slot 421, in institute
It states 44 one end of fixture block and is connected with card column 45,45 one end of the card column passes through 43 side of deck and stretches out outside deck 43, in the card
The end that column 45 is located at 43 outer side of deck is connected with adjusting block 46, and the rotation of card column 45 can be prevented by being equipped in the card column 45
Confinement block 47 runs through in 43 side of the deck and is equipped with limiting slot 48, and the confinement block 47 is arranged in limiting slot 48, pulls and adjusts
Locking nub 46 makes fixture block 44 be detached from the card slot 421 of 42 one end of articulated shaft, to make folded sheet 31 freely overturn, otherwise is pushed into adjusting block
46 make the fixture block 44 of 45 one end of card column be inserted into card slot 421 to make 31 opposed platforms 4 of folded sheet that can not rotate, and confinement block 47 is matched
It closes limiting slot 48 and ensures that card column 45 can not be rotated and can only be axially moveable.
Heretofore described connecting tube 21 is equipped with straight slot 6, locking buckle 61 is hinged in 6 side of age straight slot, in institute
It states and is equipped with lock slots 62 on telescopic rod 22 successively, 61 one end card of the locking buckle is pressed in lock slots 62, in the locking buckle 61
Side top pressure has the top pressure spring 63 that locking buckle 61 can be made to be maintained in lock slots 62, and pressing 61 one end of locking buckle makes locking buckle 61
The other end is lifted out of lock slots 62, to allow telescopic rod 22 to move.
The basic principles and main features and advantages of the present invention of the present invention, the skill of the industry has been shown and described above
Art personnel it should be appreciated that the present invention is not limited to the above embodiments, the above embodiments and description only describe
The principle of the present invention, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these
Changes and improvements all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and
Its equivalent thereof.
Claims (5)
1. a kind of dual-purpose portable unmanned plane launching platform, it is characterised in that：Including supporting rack (1), under support frame as described above (1)
End along central shaft be hinged with it is multiple can be by supporting rack (1) with respect to ground fixed folding supporting legs (4) vertically, in support frame as described above
(1) top is screwed with the dual-purpose apparatus (2) that can be taken off for unmanned plane and can be used for fixing unmanned controller, in the dual-purpose dress
It sets and is symmetrically hinged with the locking device (3) that can fix remote controler on (2).
2. a kind of dual-purpose portable unmanned plane launching platform according to claim 1, it is characterised in that：The dual-purpose apparatus
(2) include the energy landing for being screwed in supporting rack (1) top and the platform (4) for placing unmanned controller, the locking device (3)
Platform (4) both ends are respectively hinged at, T-type sliding slot (5) are equipped in the platform (4) bottom symmetrical, in the T-type sliding slot (5)
It is movably equipped with T-type sliding block (51), hinged ear is arranged with positioned at T-type sliding slot (5) opening one end on the T-type sliding block (51)
(52), it is hinged with connecting tube (21) in the hinged ear (52), being plugged in the connecting tube (21) can opposite connecting tube
(21) telescopic rod (22) of collapsing length, the telescopic rod (22) pass through curved support plate with another telescopic rod (22) end
(23) it is connected, curved support plate (23) side, which is equipped with, can be such that curved support plate (23) top pressure is prevented in operator's abdomen
The fixed band (24) that curved support plate (23) slides, the lanyard that can be hung on operator's neck is equipped in the platform (4) one end
(25)。
3. a kind of dual-purpose portable unmanned plane launching platform according to claim 1, it is characterised in that：The locking device
(3) include being hinged on platform (4) left and right ends to overturn open folded sheet (31), pull is equipped on the folded sheet (31)
Slot (32), interior be plugged with of the pull slot (32) can push locking unmanned controller to prevent remote controler from skidding off platform (4)
Card pressing plate (33), be located at the bottom both ends in pull slot (32) in the card pressing plate (33) and be respectively equipped with anti-off board (34),
Folded sheet (31) both ends are respectively equipped with the guide groove (35) being connected with pull slot (32), are set in the guide groove (35)
There are guide post (36), the anti-off board (34) to be set in guide post (36), being arranged in the guide post (36) can keep
The resetting spring (37) of pressure under card pressing plate (33), the resetting spring (37) are arranged in anti-off board (34) top surface and guide groove
(35) between the inner wall of side.
4. a kind of dual-purpose portable unmanned plane launching platform according to claim 1, it is characterised in that：In the platform
(4) left and right ends are arranged with axle bed (41), articulated shaft (42) are equipped in the folded sheet (31) one end, in the articulated shaft
(42) one end is equipped with card slot (421), is equipped with deck (43) in the axle bed (41) one end, the folded sheet (31) passes through articulated shaft
(42) it is hinged in axle bed (41), the fixture block (44) for being plugged with and capable of locking articulated shaft rotation is equipped in the card slot (421), in institute
It states fixture block (44) one end and is connected with card column (45), described card column (45) one end passes through deck (43) side and stretches out deck (43)
Outside, the end for deck (43) outer side being located in the card column (45) is connected with adjusting block (46), is set in the card column (45)
There is the confinement block (47) that can prevent card column (45) from rotating, runs through in the deck (43) side and be equipped with limiting slot (48), the limit
Clamp dog (47) setting is in limiting slot (48).
5. a kind of dual-purpose portable unmanned plane launching platform according to claim 2, it is characterised in that：In the connecting tube
(21) it is equipped with straight slot (6), locking buckle (61) is hinged in the straight slot (6) side, is set successively on the telescopic rod (22)
There are lock slots (62), described locking buckle (61) one end card to be pressed in lock slots (62), top pressure has in the locking buckle (61) side
It can make the top pressure spring (63) that locking buckle (61) is maintained in lock slots (62).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810405950.0A CN108725821B (en) | 2018-04-30 | 2018-04-30 | Dual-purpose portable unmanned aerial vehicle platform of taking off |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810405950.0A CN108725821B (en) | 2018-04-30 | 2018-04-30 | Dual-purpose portable unmanned aerial vehicle platform of taking off |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108725821A true CN108725821A (en) | 2018-11-02 |
| CN108725821B CN108725821B (en) | 2021-08-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810405950.0A Active CN108725821B (en) | 2018-04-30 | 2018-04-30 | Dual-purpose portable unmanned aerial vehicle platform of taking off |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110254735A (en) * | 2019-05-07 | 2019-09-20 | 国网吉林省电力有限公司长春供电公司 | The full landform self-balancing landing platform of multi-rotor unmanned aerial vehicle |
| CN110937126A (en) * | 2019-12-20 | 2020-03-31 | 西北工业大学 | Unmanned aerial vehicle takes off and retrieves charging device |
| CN112208762A (en) * | 2020-09-25 | 2021-01-12 | 赵荣菊 | Aerial monitoring formula unmanned aerial vehicle |
| CN112589989A (en) * | 2020-12-10 | 2021-04-02 | 滁州市悦鹏设备有限公司 | Quick die change device of mould for building |
| CN112937905A (en) * | 2021-03-22 | 2021-06-11 | 泰山学院 | Seeding formula unmanned aerial vehicle auxiliary device that takes off based on thing networked control |
| CN113859564A (en) * | 2021-10-09 | 2021-12-31 | 国网河北省电力有限公司检修分公司 | Supplementary lift operation platform under unmanned aerial vehicle all terrain environment |
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| CN206651492U (en) * | 2017-03-03 | 2017-11-21 | 巢湖学院 | A kind of lunch box |
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| EP2103518A2 (en) * | 2008-03-19 | 2009-09-23 | Honeywell International Inc. | Launch and capture systems for vertical take-off and landing (VTOL) vehicles |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110254735A (en) * | 2019-05-07 | 2019-09-20 | 国网吉林省电力有限公司长春供电公司 | The full landform self-balancing landing platform of multi-rotor unmanned aerial vehicle |
| CN110937126A (en) * | 2019-12-20 | 2020-03-31 | 西北工业大学 | Unmanned aerial vehicle takes off and retrieves charging device |
| CN110937126B (en) * | 2019-12-20 | 2021-02-02 | 西北工业大学 | Unmanned aerial vehicle takes off and retrieves charging device |
| CN112208762A (en) * | 2020-09-25 | 2021-01-12 | 赵荣菊 | Aerial monitoring formula unmanned aerial vehicle |
| CN112589989A (en) * | 2020-12-10 | 2021-04-02 | 滁州市悦鹏设备有限公司 | Quick die change device of mould for building |
| CN112937905A (en) * | 2021-03-22 | 2021-06-11 | 泰山学院 | Seeding formula unmanned aerial vehicle auxiliary device that takes off based on thing networked control |
| CN113859564A (en) * | 2021-10-09 | 2021-12-31 | 国网河北省电力有限公司检修分公司 | Supplementary lift operation platform under unmanned aerial vehicle all terrain environment |
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| Publication number | Publication date |
|---|---|
| CN108725821B (en) | 2021-08-20 |
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Effective date of registration: 20240423 Address after: 719000 Shop 1, Jinlin Community, Yima Road, Yuyang District, Yulin City, Shaanxi Province Patentee after: Yuhe Aircraft Manufacturing Co.,Ltd. in Yuyang District Yulin City Country or region after: China Address before: 719000 shop on the second floor of building 3, Yuyang East Village resettlement community, Xiyi Road, Yuyang District, Yulin City, Shaanxi Province Patentee before: Shaanxi Blue Sky Aviation Club Co.,Ltd. Country or region before: China |
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