CN106274625B - A kind of mechanical arm type unmanned plane hoistable platform - Google Patents
A kind of mechanical arm type unmanned plane hoistable platform Download PDFInfo
- Publication number
- CN106274625B CN106274625B CN201610771153.5A CN201610771153A CN106274625B CN 106274625 B CN106274625 B CN 106274625B CN 201610771153 A CN201610771153 A CN 201610771153A CN 106274625 B CN106274625 B CN 106274625B
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- rack
- rotation
- cabin
- unmanned plane
- main shaft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Transportation (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Conveying And Assembling Of Building Elements In Situ (AREA)
Abstract
The invention discloses a kind of mechanical arm type unmanned plane hoistable platforms, including the interior rack for cabin and the main shaft being arranged in rack, rotating arm one end is fixed on main shaft, and other end connection is supported by the lifter plate for carrying unmanned plane, and lifter plate is stretched out rack from hatch with main axis by rotating arm.The present invention inside sets rotating arm using rack as cabin, by the rotation of rotating arm, realizes the discrepancy cabin operation of unmanned plane hoistable platform；Swing boom configuration design of the invention simultaneously can reduce unmanned plane hoistable platform and enter and leave the space occupied during cabin；And the rack and its internal structure of the application can be used as a basic module, can combine multiple basic modules and be mounted in a cabin, realize the discrepancy cabin of multiple unmanned plane hoistable platforms.
Description
Technical field
The present invention relates to unmanned plane platform carrier more particularly to a kind of mechanical arm type unmanned plane hoistable platforms.
Background technique
The fields such as monitoring, the disaster relief, security are applied to as light-duty unmanned plane is large batch of, vehicle-mounted unmanned aerial vehicle hoistable platform is urgently
Need to correspondingly it develop perfect.The landing technology of independently taking off of vehicle-mounted unmanned aerial vehicle hoistable platform is also immature at present, such as application number
For a kind of 201520784719.9 autonomous launching apparatus of vehicle-mounted unmanned aerial vehicle, be unmanned aerial vehicle platform is fixed on to automobile top, or
It is then that unmanned plane will be installed to take off ejection application No. is 201520036064.7 vehicle-mounted unmanned aerial vehicle emergency monitoring integration apparatus
In the car, above-mentioned design all existing defects, unmanned plane first must be previously installed at roof by the former for the creeper truck placement of frame, nobody
Influence of the machine vulnerable to ambient enviroment is easy to cause to damage to unmanned plane when there are the extreme climates such as sand and dust；Although the latter exists
Automotive interior, but when emitting unmanned plane, need to output creeper truck outside automobile, consuming time is long, and works as vehicle periphery
When environment does not allow creeper truck to be steadily unfolded, unmanned plane cannot be emitted.
Summary of the invention
The purpose of the present invention is for defect existing for existing unmanned plane hoistable platform carrier, providing one kind can be by nobody
Machine hoistable platform disposes in the car, only a kind of mechanical arm outside the auto-extending vehicle of unmanned plane hoistable platform part when realizing work
Formula unmanned plane hoistable platform.
To solve the above problems, the invention provides the following technical scheme: a kind of mechanical arm type unmanned plane hoistable platform, including
The interior rack for cabin and the main shaft being arranged in rack, rotating arm one end are fixed on main shaft, and other end connection support is useful
In the lifter plate of carrying unmanned plane, lifter plate is stretched out rack from hatch with main axis by rotating arm.
The rotating arm includes rotation forearm and rotation postbrachium, wherein the one end for rotating forearm is fixedly connected with main shaft, separately
One end hinge-connection of one end and rotation postbrachium, the rotation postbrachium other end are fixed with lifter plate；One is provided on the rotation forearm
Electric pushrod, the push rod end of electric pushrod are fixed on rotation postbrachium.
The rotation postbrachium is provided with two, and two rotation postbrachiums form V-structure, and described rotation forearm one end passes through switching
The connection of the bottom of axis and V-structure, the V-structure top are fixedly connected with lifter plate, the push rod end of the electric pushrod
It is fixed therein on a rotation postbrachium.
The rotation forearm is also equipped with two, and one end of two rotation forearms is connect with main shaft, and the other end is separately connected
On the top and end of shaft, the middle section of shaft is connect with rotation postbrachium.
It is additionally provided with out cabin limit switch in the rack and receives cabin limit switch, rotating arm collides out cabin limit after going out cabin
Switch stalls main shaft, and collision receipts cabin limit switch stalls main shaft after rotating arm enters cabin.
The rack is equipped with the decelerating motor for driving spindle, and the main shaft is vertically installed in rack.
The main shaft is vertically arranged in rack hatch support prism side.
The rack designs for rectangular parallelepiped structure.
Including several racks, it is fixedly connected between adjacent rack and keeps rack hatch exposed.
Compared with prior art, the present invention at least has the advantages that rotation of the present invention by rotating arm, realizes
Unmanned plane hoistable platform is in rack when not working, and unmanned plane hoistable platform stretches out rack when work, passes through side door opening, stretches out
Purpose outside vehicle；
Further, by setting rotation forearm and rotation postbrachium, constituting tool, there are two the mechanical arms in joint, by twice
Rotation, it is possible to reduce unmanned plane hoistable platform enters and leaves the space occupied during cabin；
Further, by the way that cabin limit switch is provided, when unmanned plane being avoided to go out cabin, rotation forearm rotation is excessive, with vehicle
Window segment collides, and receives cabin limit switch by setting, guarantees that unmanned plane hoistable platform in rack space, will not occupy machine
Part outside frame, while the setting of cabin limit switch and receipts cabin limit switch can guarantee after rotating forearm in-position out, subtract
Speed motor stops working, more accurate positioning；
Further, limit main shaft and be vertically arranged in rack hatch support prism side, guarantee rotating arm around be side into
Row rotation can more be widely used in side enabling or back pullout (BPO) vehicle；
Further, the frame of the invention is rectangular parallelepiped structure, can be by multiple basic module groups as a basic module
Conjunction is mounted in a cabin, such as superposition up and down, the modes such as left and right superposition, as long as guaranteeing that the egress hatch of each rack is all outer
Reveal the discrepancy cabin, it can be achieved that multiple unmanned plane hoistable platforms, realizes interior space using maximization.
Detailed description of the invention
Fig. 1 is that the present invention receives cabin state top view；
Fig. 2 is reservoir status top view of the present invention；
Fig. 3 is receipts cabin state main view of the invention；
Fig. 4 is 3 mechanical arm type unmanned plane hoistable platform combining structure schematic diagrams.
1 is rack in figure, and 2 be decelerating motor, and 3 be main shaft, and 4 be rotation forearm, and 5 be Coupling Shaft, and 6 be rotation postbrachium, and 7 are
Electric pushrod, 8 be lifter plate, and 9 is go out cabin limit switch, and 10 be receipts cabin limit switch.
Specific embodiment
The present invention will be further described with reference to the accompanying drawing, and but the scope of the present invention is not limited thereto.
As illustrated in fig. 1 and 2, mechanical arm type unmanned plane hoistable platform of the present invention exists including the interior rack 1 for cabin and setting
Main shaft 3 in rack 1, rotating arm one end are fixed on main shaft 3, and other end connection is supported by the lifter plate for carrying unmanned plane
8, rotating arm is rotated with main shaft 3 stretches out rack 1 from hatch for lifter plate 8；Rack 1 is equipped with the deceleration electricity for driving spindle 3
Machine 2, main shaft 3 are vertically arranged in 1 hatch of rack support prism side, and rotating arm includes rotation forearm 4 and rotation postbrachium 6, wherein
One end of rotation forearm 4 is fixedly connected with main shaft 3, and one end hinge-connection of the other end and rotation postbrachium 6 rotates 6 other end of postbrachium
It is fixed with lifter plate 8；An electric pushrod 7 is provided on rotation forearm 4, the push rod end of electric pushrod 7 is fixed on rotation postbrachium 6
On；
As shown in Fig. 2, rotation postbrachium 6 is provided with two, two rotation postbrachiums 6 form V-structure, and rotation 4 one end of forearm is logical
It crosses Coupling Shaft 5 to connect with the bottom of V-structure, be fixedly connected at the top of V-structure with lifter plate 8, the push rod end of electric pushrod 7
It is fixed therein on a rotation postbrachium 6；As shown in figure 3, rotation forearm 4 is also equipped with two, one end of two rotation forearms 4
It is connect with main shaft 3, the other end is connected to the top and end of shaft 5, and the middle section of shaft 5 is connect with rotation postbrachium 6；Slow down
Motor 2 is rotated by the driving rotation forearm 4 of main shaft 3 around main shaft 3, and rotation forearm 4 and rotation postbrachium 6 are connected by the rotation of Coupling Shaft 5
It connects.
It is additionally provided with out cabin limit switch 9 in rack 1 and receives cabin limit switch 10, rotating arm touches out cabin limit after going out cabin
Bit switch 9 stalls main shaft 3, and rotating arm, which enters to touch behind cabin, to be received cabin limit switch 10 and stall main shaft 3, and effect is to limit rotation
The displacement of forearm 4；
The mechanical arm type unmanned plane hoistable platform course of work of the present invention is as follows:
Cabin operating procedure is as follows out:
When lifter plate 8 goes out cabin, decelerating motor 2 is rotated forward, and outputs power to main shaft 3, and main shaft 3 rotates, and then drives rotation
Turning forearm 4 around main shaft 3 is rotary shaft rotation, and the lifter plate 8 for driving rotation postbrachium 6 and being fixed on rotation postbrachium 6 rotates, and works as rotation
After turning the position that forearm 4 reaches out cabin limit switch 9, decelerating motor 2 is powered off, and rotation forearm 4 stops operating, at this point, being fixed on
The electric pushrod 7 rotated on forearm 4 is started to work, and electric pushrod 7 pushes rotation postbrachium 6 to rotate forearm 4 and rotate postbrachium 6
Rotating connecting part Coupling Shaft 5 is rotary shaft rotation, drives the lifter plate 8 being fixed on rotation postbrachium 6 to rotate, by turning twice
Dynamic, that realizes lifter plate 8 goes out cabin.
It is as follows to receive cabin operating procedure:
Electric pushrod 7, which is pulled back, first rotates postbrachium 6, and following decelerating motor 2, which is powered, to be inverted, and rotation forearm 4 is driven to invert,
After rotating the arrival receipts cabin limit switch 10 of forearm 4, decelerating motor 2 is powered off, and rotation forearm 4 stops rotating, and realizes lifter plate 8
Receive cabin operation.
In present embodiment, rack 1 designs for rectangular parallelepiped structure, and length is according to the size of lifter plate 8, rotation
Forearm 4 and rotate the size of postbrachium 6 and distance that lifter plate 8 stretches out outside vehicle determines；Simultaneously 2 rotation time of decelerating motor and
Electric pushrod 7 can be adjusted according to rotation forearm 4 and rotation 6 running track of postbrachium.
The position for going out cabin limit switch 9 and receiving cabin limit switch 10 being arranged in the present invention is according to unmanned plane hoistable platform
Any position of vehicle window is not touched when cabin out, after entering cabin, rotate forearm 4 and lifter plate 8 all is not have in the rack 1 of cabin inside
Any position is stretched out outside rack 1 to be gone to set for standard.
Rack 1 is rectangular parallelepiped structure in present embodiment, can be used as a unmanned plane lifting basic module, in cabin
Multiple basic modules can be combined according to cabin size, car door direction, as shown in figure 3, different unmanned plane liftings are basic
Module carry out up and down, left and right stack, as long as guaranteeing not blocking the face that the rotation of rotating arm in any one basic module enters and leaves, energy
Realize the discrepancy cabin of lifter plate in each basic module.
The foregoing is merely presently preferred embodiments of the present invention, all equivalent changes done according to scope of the present invention patent with
Modification, is all covered by the present invention.
Claims (5)
1. a kind of mechanical arm type unmanned plane hoistable platform, it is characterised in that: including the interior rack (1) for cabin and be arranged in rack
(1) main shaft (3) in, rotating arm one end are fixed on main shaft (3), and other end connection is supported by the lifting for carrying unmanned plane
Plate (8), rotating arm is rotated with main shaft (3) stretches out rack from hatch for lifter plate (8)；
The rotating arm includes rotation forearm (4) and rotation postbrachium (6), wherein one end and main shaft (3) of rotation forearm (4) are solid
Fixed connection, one end hinge-connection of the other end and rotation postbrachium (6), rotation postbrachium (6) other end and lifter plate (8) are fixed；It is described
It is provided with an electric pushrod (7) in rotation forearm (4), the push rod end of electric pushrod (7) is fixed in rotation postbrachium (6)；
The rotation postbrachium (6) is provided with two, and two rotations postbrachium (6) form V-structure, and the rotation forearm (4) one end is logical
It crosses Coupling Shaft (5) to connect with the bottom of V-structure, be fixedly connected at the top of the V-structure with lifter plate (8), it is described electronic to push away
The push rod end of bar (7) is fixed therein on a rotation postbrachium (6)；
The rotation forearm (4) is also equipped with two, and one end of two rotations forearm (4) is connect with main shaft (3), other end difference
It is connected to the top and end of Coupling Shaft (5), the middle section of Coupling Shaft (5) is connect with rotation postbrachium (6)；
It is additionally provided with out cabin limit switch (9) on the rack (1) and receives cabin limit switch (10), rotating arm collides out after going out cabin
Cabin limit switch (9) stalls main shaft (3), and collision receipts cabin limit switch (10) stall main shaft (3) after rotating arm enters cabin.
2. mechanical arm type unmanned plane hoistable platform according to claim 1, it is characterised in that: the rack (1) is equipped with
For the decelerating motor (2) of driving spindle (3), the main shaft (3) is vertically installed in rack (1).
3. mechanical arm type unmanned plane hoistable platform according to claim 1, it is characterised in that: the main shaft (3) sets vertically
It sets and supports prism side in rack (1) hatch.
4. mechanical arm type unmanned plane hoistable platform according to claim 1, it is characterised in that: the rack (1) is rectangular
The design of body structure.
5. mechanical arm type unmanned plane hoistable platform according to claim 1-4, it is characterised in that: including several machines
Frame (1) is fixedly connected between adjacent rack (1) and keeps rack (1) hatch exposed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610771153.5A CN106274625B (en) | 2016-08-29 | 2016-08-29 | A kind of mechanical arm type unmanned plane hoistable platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610771153.5A CN106274625B (en) | 2016-08-29 | 2016-08-29 | A kind of mechanical arm type unmanned plane hoistable platform |
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| Publication Number | Publication Date |
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| CN106274625A CN106274625A (en) | 2017-01-04 |
| CN106274625B true CN106274625B (en) | 2019-01-22 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610771153.5A Active CN106274625B (en) | 2016-08-29 | 2016-08-29 | A kind of mechanical arm type unmanned plane hoistable platform |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112477768A (en) * | 2019-09-12 | 2021-03-12 | 郑州宇通客车股份有限公司 | Laser radar mounting structure and vehicle |
| CN111231812A (en) * | 2020-03-03 | 2020-06-05 | 陈玲婷 | Police unmanned aerial vehicle-mounted installation device capable of automatically retracting along with sliding door |
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| CN205951803U (en) * | 2016-08-29 | 2017-02-15 | 西安天鹰防务科技有限公司 | Arm -type unmanned aerial vehicle lift platform of machinery |
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| US7410125B2 (en) * | 2005-05-05 | 2008-08-12 | Lockheed Martin Corporation | Robotically assisted launch/capture platform for an unmanned air vehicle |
| US10112710B2 (en) * | 2013-10-15 | 2018-10-30 | Elwha Llc | Motor vehicle with captive aircraft |
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20100132395A (en) * | 2009-06-09 | 2010-12-17 | 정운규 | The landing apparatus fot a pilotless plane |
| CN203986788U (en) * | 2014-06-27 | 2014-12-10 | 浙江工业大学 | Multimedia mobile classroom |
| CN104259164A (en) * | 2014-09-28 | 2015-01-07 | 乐清市金宇石化设备有限公司 | Cleaning machine of oil tank trucks |
| CN105173105A (en) * | 2015-08-04 | 2015-12-23 | 徐州创航科技有限公司 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
| CN205951803U (en) * | 2016-08-29 | 2017-02-15 | 西安天鹰防务科技有限公司 | Arm -type unmanned aerial vehicle lift platform of machinery |
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| CN106274625A (en) | 2017-01-04 |
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| TA01 | Transfer of patent application right |
Effective date of registration: 20181210 Address after: Room 402-404, Unit 1, South Building, District C, 29 Xuehai Road, Xindu Street, South New District, Yancheng City, Jiangsu Province Applicant after: Jiangsu Etam letter Aviation Technology Co. Ltd. Address before: 710075 Room 12302, Kaichuang International Building, High-tech Road, Xi'an High-tech Zone, Shaanxi Province Applicant before: XI'AN SKYHAWK DEFENSE TECHNOLOGY CO., LTD. |
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