CN206374991U - A kind of new unmanned plane battery compartment - Google Patents

A kind of new unmanned plane battery compartment Download PDF

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Publication number
CN206374991U
CN206374991U CN201621155934.3U CN201621155934U CN206374991U CN 206374991 U CN206374991 U CN 206374991U CN 201621155934 U CN201621155934 U CN 201621155934U CN 206374991 U CN206374991 U CN 206374991U
Authority
CN
China
Prior art keywords
end cap
bottom plate
unmanned plane
fixed bottom
battery compartment
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.)
Expired - Fee Related
Application number
CN201621155934.3U
Other languages
Chinese (zh)
Inventor
黄键耿
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang Tianma Xingkong Innovation Technology Co Ltd
Original Assignee
Zhejiang Tianma Xingkong Innovation Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhejiang Tianma Xingkong Innovation Technology Co Ltd filed Critical Zhejiang Tianma Xingkong Innovation Technology Co Ltd
Priority to CN201621155934.3U priority Critical patent/CN206374991U/en
Application granted granted Critical
Publication of CN206374991U publication Critical patent/CN206374991U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of new unmanned plane battery compartment, including lower central plate, fixed bottom plate, side shield, front apron, rear end cap, support column, end cap hinge, Quick bolt.Lower central plate is provided with Quick bolt hole, fixed bottom plate is connected by support column with upper central plate, side shield is surrounded by joinery and its construction, it is connected respectively with upper central plate, front apron and fixed bottom plate, front apron is also provided with joinery and its construction, it is connected respectively with upper central plate, side shield, fixed bottom plate, rear end cap carries out hinge connection with fixed bottom plate by end cap hinge, and Quick bolt is attached to rear end cap by bolt.The utility model unmanned plane battery compartment can realize the quick-replaceable of unmanned machine battery, it is simple to operate, operating efficiency is high, for light-duty unmanned plane, the underlying form of battery can reduce flight and tumble possibility, improve flight stability, and battery is arranged between foot stool within baffle plate, battery can be avoided to be sustained damage in emergency case, safety in utilization is improved.

Description

A kind of new unmanned plane battery compartment
Technical field
The utility model is related to a kind of UAV Components, specifically a kind of new unmanned plane battery compartment.
Background technology
Unmanned plane(Unmanned Aerial Vehicle)Specific boat is exactly performed using wireless remote control or programme-control The aircraft of idle task, refers to a kind of power airborne aircraft for not carrying operating personnel, uses air force to be provided for aircraft Required lift, can automatically fly or remotely guide;Disposable it can also can be reclaimed;Can carry mortality and Non-lethal pay(useful) load.Unmanned plane is by purposes point:It is scounting aeroplane, Electronic Warfare UAV, target drone, anti-radiation drone, right Ground attack unmanned plane, communication relay unmanned plane, cannon relatively penetrate unmanned plane, extraordinary unmanned plane, bait unmanned plane.
In the last few years, middle-size and small-size rotor wing unmanned aerial vehicle be gradually utilized to investigation, measurement, shoot etc. field, but many rotors without Man-machine because its endurance is had to using the larger battery of electricity, but the battery volume of big electricity is larger, to miniature self-service The installation of machine battery is made troubles, and many unmanned planes just lay battery using the binding mode such as VELCRO, and this method is obviously deposited In larger potential safety hazard, once being destroyed serious accident easily occurs for exposed battery.Certainly, there is part unmanned plane The installation of battery is more reliable, but it installs extremely inconvenient with dismounting, or even to use the extracting tool of specialty to dismantle, pacify Dress, the use to unmanned plane brings great inconvenience.Furthermore, many unmanned planes are contour in oar plane by battery mounting arrangement Position or higher position, for loading less SUAV, such layout is easy in unmanned plane deflecting Body is caused to be tumbled, therefore the layout of battery location can not be hasty.
Utility model content
The purpose of this utility model is to provide a kind of new unmanned plane battery compartment, to solve to propose in above-mentioned background technology The problem of.
To achieve the above object, the utility model provides following technical scheme:The utility model discloses a kind of new nothing Man-machine battery compartment, including lower central plate, fixed bottom plate, side shield, front apron, rear end cap, support column, end cap hinge, quick insert Pin.The lower central plate is provided with Quick bolt hole, is cooperated with Quick bolt, and battery is locked in battery compartment, described solid Determine bottom plate with lower central plate to be connected, provided with 5 support columns between it, lower central plate and fixed bottom plate be bolted respectively, The side shield is surrounded by joinery and its construction, is connected respectively with lower central plate, front apron and fixed bottom plate, the front apron is also set There is joinery and its construction, be connected respectively with lower central plate, side shield, fixed bottom plate, the rear end cap is provided with Quick bolt, passes through Bolt is connected with each other, and the end cap hinge connects rear end cap and fixed bottom plate respectively, realizes the hinge of fixed bottom plate and rear end cap Connection.
It is used as further program of the utility model:The lower central plate is coordinated by pin hole and Quick bolt.
It is used as further program of the utility model:It is described to state fixed bottom plate and be fastened on by support column on lower central plate.
It is used as further program of the utility model:The side shield is connected with each other with front apron by joinery and its construction.
It is used as further program of the utility model:The side shield, rear end cap are provided with radiating hole slot.
It is used as further program of the utility model:The rear end cap is movable part, is closed with fixed bottom plate by end cap Page is in hinge connection.
It is used as further program of the utility model:The lower central plate of support column connection and fixed bottom plate, strengthen fixing The installation of bottom plate.
It is used as further program of the utility model:The Quick bolt realizes the quick closedown and unlatching of hatchcover.
Compared with prior art, the beneficial effects of the utility model are:One, the utility model is simple and reasonable for structure, realizes Convenient dismounting, on the premise of not possessing any professional skill and instrument, can realize Fast Installation and the dismounting of battery, improve The service efficiency of unmanned plane.Two, the utility model battery uses underlying structure, for SUAV, appropriate reduction Center of gravity is conducive to weakening its probability tumbled, and improves flight stability.Three, it is contemplated that deadly condition distribution life, when complete machine occurs During major accident, due to battery compartment " full-enclosed " structure and support column it is structure-reinforced, greatly avoid battery in great thing Therefore when by major injury so as to triggering peril.
Brief description of the drawings
Fig. 1 is utility model overall structure diagram.
Fig. 2 is battery compartment partial detailed structural representation.
In figure:Central plate under 1-, 2- rear end caps, 3- Quick bolts, 4- dormant bolts, 5- stop nuts, 6- end caps hinge, 7- fix bottom plate, 8- cylinder head bolts, 9- side shields, 10- Quick bolts support base, 11- helical springs, 12- buckles button, 13- latches buckle, 14- cylinders back-up ring, 15- latch posts, 16- Quick bolts rear end cap, 17- volute springs, 18- split washers, 19- support columns, 20- front aprons.
Embodiment
Below in conjunction with the accompanying drawing in this implementation new embodiment, the technical scheme in the utility model embodiment is carried out It is clear, it is fully described by, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belongs to the scope of the utility model protection.
Refer in Fig. 1, Fig. 2, the utility model embodiment, a kind of new unmanned plane battery compartment, fixed bottom plate 7 passes through circle Stud bolt 8 is connected with support column 19 and lower central plate 1, installs each by mortise-tenon joint between fixed bottom plate 7 and lower central plate 1 Wall, wherein flight direction of advance install front apron 20, and side shield 9 is installed in both sides, and rear end cap 1 is by end cap hinge 6 with fixing The hinge connection of bottom plate 7, end cap hinge 6 is reliably fixed on fixed bottom plate 7 by dormant bolt 4 and stop nut 5 and rear end cap 2 connects Place is met, the top of rear end cap 2 is provided with Quick bolt 3 by dormant bolt 4 and stop nut 5, can be by pin when rear end cap 2 is closed In the lower central plate corresponding jack of the insertion of inserting column 14.The internal helicoid spring 11 of Quick bolt 3 is installed on split washer 18 and support base Between 10, when the upward central plate pin hole motion of latch post 15, helical spring is compressed, and latch buckle 13 is in volute spring 17 Moved under active force to the direction of buckle button 12, while into the buckle ladder of latch post 15 that latch post 15 is locked, realizing The locking functions of Quick bolt 3;When pressing buckle button 12, latch buckle 13 departs from the buckle ladder of latch post 15, realizes The open function of Quick bolt.
The utility model is simple in construction, novelty.By appropriate structure design, the convenient dismounting of battery is accomplished, has used During without using professional tool, relatively low to user's technical requirements, practicality is stronger, on the whole using " full-enclosed " structure Certain physical damnification is caused during reduction accident to battery, body is reduced using the underlying arrangement of battery and tumbled possibility, is carried The high stability and security of complete machine flight.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned example embodiment, and In the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped Containing an independent technical scheme, this narrating mode of specification is only that for clarity, those skilled in the art should Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art It may be appreciated other embodiment.

Claims (9)

1. a kind of new unmanned plane battery compartment, including lower central plate, fixed bottom plate, side shield, front apron, rear end cap, support column, End cap hinge, Quick bolt, it is characterised in that the lower central plate is provided with Quick bolt hole, cooperate with Quick bolt, will Battery is locked in battery compartment, and the fixed bottom plate is connected with lower central plate, provided with 5 support columns between it, passes through spiral shell respectively Tether and connect lower central plate and fixed bottom plate, the side shield is surrounded by joinery and its construction, respectively with lower central plate, front apron and solid Determine bottom plate to be connected, the front apron is also provided with joinery and its construction, be connected respectively with lower central plate, side shield, fixed bottom plate, it is described Rear end cap is provided with Quick bolt, is inter-connected via a bolt joint, and the end cap hinge connects rear end cap and fixed bottom plate respectively, real Now fix the hinge connection of bottom plate and rear end cap.
2. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The lower central plate is provided with quick Pin hole.
3. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The fixed bottom plate is provided with 5 Support column mounting hole and 4 end cap hinge mounting holes.
4. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The side shield, front apron are equal There is joinery and its construction, be connected with upper central plate, fixed bottom plate, and also connect each other locked.
5. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The side shield, rear end cap are equal It is provided with radiating hole slot.
6. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The rear end cap bottom is provided with 4 Individual end cap hinge mounting hole, top is provided with 4 each Quick bolt mounting holes and trapezoidal logical wire casing.
7. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The support column passes through bolt The lower central plate of connection and fixed bottom plate.
8. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The end cap hinge passes through spiral shell Rear end cap is carried out hinge connection by bolt with fixed bottom plate.
9. a kind of new unmanned plane battery compartment according to claim 1, it is characterised in that:The Quick bolt passes through spiral shell Bolt is attached to rear end cap, and cooperate with upper central plate pin hole battery compartment is closed it is locked.
CN201621155934.3U 2016-10-31 2016-10-31 A kind of new unmanned plane battery compartment Expired - Fee Related CN206374991U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621155934.3U CN206374991U (en) 2016-10-31 2016-10-31 A kind of new unmanned plane battery compartment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621155934.3U CN206374991U (en) 2016-10-31 2016-10-31 A kind of new unmanned plane battery compartment

Publications (1)

Publication Number Publication Date
CN206374991U true CN206374991U (en) 2017-08-04

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201621155934.3U Expired - Fee Related CN206374991U (en) 2016-10-31 2016-10-31 A kind of new unmanned plane battery compartment

Country Status (1)

Country Link
CN (1) CN206374991U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109407684A (en) * 2017-08-18 2019-03-01 昊翔电能运动科技(昆山)有限公司 Rotor wing unmanned aerial vehicle attitude control method and system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109407684A (en) * 2017-08-18 2019-03-01 昊翔电能运动科技(昆山)有限公司 Rotor wing unmanned aerial vehicle attitude control method and system
CN109407684B (en) * 2017-08-18 2022-08-19 昊翔电能运动科技(昆山)有限公司 Rotor unmanned aerial vehicle attitude control method and system

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170804

Termination date: 20171031