CN205854472U - A kind of Telescopic adjustable aircraft - Google Patents
A kind of Telescopic adjustable aircraft Download PDFInfo
- Publication number
- CN205854472U CN205854472U CN201620725891.1U CN201620725891U CN205854472U CN 205854472 U CN205854472 U CN 205854472U CN 201620725891 U CN201620725891 U CN 201620725891U CN 205854472 U CN205854472 U CN 205854472U
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- CN
- China
- Prior art keywords
- aircraft
- battery
- basket
- expansion link
- devices room
- Prior art date
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Abstract
The utility model discloses a kind of Telescopic adjustable aircraft, place basket, aircraft devices room, support tube, expansion link, pillar and base including battery；Described battery is placed basket and is arranged on the surface of aircraft devices room；Described battery is placed basket and is provided with battery protective cover and snap close；Described battery protective cover is arranged on battery and places the left upper portion edge of basket；Described snap close is arranged on battery protective cover and places at basket right contact with battery, and snap close can press locking design；Described aircraft devices room is arranged on the surface of three pillars；Described aircraft devices room is provided with hinge, arc covers, chip pad and fixing projection；Base is used for increasing contact area, and make that aircraft lands is more steady；This utility model Telescopic adjustable aircraft has simple in construction, and landing steadiness is more preferable；The volume size of aircraft can be regulated；Can support that dress stores up the advantages such as jumbo battery designs.
Description
Technical field
This utility model relates to a kind of aircraft, specifically a kind of Telescopic adjustable aircraft.
Background technology
At present, on market, the design structure of seen aircraft is all to use fixed design, it is impossible to enough support that user opens up
Exhibition Amending design, it is impossible to enough change the model of motor and the volume size design of whole aircraft；And land at aircraft
Time its bottom the whole fuselage weight of support that can not consolidate of bracing frame, and the stationarity of landing is not enough；It addition, can not
Installing jumbo accumulator, corresponding flight path is shorter waits deficiency；It would therefore be desirable to a kind of Telescopic adjustable flight
Device.
Utility model content
The purpose of this utility model is to provide a kind of Telescopic adjustable aircraft, to solve to carry in above-mentioned background technology
The problem gone out.
For achieving the above object, the following technical scheme of this utility model offer:
A kind of Telescopic adjustable aircraft, places basket, aircraft devices room, support tube, expansion link, pillar including battery
And base；Described battery is placed basket and is arranged on the surface of aircraft devices room；Described battery is placed basket and is provided with battery protection
Lid and snap close；Described battery protective cover is arranged on battery and places the left upper portion edge of basket；Described snap close is arranged on battery and protects
Protecting cover is placed at basket right contact with battery, and snap close can press locking design；Described aircraft devices room is arranged on three
On the surface of pillar, and the seamless top end face being fixed on pillar of aircraft devices room level；Described aircraft devices room is arranged
There are hinge, arc covers, chip pad and fixing projection；It is left with arc covers contact position that described hinge is arranged on aircraft devices room
Side, and hinge is separately fixed on aircraft devices room and arc covers；Described arc covers is arranged in front, aircraft devices room
Position, centre；Described arc covers is provided with and draws handle；Described draw the middle position, right side being arranged on arc covers, and draw the most vertical
It is weldingly fixed on arc covers；Described chip pad is arranged in the internal backplane of aircraft devices room, and chip pad level
Design and be fixedly welded on base plate；Described fixing projection is arranged on the left and right sides in chip pad；Described fixing projection is arranged
There is flying vehicles control chip；Described flying vehicles control chip level is fixed on fixing flange and uses screw to reinforce；Described
Support cylinder is arranged on middle position on the periphery of aircraft devices room；Described support tube is provided with steady pin；Described steady pin sets
Put and design on the middle position, outside at support tube, and the vertical same periphery of three steady pins；Described expansion link is arranged on support
In cylinder；Described expansion link is provided with circular hole and motor；Described circular hole is arranged on expansion link；Described motor is arranged on expansion link
At outboard end upper surface, and motor is vertically weldingly fixed on expansion link；Described motor is provided with flabellum protective frame and flabellum；
Described flabellum protective frame is arranged on the middle part periphery of motor；Described flabellum is arranged on the upper end surface of motor, and flabellum energy
Enough freely rotatable designs；Described pillar is arranged on the bottom outer wall of aircraft devices room, and three pillars vertical vertical flight device
Canyon seamless welding Fixed Design；Described pillar is provided with support bar；Described support bar is arranged on pillar, and support bar inclines
Inclined weld is connected on pillar, and the lower end of support bar is welded on base；Described base is arranged on the underface of pillar.
As further program of the utility model: described battery is placed basket and is arranged on the surface of aircraft devices room,
And battery places basket level design fixing with aircraft devices room seamless welding, edge and the aircraft devices of basket placed by battery
The concordant design of outside periphery.
As further program of the utility model: described battery protective cover is arranged on battery and places the left upper portion limit of basket
At edge, and battery protective cover 120 degree of rotations can design and use iron wire to be fixed on battery placement basket.
As further program of the utility model: described arc covers is arranged on middle position, front, aircraft devices room,
And arc covers is fixed on aircraft devices room by hinge, arc covers can 120 degree of rotation designs.
As further program of the utility model: described support tube is arranged on the periphery of aircraft devices room central authorities
Position, and three support tube horizontal vertical are fixed on aircraft devices room, the external diameter of support tube is less than outside aircraft devices room
Side height.
As further program of the utility model: described expansion link is arranged in support tube, and expansion link can prop up
Twitch back and forth and be fixed on support tube by steady pin in support cylinder.
As further program of the utility model: described circular hole is arranged on expansion link, and circular hole is evenly distributed on and stretches
On contracting bar and being vertically perforated through expansion link design, the diameter of circular hole is less than the diameter of expansion link, more than the lower diameter of steady pin.
As further program of the utility model: described flabellum protective frame is arranged on the middle part periphery of motor, and
The top circular design of flabellum protective frame and diameter are more than flabellum rotating diameter.
As this utility model further scheme: described base is arranged on the underface of pillar, and the diameter of base
More than three times of strut diameter designs.
Compared with prior art, the beneficial effects of the utility model are:
Battery of the present utility model is placed basket and is used for installing placement accumulator and supplying electrical power to aircraft using；Battery is protected
Protecting cover for placing the accumulator in basket to fixing locking by battery；The arc covers of aircraft devices room is used for facilitating aircraft control
Coremaking sheet is installed；Drawing for arc covers being closed and opening use on arc covers；Support tube is flexible for installing and regulating
Bar uses, and expansion link is fixed on support tube by the circular hole being perforated through on expansion link with steady pin；Motor on expansion link is used
In driving flabellum to rotate, thus whole aircraft will be promoted, make aircraft free flight；Flabellum fender bracket is for protecting inside
Flabellum uses；Pillar is for when aircraft lands, and the firm weight supporting whole aircraft and stable landing use；Support bar
Design for strengthening the structure support strength of pillar；Base is used for increasing contact area, and make that aircraft lands is more steady；This
Utility model Telescopic adjustable aircraft has simple in construction, and landing steadiness is more preferable；The volume that can regulate aircraft is big
Little；Can support that dress stores up the advantages such as jumbo battery designs.
Accompanying drawing explanation
Fig. 1 is the structural representation of Telescopic adjustable aircraft.
Fig. 2 is the structural representation of Telescopic adjustable aircraft chips base.
Fig. 3 is the structural representation of support bar in Telescopic adjustable aircraft.
In figure: 1-flabellum protective frame, 2-flabellum, 3-motor, 4-expansion link, 5-steady pin, 6-support tube, 7-hinge, 8-
Arc covers, 9-draws handle, 10-pillar, 11-base, 12-support bar, 13-circular hole, and 14-battery places basket, 15-snap close, 16-battery
Protection cap, 17-flying vehicles control chip, 18-fixes projection, 19-aircraft devices room, 20-chip pad.
Detailed description of the invention
Below in conjunction with detailed description of the invention, the technical scheme of this patent is described in more detail.
Refer to Fig. 1-3, a kind of Telescopic adjustable aircraft, place basket 14, aircraft devices room 19 including battery, prop up
Support cylinder 6, expansion link 4, pillar 10 and base 11；Described battery is placed basket 14 and is arranged on the surface of aircraft devices room 19, and
Battery is placed basket 14 level design and fixes with aircraft devices room 19 seamless welding, and edge and the aircraft of basket 14 placed by battery
The concordant design in canyon 19 outer circumference face；Described battery is placed basket 14 and is provided with battery protective cover 16 and snap close 15；Described electricity
Pond protection cap 16 is arranged on battery and places the left upper portion edge of basket 14, and battery protective cover 16 can 120 degree of rotation designs
And use iron wire to be fixed on battery placement basket 14；Described snap close 15 is arranged on battery protective cover 16 and places on the right side of basket 14 with battery
Contact position, and snap close 15 can press locking design；Described aircraft devices room 19 is arranged on the surface of three pillars 10, and
On aircraft devices room 19 level the is seamless top end face being fixed on pillar 10；Described aircraft devices room 19 is provided with hinge 7, arc
Shape lid 8, chip pad 20 and fixing projection 18；It is left with arc covers 8 contact position that described hinge 7 is arranged on aircraft devices room 19
Side, and hinge 7 is separately fixed on aircraft devices room 19 and arc covers 8；Described arc covers 8 is arranged on aircraft devices room 19
Middle position, front, and arc covers 8 is fixed on aircraft devices room 19 by hinge 7, arc covers 8 can set in 120 degree of rotations
Meter；Described arc covers 8 is provided with and draws 9；The described middle position, right side being arranged on arc covers 89 of drawing, and draw and vertically hang down 9
Directly it is weldingly fixed on arc covers 8；Described chip pad 20 is arranged in the internal backplane of aircraft devices room 19, and at the bottom of chip
Seat 20 level design are also fixedly welded on base plate；Described fixing projection 18 is arranged on the left and right sides in chip pad 20；Described
Fixing projection 18 is provided with flying vehicles control chip 17；Described flying vehicles control chip 17 is horizontally fixed on fixing flange 18 also
Employing screw is reinforced；Described support tube 6 is arranged on middle position on the periphery of aircraft devices room 19, and three support tube 6 water
Putting down and be vertically fixed on aircraft devices room 19, the external diameter of support tube 6 is less than the outside height of aircraft devices room 19；Described
Support cylinder 6 is provided with steady pin 5；Described steady pin 5 is arranged on the middle position, outside of support tube 6, and three steady pins 5 are the most same
Design on periphery；Described expansion link 4 is arranged in support tube 6, and expansion link 4 can be twitched back and forth in support tube 6 and lead to
Cross steady pin 5 to be fixed on support tube 6；Described expansion link 4 is provided with circular hole 13 and motor 3；Described circular hole 13 is arranged on flexible
On bar 4, and circular hole 13 is evenly distributed on expansion link 4 and is vertically perforated through expansion link 4 and designs, and the diameter of circular hole 13 is less than flexible
The diameter of bar 4, more than the lower diameter of steady pin 5；Described motor 3 is arranged at the outboard end upper surface of expansion link 4, and electricity
Machine 3 is vertically weldingly fixed on expansion link 4；Described motor 3 is provided with flabellum protective frame 1 and flabellum 2；Described flabellum protective frame 1
It is arranged on the middle part periphery of motor 3, and the top circular design of flabellum protective frame 1 and diameter rotate more than flabellum 2
Diameter；Described flabellum 2 is arranged on the upper end surface of motor 3, and flabellum 2 can freely rotatable design；Described pillar 10 is arranged on
On the bottom outer wall of aircraft devices room 19, and three pillars 10 vertical vertical flight device canyon 19 seamless welding Fixed Design；
Described pillar 10 is provided with support bar 12；Described support bar 12 is arranged on pillar 10, and support bar 12 oblique weld is at pillar
On 10, the lower end of support bar 12 is welded on the pedestal 11；Described base 11 is arranged on the underface of pillar 10, and base 11 is straight
Footpath is more than three times of pillar 10 diameter design；Battery is placed basket 14 and is used for installing placement accumulator and supplying electrical power to aircraft making
With；Battery protective cover 16 for placing the accumulator in basket 14 to fixing locking by battery；The arc covers 8 of aircraft devices room 19
For facilitating flying vehicles control chip 17 to install；Drawing 9 for arc covers 8 being closed and opening use on arc covers 8；Support
Cylinder 6 uses with adjustable telescopic rod 4 for installing, and expansion link 4 is fixed by the circular hole 13 being perforated through on expansion link 4 with steady pin 5
On support tube 6；Motor 3 on expansion link 4 is used for driving flabellum 2 to rotate, thus will promote whole aircraft, makes aircraft certainly
By flying；Flabellum fender bracket 1 uses for protecting the flabellum 2 of inside；Pillar 10 is for when aircraft lands, and firm support is whole
The weight of individual aircraft and stable landing use；Support bar 12 is for strengthening the structure support strength design of pillar 10；Base 11
For increasing contact area, make that aircraft lands is more steady.
Above the better embodiment of this patent is explained in detail, but this patent is not limited to above-mentioned embodiment party
Formula, in the ken that one skilled in the relevant art is possessed, it is also possible on the premise of without departing from this patent objective
Make a variety of changes.
Claims (9)
1. a Telescopic adjustable aircraft, including battery place basket, aircraft devices room, support tube, expansion link, pillar and
Base；It is characterized in that, described battery is placed basket and is arranged on the surface of aircraft devices room；Described battery is placed basket and is provided with
Battery protective cover and snap close；Described battery protective cover is arranged on battery and places the left upper portion edge of basket；Described snap close is arranged
Place at basket right contact with battery at battery protective cover, and snap close can press locking design；Described aircraft devices room sets
Put on the surface at three pillars, and the seamless top end face being fixed on pillar of aircraft devices room level；Described aircraft sets
Standby room is provided with hinge, arc covers, chip pad and fixing projection；Described hinge is arranged on aircraft devices room and connects with arc covers
On the left of synapsis, and hinge is separately fixed on aircraft devices room and arc covers；Described arc covers is arranged on aircraft devices room
Middle position, front；Described arc covers is provided with and draws handle；Described draw the middle position, right side being arranged on arc covers, and draw perpendicular
Straight vertical welding is fixed on arc covers；Described chip pad is arranged in the internal backplane of aircraft devices room, and at the bottom of chip
Seat level design is also fixedly welded on base plate；Described fixing projection is arranged on the left and right sides in chip pad；Described fixing convex
Block is provided with flying vehicles control chip；Described flying vehicles control chip level is fixed on fixing flange and uses screw to reinforce；
Described support tube is arranged on middle position on the periphery of aircraft devices room；Described support tube is provided with steady pin；Described solid
Rationed marketing is arranged on the middle position, outside of support tube, and the vertical same periphery of three steady pins design；Described expansion link is arranged
In support tube；Described expansion link is provided with circular hole and motor；Described circular hole is arranged on expansion link；Described motor is arranged on to be stretched
At the outboard end upper surface of contracting bar, and motor is vertically weldingly fixed on expansion link；Described motor is provided with flabellum protective frame
And flabellum；Described flabellum protective frame is arranged on the middle part periphery of motor；Described flabellum is arranged on the upper end surface of motor, and
Flabellum can freely rotatable design；Described pillar is arranged on the bottom outer wall of aircraft devices room, and three pillars are the most vertical
Aircraft devices room seamless welding Fixed Design；Described pillar is provided with support bar；Described support bar is arranged on pillar, and
Strut oblique weld is on pillar, and the lower end of support bar is welded on base；Described base is arranged on the underface of pillar.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described battery placement basket is arranged on and flies
The surface of row device canyon, and battery places basket level design fixing with aircraft devices room seamless welding, battery is placed
The edge of basket and the concordant design of periphery of aircraft devices outside.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described battery protective cover is arranged on electricity
The left upper portion edge of basket is placed in pond, and battery protective cover can 120 degree rotate and design and use iron wire to be fixed on battery to put
Put on basket.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described arc covers is arranged on aircraft
Middle position, canyon front, and arc covers is fixed on aircraft devices room by hinge, arc covers can set in 120 degree of rotations
Meter.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described support tube is arranged on aircraft
Middle position on the periphery of canyon, and three support tube horizontal vertical are fixed on aircraft devices room, the external diameter of support tube
Outside height less than aircraft devices room.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described expansion link is arranged on support tube
In, and expansion link can be twitched back and forth in support tube and be fixed on support tube by steady pin.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described circular hole is arranged on expansion link
On, and circular hole is evenly distributed on expansion link and is vertically perforated through expansion link design, the diameter of circular hole less than the diameter of expansion link,
Lower diameter more than steady pin.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described flabellum protective frame is arranged on electricity
On the middle part periphery of machine, and the top circular design of flabellum protective frame and diameter are more than flabellum rotating diameter.
Telescopic adjustable aircraft the most according to claim 1, it is characterised in that described base is just being arranged on pillar
Lower section, and the diameter of base is more than three times of strut diameter designs.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725891.1U CN205854472U (en) | 2016-07-11 | 2016-07-11 | A kind of Telescopic adjustable aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725891.1U CN205854472U (en) | 2016-07-11 | 2016-07-11 | A kind of Telescopic adjustable aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205854472U true CN205854472U (en) | 2017-01-04 |
Family
ID=57646034
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620725891.1U Expired - Fee Related CN205854472U (en) | 2016-07-11 | 2016-07-11 | A kind of Telescopic adjustable aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205854472U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106927042A (en) * | 2017-03-29 | 2017-07-07 | 深圳市雷凌广通技术研发有限公司 | A kind of unmanned plane of changeable form |
-
2016
- 2016-07-11 CN CN201620725891.1U patent/CN205854472U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106927042A (en) * | 2017-03-29 | 2017-07-07 | 深圳市雷凌广通技术研发有限公司 | A kind of unmanned plane of changeable form |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170104 Termination date: 20170711 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |