CN107200117A - A kind of aircraft that easing gear is filled with recession formula - Google Patents
A kind of aircraft that easing gear is filled with recession formula Download PDFInfo
- Publication number
- CN107200117A CN107200117A CN201710237705.9A CN201710237705A CN107200117A CN 107200117 A CN107200117 A CN 107200117A CN 201710237705 A CN201710237705 A CN 201710237705A CN 107200117 A CN107200117 A CN 107200117A
- Authority
- CN
- China
- Prior art keywords
- easing gear
- recession
- fuselage
- aircraft
- filled
- 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.)
- Pending
Links
- 210000000078 claw Anatomy 0.000 claims abstract description 8
- 238000010586 diagram Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The present invention relates to dress easing gear, more particularly to a kind of aircraft that easing gear is filled with recession formula, the body upper is provided with below lid, fuselage provided with dress easing gear, and the dress easing gear is used in conjunction with each other by pressing structure with fuselage.The pressing structure, which includes being provided with below contiguous block, contiguous block below upper cover plate, upper cover plate, is provided with claw, pressing structure is additionally provided with lower supporting rod, the lower supporting rod when in use stretched into claw by one end, and the upper cover plate is fixed on fuselage, and the other end of the lower supporting rod is fixed on dress easing gear.It is used for handling goods present invention employs recession formula dress easing gear, recession formula handler is used in conjunction with each other by slide-bar with track, it is easy to pull, pressing structure is provided with dress easing gear, the unlatching of convenient dress easing gear fills easing gear with closure and in aircraft flight and do not fallen out；Body upper is provided with lid, is conveniently replaceable battery；Fuselage uses integral structure, rain-proof.
Description
Technical field
The present invention relates to the handler of aircraft, more particularly to a kind of flight that easing gear is filled with recession formula
Device.Background technology
At present, toward truck or baby plane and other mechanically, all manually load and unload, inefficiency and waste labor
Power, also or is loading goods using conveyer belt or other devices, but in unmanned plane field using not
It is easily even to say that some troubles may be produced.
The content of the invention
The shortcomings of present invention is for the inconvenience of handling goods in the prior art and lost labor carries recession there is provided one kind
Formula fills the aircraft of easing gear.
In order to solve the above-mentioned technical problem, the present invention is addressed by following technical proposals：
A kind of aircraft that easing gear is filled with recession formula, including fuselage, the body upper are provided with below lid, fuselage and set
There is dress easing gear, the dress easing gear is used in conjunction with each other by pressing structure with fuselage.
Preferably, the pressing structure includes being provided with below upper cover plate, upper cover plate below contiguous block, contiguous block provided with card
Pawl, pressing structure is additionally provided with lower supporting rod, and the lower supporting rod when in use stretch into claw by one end, and the upper cover plate is fixed on fuselage
On, the other end of the lower supporting rod is fixed on dress easing gear.
Preferably, the lower supporting rod upper end is provided with fastener.
Preferably, the dress easing gear includes support and housing, the support is provided with slide-bar, the housing and set
There is track, the slide-bar is used in conjunction with each other with track.
Preferably, the housing includes bottom plate, two side and rear wall, the bottom plate, two side and rear wall are integrated
Change on the upside of structure, the bottom plate with being respectively equipped with track on the inside of two side.
Preferably, the track is slide rail.
Preferably, the slide-bar is provided with sliding block, sliding block size is less than inner track radius size.
Preferably, being provided with battery in the fuselage, the lid is arranged on the fuselage directly over battery.
The present invention is as a result of above technical scheme, with significant technique effect：
It is used for handling goods present invention employs recession formula dress easing gear, recession formula handler is mutual with track by slide-bar
Use cooperatively, be easy to pull, be provided with pressing structure on dress easing gear, the unlatching of convenient dress easing gear with closure and
Easing gear is filled in aircraft flight not fall out；Body upper is provided with lid, is conveniently replaceable battery；Fuselage uses integral type knot
Structure, rain-proof.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing skill
The accompanying drawing used required in art description is briefly described, it should be apparent that, drawings in the following description are only the present invention
Some embodiments, for those of ordinary skill in the art, without having to pay creative labor, can be with root
Other accompanying drawings are obtained according to these accompanying drawings.
Fig. 1 is overall structure figure of the invention；
Fig. 2 is handling goods schematic device of the invention；
Fig. 3 is partial devices schematic diagram of the invention；
Fig. 4 is pressing structure schematic diagram of the invention.
Label declaration：Fuselage 1, lid 2, dress easing gear 3, pressing structure 4, cover plate 41, contiguous block 42, claw 43, under
Pillar 44, fastener 45, support 31, housing 32, slide-bar 33, track 34, bottom plate 35, side wall 36, rear wall 37, sliding block 38.
Embodiment
With reference to embodiment, the present invention is described in further detail, and following examples are explanation of the invention and this hair
It is bright to be not limited to following examples.
Embodiment 1：
A kind of aircraft that easing gear is filled with recession formula, including fuselage 1, are provided with mutual with fuselage 1 in the surface of fuselage 1
The lid 2 of cooperation, lid 2 can be raised, the lower section of fuselage 1 provided with dress easing gear 3, dress easing gear 3 by pressing structure 4 with
Fuselage 1 is used in conjunction with each other.It is used for handling goods present invention employs recession formula dress easing gear, recession formula handler passes through
Slide-bar is used in conjunction with each other with track, is easy to pull, and pressing structure is provided with dress easing gear, convenient to fill opening for easing gear
Open and close and easing gear is filled in aircraft flight and is not fallen out and be used for present invention employs recession formula dress easing gear
Handling goods, recession formula handler is used in conjunction with each other by slide-bar with track, is easy to pull, is provided with dress easing gear
Pressing structure, the unlatching of convenient dress easing gear fills easing gear with closure and in aircraft flight and not fallen out.
Embodiment 2：
A kind of aircraft that easing gear is filled with recession formula, including fuselage 1, are provided with mutual with fuselage 1 in the surface of fuselage 1
The lid 2 of cooperation, lid 2 can be raised, the lower section of fuselage 1 provided with dress easing gear 3, dress easing gear 3 by pressing structure 4 with
Fuselage 1 is used in conjunction with each other.
Pressing structure 4 includes upper cover plate 41, and the lower section of upper cover plate 41 is provided with contiguous block 42, and the lower section of contiguous block 42 is provided with claw
43, pressing structure 4 is additionally provided with lower supporting rod 44, and the lower supporting rod 44 when in use stretch into claw 43 by one end, the upper cover plate 41
Fix on the fuselage 1, the other end of lower supporting rod 44 is fixed on dress easing gear 3, and the upper end of lower supporting rod 44 is provided with fastener 45.
The structure of dress easing gear 3 is constituted including support 31 with housing 32, and in embodiment, described support 31 is actually
Framework, this framework does supporting role, including former and later two frameworks, and former and later two frameworks pass through the pillar of left and right two and bottom two
Root pillar is fixed, on the outside of two pillars in left and right be provided with slide-bar 33, the pillar of bottom two be provided with slide-bar 33, housing 32
Including bottom plate 35, two side 36 and rear wall 37, bottom plate 35, two side 36 and rear wall 37 are integrated, the upside of bottom plate 35
Track 34 is respectively equipped with the inner side of two side 36, slide-bar 33 is provided with sliding block 38, and the size of sliding block 38 is less than track 34
Internal diameter size, sliding block 38 enters line slip in track 34.
In this embodiment, track 34 is slide rail.
Battery is provided with fuselage 1, battery is that lid 2 is arranged on the machine directly over battery in order to be used to aircraft continuation of the journey
On body 1, lid 2 can be raised, and battery is taken out, and be convenient for changing battery or charged the battery.
Furthermore, it is necessary to explanation, the specific embodiment described in this specification, is named the shape of its parts and components
Title etc. can be different.The equivalent or simple change that all construction, feature and principles according to described in inventional idea of the present invention are done, is wrapped
Include in the protection domain of patent of the present invention.Those skilled in the art can be to described specific implementation
Example is made various modifications or supplement or substituted using similar mode, structure without departing from the present invention or surmounts this
Scope as defined in the claims, all should belong to protection scope of the present invention.
Claims (8)
1. a kind of aircraft that easing gear is filled with recession formula, including fuselage（1）, it is characterised in that：The fuselage（1）Top
Provided with lid（2）, fuselage（1）Lower section is provided with dress easing gear（3）, the dress easing gear（3）Pass through pressing structure（4）With machine
Body（1）It is used in conjunction with each other.
2. a kind of aircraft that easing gear is filled with recession formula according to claim 1, it is characterised in that：The pressing
Structure（4）Including upper cover plate（41）, upper cover plate（41）Lower section is provided with contiguous block（42）, contiguous block（42）Lower section is provided with claw
（43）, pressing structure（4）It is additionally provided with lower supporting rod（44）, the lower supporting rod（44）Claw is stretched into one end when in use（43）In, institute
State upper cover plate（41）It is fixed on fuselage（1）On, the lower supporting rod（44）The other end be fixed on dress easing gear（3）On.
3. a kind of aircraft that easing gear is filled with recession formula according to claim 2, it is characterised in that：The lower branch
Post（44）Upper end is provided with fastener（45）.
4. a kind of aircraft that easing gear is filled with recession formula according to claim 1 or 2, it is characterised in that：It is described
Fill easing gear（3）Including support（31）With housing（32）, the support（31）It is provided with slide-bar（33）, the housing（32）On
Provided with track（34）, the slide-bar（33）With track（34）It is used in conjunction with each other.
5. a kind of aircraft that easing gear is filled with recession formula according to claim 2, it is characterised in that：The housing
（32）Including bottom plate（35）, two side（36）And rear wall（37）, the bottom plate（35）, two side（36）With rear wall（37）For one
Body structure, the bottom plate（35）Upside and two side（36）Inner side is respectively equipped with track（34）.
6. a kind of aircraft that easing gear is filled with recession formula according to claim 4, it is characterised in that：The track
（34）For slide rail.
7. a kind of aircraft that easing gear is filled with recession formula according to claim 3, it is characterised in that：The slide-bar
（33）It is provided with sliding block（38）, sliding block（38）Size is less than track（34）Internal diameter size.
8. a kind of aircraft that easing gear is filled with recession formula according to claim 1, it is characterised in that：The fuselage
（1）It is interior to be provided with battery, the lid（2）It is arranged on the fuselage directly over battery（1）On.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710237705.9A CN107200117A (en) | 2017-04-12 | 2017-04-12 | A kind of aircraft that easing gear is filled with recession formula |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710237705.9A CN107200117A (en) | 2017-04-12 | 2017-04-12 | A kind of aircraft that easing gear is filled with recession formula |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107200117A true CN107200117A (en) | 2017-09-26 |
Family
ID=59905595
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710237705.9A Pending CN107200117A (en) | 2017-04-12 | 2017-04-12 | A kind of aircraft that easing gear is filled with recession formula |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107200117A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107933926A (en) * | 2017-11-23 | 2018-04-20 | 顺丰科技有限公司 | A kind of unmanned plane clamping device, unmanned plane cargo hold and unmanned plane |
| CN108520376A (en) * | 2018-04-08 | 2018-09-11 | 中博宇图信息科技有限公司 | A kind of Intelligent logistics delivery system and delivering method based on unmanned plane |
| CN111806694A (en) * | 2020-07-24 | 2020-10-23 | 周海娅 | Eight rotor type unmanned aerial vehicle for logistics transportation |
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| US20030146636A1 (en) * | 2002-02-01 | 2003-08-07 | Keller Cyril N. | Pull-out load platform for truck cargo beds |
| CN200965211Y (en) * | 2006-11-15 | 2007-10-24 | 戴雪珍 | Lamp cover pressed switch type seating lamp |
| CN101068714A (en) * | 2004-12-09 | 2007-11-07 | 空中客车法国公司 | Super-transporter aircraft |
| CN103818544A (en) * | 2014-01-24 | 2014-05-28 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body and manufacturing method thereof |
| CN203781159U (en) * | 2014-04-04 | 2014-08-20 | 无锡普智联科高新技术有限公司 | Drawer-type goods shelf suitable for automatically loading and unloading goods |
| CN104442504A (en) * | 2014-12-30 | 2015-03-25 | 左常亮 | Self-loading-unloading truck carriage |
| CN205131674U (en) * | 2015-11-10 | 2016-04-06 | 湖南云顶智能科技有限公司 | Small -size all -wing aircraft overall arrangement unmanned aerial vehicle |
| CN105923163A (en) * | 2016-06-01 | 2016-09-07 | 北京小米移动软件有限公司 | Transportation shelf and unmanned aerial vehicle |
| CN106081163A (en) * | 2016-08-23 | 2016-11-09 | 成都翼高九天科技有限公司 | A kind of unmanned plane changes power source system automatically |
| CN205707289U (en) * | 2016-06-02 | 2016-11-23 | 比亚迪股份有限公司 | Unmanned plane battery hatch structure and unmanned plane |
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2017
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Patent Citations (12)
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|---|---|---|---|---|
| JPH0659618U (en) * | 1993-02-04 | 1994-08-19 | ポップリベット・ファスナー株式会社 | Article mounting structure |
| CN1257025A (en) * | 1998-11-09 | 2000-06-21 | 西科尔斯基飞机公司 | Goods-carring box assembly for cargo of helicopter |
| US20030146636A1 (en) * | 2002-02-01 | 2003-08-07 | Keller Cyril N. | Pull-out load platform for truck cargo beds |
| CN101068714A (en) * | 2004-12-09 | 2007-11-07 | 空中客车法国公司 | Super-transporter aircraft |
| CN200965211Y (en) * | 2006-11-15 | 2007-10-24 | 戴雪珍 | Lamp cover pressed switch type seating lamp |
| CN103818544A (en) * | 2014-01-24 | 2014-05-28 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body and manufacturing method thereof |
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| CN205131674U (en) * | 2015-11-10 | 2016-04-06 | 湖南云顶智能科技有限公司 | Small -size all -wing aircraft overall arrangement unmanned aerial vehicle |
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| CN205707289U (en) * | 2016-06-02 | 2016-11-23 | 比亚迪股份有限公司 | Unmanned plane battery hatch structure and unmanned plane |
| CN106081163A (en) * | 2016-08-23 | 2016-11-09 | 成都翼高九天科技有限公司 | A kind of unmanned plane changes power source system automatically |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107933926A (en) * | 2017-11-23 | 2018-04-20 | 顺丰科技有限公司 | A kind of unmanned plane clamping device, unmanned plane cargo hold and unmanned plane |
| CN108520376A (en) * | 2018-04-08 | 2018-09-11 | 中博宇图信息科技有限公司 | A kind of Intelligent logistics delivery system and delivering method based on unmanned plane |
| CN108520376B (en) * | 2018-04-08 | 2022-12-23 | 广东诚进科技股份有限公司 | Intelligent logistics delivery system and delivery method based on unmanned aerial vehicle |
| CN111806694A (en) * | 2020-07-24 | 2020-10-23 | 周海娅 | Eight rotor type unmanned aerial vehicle for logistics transportation |
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