CN107010217A - A kind of screen turning device and aircraft - Google Patents
A kind of screen turning device and aircraft Download PDFInfo
- Publication number
- CN107010217A CN107010217A CN201710342371.1A CN201710342371A CN107010217A CN 107010217 A CN107010217 A CN 107010217A CN 201710342371 A CN201710342371 A CN 201710342371A CN 107010217 A CN107010217 A CN 107010217A
- Authority
- CN
- China
- Prior art keywords
- screen
- fixed seat
- turning device
- aircraft
- rotating shaft
- 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.)
- Granted
Links
- 239000007787 solid Substances 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 7
- 238000005516 engineering process Methods 0.000 abstract description 5
- 210000003739 neck Anatomy 0.000 description 9
- 230000008859 change Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 244000144977 poultry Species 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- 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
- B64D47/00—Equipment not otherwise provided for
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Catching Or Destruction (AREA)
- Devices For Indicating Variable Information By Combining Individual Elements (AREA)
Abstract
The invention discloses a kind of screen turning device and aircraft, belong to vehicle technology field.Screen turning device provided by the present invention includes screen fixed seat and renovated, screen fixed seat can be rotated so as in embedded renovate around one end is renovated, the screen turning device is by the way that screen is placed in screen fixed seat, screen fixed seat is around renovating in one end rotates into and renovate, renovating spiral-lock can reach on aircraft skin when needing repairing aircraft or needing the part for taking out aircraft interior, aircraft skin, which need not be dismantled, to come out screen automatic turning, the screen turning device is not only simple in structure, operation is flexible, it is time saving and energy saving, and can prevent from repeatedly dismantling screen influence FPC cablings, be conducive to improving the reliability of FPC cablings, increase the service life of aircraft, improve maintenance efficiency, present invention also offers a kind of aircraft for including above-mentioned screen turning device.
Description
Technical field
The present invention relates to vehicle technology field, more particularly to a kind of screen turning device and apply the screen turning device
Aircraft.
Background technology
Aircraft is used for military field monitoring and information gathering earliest, with the development of science and technology and people's life water
Flat is substantially improved, and the function of aircraft is more and more diversified, and because it has good mobility, takeoff and anding place small
With can more and more widely be applied in other field the advantages of maneuvering flight in a wide range of, such as crop survey, domestic animal
Poultry monitoring, road patrol, search and rescue activity, City fireproof are maked an inspection tour, surveyed and drawn, taking photo by plane, wedding celebration, contest etc..
Because the function of aircraft is more and more, therefore display device is equipped with increasing aircraft to be used to show
The indices of aircraft, such as amount of batteries, status, whether break down and occur which kind of failure etc., yet with
The volume of existing aircraft is generally smaller, is generally embedded in by display device on aircraft, is placed in the parts such as placing battery
Above groove, after display device insertion aircraft, if aircraft interior needs repairing or parts need to change, such as more
Battery etc. is changed, then needs to disassemble display device, not only complex operation, wastes time and energy, aircraft surface is easily damaged, dropped
Low aircraft service life, and display device FPC cabling is easily influenceed on this dismounting display device, FPC reliability is low, from
And have a strong impact on the service life of aircraft.
The content of the invention
It is an object of the present invention to provide a kind of screen turning device, the screen turning device can not only be neatly
Screen and aircraft skin are split, need not be dismantled just when repairing aircraft or needing the part for taking out aircraft interior
Automatically screen can be flipped out, operation is flexible, time saving and energy saving, disassembly and assembly efficiency high, and is conducive to improving FPC cablings
Reliability, increase aircraft service life.
It is another object of the present invention to provide a kind of aircraft, the aircraft includes above-mentioned screen turning device, tool
Have simple in construction, screen is easy to installation and maintenance, time saving and energy saving, the reliability of FPC cablings is high, the advantages of service life is long.
For up to this purpose, the present invention uses following technical scheme：
A kind of screen turning device is provided, includes screen fixed seat and spiral-lock the turning on aircraft skin of fixed mask
Lid, the screen fixed seat can renovate one end rotation so as to be renovated described in embedded interior around described.
Preferably, the screen turning device also includes rotating shaft fixed block, the rotating shaft fixed block is arranged on the screen
Curtain fixed seat and it is described renovate between, described rotating shaft fixed block one end is fixedly connected with described renovate, and the rotating shaft fixed block is another
One end rotates with the screen fixed seat and is connected, the one end of the screen fixed seat away from the rotating shaft fixed block and the flight
Device shell rotates connection.
Preferably, the screen turning device also includes fixed plate, described fixed plate one end and the screen fixed seat
Connection is rotated, the fixed plate other end is fixedly connected with the aircraft skin.
Preferably, described renovate renovates housing and connecting portion including what is be fixedly connected, described renovate is provided with housing
For the opening of display screen, described renovate can be fixedly connected by the connecting portion with the aircraft skin.
Preferably, being provided with grab on the connecting portion, neck, the grab energy are provided with the aircraft skin
Enough it is caught in the neck and is renovated described and the aircraft skin clamping.
Preferably, the screen fixed seat includes fixed seat body, the first otic placode and the second otic placode, first otic placode
Projection is distinguished on the relative two sides of the fixed seat body with second otic placode, and first otic placode is consolidated with the rotating shaft
Determine block and rotate connection, second otic placode is rotated with the fixed plate and is connected.
Preferably, setting the first connecting hole on first otic placode, third ear plate is convexly equipped with the rotating shaft fixed block,
The 3rd connecting hole is provided with the third ear plate, first rotating shaft sequentially passes through the first connecting hole and the 3rd connecting hole by the screen
Curtain fixed seat is rotated with the rotating shaft fixed block and is connected.
The 4th connecting hole is provided with preferably, being provided with second otic placode in the second connecting hole, the fixed plate,
Second rotating shaft sequentially passes through the second connecting hole and the 4th connecting hole and is connected the screen fixed seat with fixed plate rotation.
Preferably, being provided with slot on the aircraft skin, hole clipping is provided with the slot, the fixed plate is remote
One end from the screen fixed seat is convexly equipped with fixture block, and the fixed plate is inserted into the slot, and the fixture block can block
Enter and be fixedly connected with the fixed plate with the aircraft skin in the hole clipping.
A kind of aircraft, includes screen turning device described above.
Beneficial effects of the present invention：
Screen turning device provided by the present invention includes screen fixed seat and renovated, and screen is placed in screen fixed seat,
Spiral-lock is renovated on aircraft skin, screen fixed seat can be rotated so as in embedded renovate around one end is renovated.Compared to existing
Directly screen is fixed on aircraft skin in technology, the present invention is by the way that screen is placed in screen fixed seat, and screen is fixed
Seat around renovating in one end rotates into and renovate, renovate spiral-lock can be reached on aircraft skin when need repairing aircraft or
When needing the part for taking out aircraft interior, it is not necessary to which dismantling aircraft skin automatically can just flip out screen, maintenance
Screen is overturn into rear spiral-lock is renovated in flying machine shell again after finishing, the device is not only simple in structure, operation spirit
It is living, time saving and energy saving, disassembly and assembly efficiency high, and can prevent from repeatedly dismantling screen influence FPC cablings, be conducive to improving FPC
The reliability of cabling, increases the service life of aircraft, improves maintenance efficiency.Aircraft provided by the present invention includes above-mentioned screen
Curtain turning device.
Brief description of the drawings
Fig. 1 is the structural representation of the aircraft provided by the present invention when renovating closure；
Fig. 2 is the structural representation of the aircraft provided by the present invention when renovating opening；
Fig. 3 is the explosive view of aircraft provided by the present invention；
Fig. 4 is Fig. 1 sectional view；
Fig. 5 is the structural representation provided by the present invention renovated；
Fig. 6 is the structural representation of screen fixed seat provided by the present invention；
Fig. 7 is the structural representation of rotating shaft fixed block provided by the present invention；
Fig. 8 is the structural representation of fixed plate provided by the present invention.
In figure：1st, aircraft skin；101st, mounting groove；102nd, slot；103rd, neck；
2nd, renovate；201st, housing is renovated；202nd, connecting portion；203rd, it is open；204th, grab；205th, handle portion；
3rd, screen fixed seat；301st, fixed seat body；302nd, the first otic placode；303rd, the first connecting hole；304th, the second otic placode；
305th, the second connecting hole；
4th, rotating shaft fixed block；401st, third ear plate；402nd, the 3rd connecting hole；403rd, screwed hole；
5th, fixed plate；501st, the 4th connecting hole；502nd, fixture block；
6th, first rotating shaft；7th, the second rotating shaft；8th, screen.
Embodiment
Further illustrate technical scheme below in conjunction with the accompanying drawings and by embodiment.
As shown in Figures 1 to 4, screen turning device includes renovating 2 and screen fixed seat 3, and screen 8 is placed in screen fixed seat
In 3, screen fixed seat 3 can around renovate 2 one end rotate so as to insertion renovate in 2, renovate 2 can spiral-lock in aircraft skin
On 1.
Compared to directly screen 8 is fixed on aircraft skin in the prior art, when needing to carry out aircraft interior dimension
, it is necessary to which screen 8 is disassembled when repairing or needing to change aircraft interior part, the present invention by screen 8 by being placed in screen
In fixed seat 3,2 spiral-locks are renovated on aircraft skin 1, and screen fixed seat 3 rotates into that renovate can in 2 around renovating 2 one end
Realization needs repairing and aircraft or needs that aircraft skin 1 need not be dismantled during the part for taking out aircraft interior, it is only necessary to
2 will be renovated to separate with aircraft skin 1, lifting upwards renovates 2, screen 8 just can automatic turning come out, maintenance will screen after finishing
Curtain 8 again upset enter renovate 2 after spiral-lock is in flying machine shell 1 again, the device is not only simple, and operation is flexible, and energy
Enough prevent from repeatedly dismantling screen influence FPC cablings, be conducive to improving the reliability of FPC cablings, increase the service life of aircraft.
Specifically, being provided with the mounting groove 101 for accommodating parts (such as battery, FPC) on aircraft skin 1.Such as Fig. 5
Shown, renovating 2 includes renovating housing 201 and connecting portion 202, and the projection of connecting portion 202 is renovated on the side for renovating housing 201
Opening 203 is provided with housing 201, can be intuitively by opening 203 when screen fixed seat 3, which is rotated into, renovates 2 inside
See the information on screen, for the ease of will repeatedly renovate 2 spiral-locks on aircraft skin 1, be provided with aircraft skin 1
Neck 103, is provided with grab 204 on connecting portion 202, and grab 204 can be caught in aircraft skin 1 in neck 103 and turn over
The clamping of lid 2, clamping is not only simple in structure, conveniently opening and closing, and is hardly damaged aircraft skin during multiple keying renovates 2
1 and renovate 2.For the clamping intensity for improving aircraft skin 1 with renovating 2, in the present embodiment, the quantity of connecting portion 202 is
Four, four connecting portions 202 are provided with a grab 204 along renovating on being arranged circumferentially for housing 201, each connecting portion 202,
Corresponding, the neck 103 on aircraft skin 1 is similarly four, and sideline of four necks 103 along mounting groove 101 is uniformly arranged,
Overall radial, each grab 204 can be caught in a neck 103.2 are renovated for the ease of renovating 2 in spiral-lock or detaining to open
When exert oneself, handle portion 205 is provided with the side for renovate 2, in order to increase friction, handle portion 502 be provided with wheel dentation knot
Structure, in the present embodiment, in order to further be easy to exert oneself, the quantity of handle portion 502 is set to two, two 502 points of handle portions
It is not arranged on and renovates on 2 two relative sides.
As shown in fig. 6, screen fixed seat 3 includes fixed seat body 301, the first otic placode 302 and the second otic placode 304, it is fixed
The screen mounting groove for installing screen, one side of the projection of the first otic placode 302 in fixed seat body 301 are provided with seat body 301
On, the first connecting hole 303 is provided with being convexly equipped with this sideways relative side on the second otic placode 302, the first otic placode 302,
It is provided with the second connecting hole 305 on two otic placodes 304, the quantity of the first otic placode 302 and the second otic placode 304 is set as the case may be
It is fixed, do not limit herein, in the present embodiment, in order to improve the quantity of bonding strength, the first otic placode 302 and the second otic placode 304
It is two.
In order to improve renovate 2 and screen fixed seat 3 rotate connection flexibility and reduction renovate 2 and screen fixed seat 3
Loss in rotation process, rotating shaft fixed block 4 is provided with renovating between 2 and screen fixed seat 3, as shown in fig. 7, rotating shaft is solid
It is convexly equipped with the lower surface for determining block 4 on third ear plate 401, third ear plate 401 and is provided with the 3rd connecting hole 402, rotating shaft fixed block 4
Upper surface be provided with screwed hole 403, screw rotating shaft fixed block 4 is fixedly connected on through screwed hole 403 renovate 2 inner face
On, first rotating shaft 6 sequentially passes through the first connecting hole 302 and the 3rd connecting hole 402 by 3 turns of rotating shaft fixed block 4 and screen fixed seat
Dynamic connection, screen fixed seat 3 can be rotated into around first rotating shaft 6 and renovated in housing 201.
Screen fixed seat 3 and aircraft skin are connected and reduce in order to which screen fixed seat 3 is rotated with aircraft skin 1
1 loss in rotation process, is provided with fixed plate 5 between screen fixed seat 3 and aircraft skin 1, as shown in figure 8, solid
One end of fixed board 501 rotates with the second otic placode 304 and is connected, specifically, the 4th connecting hole 501 is provided with fixed plate 5, second turn
Axle 7 sequentially passes through the second connecting hole 305 and screen fixed seat 3 is rotated and is connected by the 4th connecting hole 501 with fixed plate 5.
In order to improve the smart and be easy to whole screen to overturn that whole screen turning device is connected with aircraft skin 1
The dismounting and installation of device, in the present embodiment, are provided with the slot 102 being made up of plate body, plate body on the inwall of mounting groove 101
On be provided with hole clipping, fixed plate 5 is provided with fixture block 502 away from the one end of screen fixed seat 3, and fixed plate 5 is inserted into slot 102
Interior, fixture block 502 can be caught in hole clipping and be fixedly connected with fixed plate 501 with aircraft skin 1.Certainly in other embodiments,
Hole clipping can also be replaced with the guide groove being arranged on plate body, fixture block 502 is caught in guide groove and can moved along guide groove,
When lifting renovates 2 upwards, fixed plate 5 can be removed mounting groove 101, so as to expand the movable model of whole screen turning device
Enclose, in order to expand maintenance aircraft or change the operating space for the parts being located in mounting groove 101.
The present embodiment additionally provides a kind of aircraft for including above-mentioned screen turning device, the aircraft needing repairing or
When person changes the parts such as battery, it is not necessary to disassemble whole aircraft skin 1 and screen 8, it is only necessary to renovating 2 use
Power, will renovate 2 grab 204 and is separated with the neck 103 on aircraft skin 1, then up lifting renovate 2 just can automatically by
The screen fixed seat 3 for being fixed with screen 8 is flipped out, and not only operates flexible, and the used time is short, and screen fixed seat 3 is placed in renovates 2
Inside be conducive to improving the reliability of FPC cablings, the energy of rotating shaft fixed block 4 is set between 2 and screen fixed seat 3 by being arranged on to renovate
It is enough multiple rotary is given renovate 2 and screen fixed seat 3 damage that brings be transferred on rotating shaft fixed block 4, increase aircraft makes
With the life-span, reduction maintenance and replacement cost, can by setting fixed plate 5 between screen fixed seat 3 and aircraft skin 1
The time that whole screen turning device is attached to aircraft skin 1 is reduced, installation effectiveness is improved.
Obviously, the above embodiment of the present invention is just for the sake of clear explanation example of the present invention, and is not pair
The restriction of embodiments of the present invention.For those of ordinary skill in the field, may be used also on the basis of the above description
To make other changes in different forms.There is no necessity and possibility to exhaust all the enbodiments.It is all this
Any modifications, equivalent substitutions and improvements made within the spirit and principle of invention etc., should be included in the claims in the present invention
Protection domain within.
Claims (10)
1. a kind of screen turning device, it is characterised in that screen fixed seat (3) and spiral-lock including fixed mask (8) are in flight
Renovating (2) on device shell (1), the screen fixed seat (3) can renovate the rotation of (2) one end so as to be turned over described in embedded around described
Cover in (2).
2. screen turning device according to claim 1, it is characterised in that the screen turning device is also solid including rotating shaft
Determine block (4), the rotating shaft fixed block (4) be arranged on the screen fixed seat (3) and it is described renovate between (2), the rotating shaft is consolidated
Determine block (4) one end to be fixedly connected with renovate (2), rotating shaft fixed block (4) other end turns with the screen fixed seat (3)
Dynamic connection, the one end of the screen fixed seat (3) away from the rotating shaft fixed block (4) is rotated with the aircraft skin (1) to be connected
Connect.
3. screen turning device according to claim 2, it is characterised in that the screen turning device also includes fixed plate
(5), described fixed plate (5) one end rotates with the screen fixed seat (3) and is connected, and fixed plate (5) other end flies with described
Row device shell (1) is fixedly connected.
4. screen turning device according to claim 3, it is characterised in that described renovate (2) include turning over for being fixedly connected
Lid housing (201) and connecting portion (202), it is described to renovate the opening (203) being provided with housing (201) for display screen (8),
Renovate (2) can be fixedly connected by the connecting portion (202) with the aircraft skin (1).
5. screen turning device according to claim 4, it is characterised in that be provided with grab on the connecting portion (202)
(204) neck (103), is provided with the aircraft skin (1), the grab (204) can be caught in the neck (103)
(2) and the aircraft skin (1) clamping is renovated by described.
6. screen turning device according to claim 4, it is characterised in that the screen fixed seat (3) includes fixed seat
Body (301), the first otic placode (302) and the second otic placode (304), first otic placode (302) and second otic placode (304) point
Other projection is on the relative two sides of the fixed seat body (301), first otic placode (302) and the rotating shaft fixed block
(4) connection is rotated, second otic placode (304) rotates with the fixed plate (5) and is connected.
7. screen turning device according to claim 6, it is characterised in that set first on first otic placode (302)
It is convexly equipped with third ear plate (401), the third ear plate (401) and is provided with connecting hole (303), the rotating shaft fixed block (4)
3rd connecting hole (402), first rotating shaft (6) sequentially passes through the first connecting hole (303) and the 3rd connecting hole (402) by the screen
Fixed seat (3) is rotated with the rotating shaft fixed block (4) and is connected.
8. screen turning device according to claim 6, it is characterised in that is provided with second otic placode (304)
The 4th connecting hole (501) is provided with two connecting holes (305), the fixed plate (5), the second rotating shaft (7) sequentially passes through the second company
Hole (305) and the 4th connecting hole (501) is connect to be connected the screen fixed seat (3) with the fixed plate (5) rotation.
9. screen turning device according to claim 8, it is characterised in that be provided with the aircraft skin (1) slotting
Hole clipping is provided with groove (102), the slot (102), the one end of the fixed plate (5) away from the screen fixed seat (3) is convex
Provided with fixture block (502), the fixed plate (5) is inserted into the slot (102), and the fixture block (502) can be caught in described
The fixed plate (5) is fixedly connected with the aircraft skin (1) in hole clipping.
10. a kind of aircraft, it is characterised in that include the screen turning device any one of claim 1-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710342371.1A CN107010217B (en) | 2017-05-16 | 2017-05-16 | Screen turning device and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710342371.1A CN107010217B (en) | 2017-05-16 | 2017-05-16 | Screen turning device and aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107010217A true CN107010217A (en) | 2017-08-04 |
| CN107010217B CN107010217B (en) | 2023-07-25 |
Family
ID=59449620
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710342371.1A Active CN107010217B (en) | 2017-05-16 | 2017-05-16 | Screen turning device and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107010217B (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140297067A1 (en) * | 2012-08-02 | 2014-10-02 | Benjamin Malay | Vehicle control system |
| CN204390741U (en) * | 2015-01-16 | 2015-06-10 | 苏州普福斯信息科技有限公司 | A kind of operator guards of flip-shell solid state hard disc |
| CN105857587A (en) * | 2016-03-31 | 2016-08-17 | 英华达（上海）科技有限公司 | Multi-axis unmanned aerial vehicle and flight method thereof |
| CN205782254U (en) * | 2016-05-27 | 2016-12-07 | 温州冠天科技有限公司 | A kind of multi-functional LED desk lamp |
| CN106218909A (en) * | 2016-09-23 | 2016-12-14 | 珠海格力电器股份有限公司 | aircraft and aerial photography system |
| US20160376004A1 (en) * | 2015-03-16 | 2016-12-29 | XCraft Enterprises, LLC | Unmanned aerial vehicle with detachable computing device |
| CN205872491U (en) * | 2016-04-14 | 2017-01-11 | 普宙飞行器科技（深圳）有限公司 | Unmanned vehicles with display screen |
| CN207328824U (en) * | 2017-05-16 | 2018-05-08 | 上海未来伙伴机器人有限公司 | A kind of screen turnover device and aircraft |
-
2017
- 2017-05-16 CN CN201710342371.1A patent/CN107010217B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140297067A1 (en) * | 2012-08-02 | 2014-10-02 | Benjamin Malay | Vehicle control system |
| CN204390741U (en) * | 2015-01-16 | 2015-06-10 | 苏州普福斯信息科技有限公司 | A kind of operator guards of flip-shell solid state hard disc |
| US20160376004A1 (en) * | 2015-03-16 | 2016-12-29 | XCraft Enterprises, LLC | Unmanned aerial vehicle with detachable computing device |
| CN105857587A (en) * | 2016-03-31 | 2016-08-17 | 英华达（上海）科技有限公司 | Multi-axis unmanned aerial vehicle and flight method thereof |
| CN205872491U (en) * | 2016-04-14 | 2017-01-11 | 普宙飞行器科技（深圳）有限公司 | Unmanned vehicles with display screen |
| CN205782254U (en) * | 2016-05-27 | 2016-12-07 | 温州冠天科技有限公司 | A kind of multi-functional LED desk lamp |
| CN106218909A (en) * | 2016-09-23 | 2016-12-14 | 珠海格力电器股份有限公司 | aircraft and aerial photography system |
| CN207328824U (en) * | 2017-05-16 | 2018-05-08 | 上海未来伙伴机器人有限公司 | A kind of screen turnover device and aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107010217B (en) | 2023-07-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206834876U (en) | Ceiling fan motor | |
| CN207328824U (en) | A kind of screen turnover device and aircraft | |
| CN107010217A (en) | A kind of screen turning device and aircraft | |
| CN206186820U (en) | Charge post for electric vehicles | |
| CN207772919U (en) | A kind of foldable charging equipment for automobile of cable | |
| CN209653960U (en) | A kind of Ice removing machine | |
| CN107516927B (en) | A kind of autonomous power supply device of drag conveyor chain monitoring node | |
| CN103217077B (en) | Intelligent ammunition carrying box | |
| CN204140307U (en) | The novel air compressor that a kind of resuscitation apparatus is optimized | |
| CN105539857B (en) | Unmanned plane battery interface arrangment | |
| CN204946353U (en) | Improvement type vehicle location monitor device | |
| CN208007283U (en) | A kind of forest early warning and reconnaissance unmanned plane | |
| CN209320737U (en) | A kind of charging gun and charging pile | |
| CN205388979U (en) | Battery structure for unmanned aerial vehicle | |
| CN207474916U (en) | A kind of lightning-arrest needle construction of prefabricated cabin | |
| CN203633562U (en) | Multifunctional safety helmet | |
| CN208838926U (en) | A kind of Vehicular multifunctional fire bucket | |
| CN205358592U (en) | Financial management bill strorage device | |
| CN205908624U (en) | A pivot structure for dressing equipment | |
| CN206176108U (en) | Flashlight | |
| CN206664919U (en) | A kind of unmanned plane | |
| CN205311720U (en) | Electric automobile's mouthful structure of charging | |
| CN204984665U (en) | Automatic clearance dust car air inlet filter equipment | |
| CN215249013U (en) | Hoisting sling | |
| CN212564124U (en) | Clutch driven disc assembly with reinforcing protection device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |