CN204197278U - A kind of mechanism connected for alighting gear - Google Patents
A kind of mechanism connected for alighting gear Download PDFInfo
- Publication number
- CN204197278U CN204197278U CN201420647947.7U CN201420647947U CN204197278U CN 204197278 U CN204197278 U CN 204197278U CN 201420647947 U CN201420647947 U CN 201420647947U CN 204197278 U CN204197278 U CN 204197278U
- Authority
- CN
- China
- Prior art keywords
- swing arm
- drive shaft
- supporting seat
- axle drive
- hole
- 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
Links
Landscapes
- Seats For Vehicles (AREA)
Abstract
The utility model discloses a kind of mechanism connected for alighting gear, described mechanism comprises: S. A.; Axle drive shaft; Swing arm, one end of swing arm is fixedly connected with one end of alighting gear, and the other end of swing arm is flexibly connected with S. A. respectively, is fixedly connected with axle drive shaft; Supporting seat, one end of supporting seat is fixedly connected with fuselage, the other end of supporting seat is flexibly connected with S. A. respectively, is connected with axle drive shaft slide rail, achieve when unmanned plane needs flight operation, axle drive shaft is by driving swing arm rotating shaft centered by S. A. to rotate with supporting seat relative sliding, make the swing arm in rotating drive alighting gear carry out reclaiming and be in indentation state, realize the unobstructed flight Collecting operation of information collecting device 360 ° be arranged on bottom unmanned aerial vehicle body; Overcome alighting gear in prior art and often block parts of images, video information, and then cause information collecting device to occur the phenomenon of " leakage is adopted ", the information that information collecting device is gathered incomplete defect.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, particularly a kind of mechanism connected for alighting gear.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Without driving compartment on machine, but the equipment such as autopilot, process controller, information collecting device are installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, it is followed the tracks of, locates, remote control, remote measurement and digital communication.Can take off as conventional airplane under radio telecommand or launch with booster rocket, also can be taken to by machine tool and throw in flight in the air.
Unmanned plane comprises fuselage, information collecting device (cloud platform control system), this information collecting device is arranged on the bottom of unmanned aerial vehicle body, for graphicinformation, the collection of video information, in prior art, the fuselage of unmanned plane often adopts with the alighting gear for supporting this fuselage the mode be fixedly connected with, alighting gear is made to be in the state of relative securement relative to the fuselage of unmanned plane, so that realize firm support to unmanned aerial vehicle body, but the mode that this fuselage is fixedly connected with alighting gear makes unmanned plane no matter be when flying operation, due to the existence of alighting gear, in camera in information collecting device 360 ° of rotating acquisition operation process, when gathering sight line and alighting gear is same direction, alighting gear often blocks parts of images, video information, and then cause information collecting device to occur the phenomenon of " leakage is adopted ", the information that information collecting device is gathered is also imperfect.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of mechanism connected for alighting gear, this mechanism achieves when unmanned plane needs flight operation, axle drive shaft is by driving swing arm rotating shaft centered by S. A. to rotate with supporting seat relative sliding, make the swing arm in rotating drive alighting gear carry out reclaiming and be in indentation state, realize the unobstructed flight Collecting operation of described information collecting device 360 °.
For solving the problems of the technologies described above, the utility model provides a kind of mechanism connected for alighting gear, and be applied to unmanned plane, described unmanned plane comprises fuselage, information collecting device, described information collecting device is arranged on the bottom of described fuselage, and described mechanism comprises: S. A.; Axle drive shaft; Swing arm, one end of described swing arm is fixedly connected with one end of described alighting gear, the other end of described swing arm is flexibly connected with described S. A. respectively, is fixedly connected with described axle drive shaft, described swing arm can be rotated centered by described S. A. in rotating shaft, and described S. A. is positioned at the top of described axle drive shaft; Supporting seat, one end of described supporting seat is fixedly connected with described fuselage, the other end of described supporting seat is flexibly connected with described S. A. respectively, be connected with described axle drive shaft slide rail, and when described axle drive shaft is connected by described slide rail and described supporting seat carries out relative sliding, described swing arm rotating shaft centered by described S. A. can be made to carry out relative rotation with described supporting seat; Wherein, when described unmanned plane needs flight operation, described axle drive shaft is by driving described swing arm rotating shaft centered by described S. A. to rotate with described supporting seat relative sliding, make the described swing arm in rotating drive described alighting gear carry out reclaiming and be in indentation state, realize the unobstructed flight Collecting operation of described information collecting device 360 °; When described unmanned plane does not need flight operation, described axle drive shaft is by driving described swing arm rotating shaft centered by described S. A. to rotate with described supporting seat relative sliding, make the described swing arm in rotating drive described alighting gear to carry out launching and being in open configuration, realize described unmanned plane by described gear support on the ground.
Further, the other end of described swing arm is respectively arranged with the first through hole, the second through hole, and described first through hole is positioned at the top of described second through hole, the aperture of described first through hole and the external diameter of described S. A. suitable, the aperture of described second through hole and the external diameter of described axle drive shaft suitable, described S. A. is flexibly connected with described swing arm through described first through hole, and described axle drive shaft is fixedly connected with described swing arm through described second through hole.
Further, the other end of described supporting seat is respectively arranged with third through-hole and chute, described third through-hole is corresponding with the position of described first through hole, described supporting seat is flexibly connected with described swing arm through described third through-hole, described first through hole by described S. A. successively, described chute is corresponding with the position of described second through hole, the end of described axle drive shaft is horizontal to be connected with described supporting seat slide rail in described chute inside, makes described axle drive shaft drive described swing arm to rotate around described S. A. when sliding in described chute inside.
Further, described supporting seat comprises: the first strut member, and described first strut member is square structure, and described first strut member is fixedly connected with described fuselage; Second strut member, described second strut member is square structure, and the position, top of described second strut member offers described third through-hole, the lower portion of described second strut member offers described chute, and described first strut member is fixedly connected with described second strut member.
Further, the quantity of described supporting seat is 2, and 2 described supporting seats are symmetrically distributed in the both sides of described swing arm, corresponding horizontal 2 described chutes at 2 supporting seats are inner respectively in the end, two ends of described axle drive shaft, make described axle drive shaft drive described swing arm to rotate around described S. A. when sliding in the chute inside of 2 described supporting seats.
Further, being fixedly connected with between one end of described swing arm and one end of described alighting gear is that bolt is connected; And/or the other end of described swing arm is weld with being fixedly connected with between described axle drive shaft.
Further, one end of described supporting seat is that bolt is connected with being fixedly connected with between described fuselage.
Further, described first strut member is that bolt is connected with being fixedly connected with between described fuselage; And/or being fixedly connected with between described first strut member with described second strut member is that bolt is connected.
A kind of mechanism connected for alighting gear that the utility model provides, by one end of swing arm is fixedly connected with one end of alighting gear, the other end of swing arm is flexibly connected with S. A. respectively, be fixedly connected with axle drive shaft, one end of supporting seat is fixedly connected with fuselage, being flexibly connected with S. A. respectively of the other end of supporting seat, be connected with axle drive shaft slide rail, achieve when unmanned plane needs flight operation, axle drive shaft is by driving swing arm rotating shaft centered by S. A. to rotate with supporting seat relative sliding, the swing arm in rotating is made to drive alighting gear carry out reclaiming and be in indentation state, realize the unobstructed flight Collecting operation of information collecting device 360 ° be arranged on bottom unmanned aerial vehicle body, overcome alighting gear in prior art and often block parts of images, video information, and then cause information collecting device to occur the phenomenon of " leakage is adopted ", the information that information collecting device is gathered incomplete defect.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
The annexation schematic diagram of the alighting gear that Fig. 1 provides for the utility model embodiment, supporting seat, swing arm, axle drive shaft and S. A.; And
The annexation front view of the supporting seat that Fig. 2 provides for the utility model embodiment, swing arm, axle drive shaft and S. A.; And
The fractionation structural representation of the supporting seat that Fig. 3 provides for the utility model embodiment, swing arm, axle drive shaft and S. A..
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, the every other embodiment that those of ordinary skill in the art obtain, all belongs to the scope of the utility model protection; Wherein involved in this enforcement "and/or" keyword, represent and or two kinds of situations, in other words, A and/or B mentioned by the embodiment of the present invention, illustrates A and B, A or B two kinds of situations, describes three kinds of states existing for A and B, as A and/or B, represent: only include A and do not comprise B; Only include B and do not comprise A; Comprise A and B.
See Fig. 1, a kind of mechanism connected for alighting gear that the utility model embodiment provides, be applied to unmanned plane, wherein, unmanned plane comprises fuselage, information collecting device, information collecting device is arranged on the bottom of fuselage, this mechanism achieves when unmanned plane needs flight operation, axle drive shaft 11 is by driving swing arm 12 rotating shaft centered by S. A. 10 to rotate with supporting seat relative sliding, the swing arm 12 in rotating is made to drive alighting gear 13 carry out reclaiming and be in indentation state, realize the unobstructed flight Collecting operation of information collecting device 360 °, the fuselage overcoming unmanned plane in prior art with the alighting gear for supporting this fuselage owing to adopting the mode be fixedly connected with, unmanned plane is made no matter to be when flying operation, due to the existence of alighting gear, in camera in information collecting device 360 ° of rotating acquisition operation process, when gathering sight line and alighting gear is same direction, alighting gear often blocks parts of images, video information, and then cause information collecting device to occur the phenomenon of " leakage is adopted ", the information that information collecting device is gathered incomplete defect.
Specifically, refer to Fig. 2-3, this mechanism at least comprises: S. A. 10, axle drive shaft 11, swing arm 12, supporting seat, wherein, one end of swing arm 12 is fixedly connected with one end of alighting gear 13, the position, top of the other end of swing arm 12 is flexibly connected with S. A. 10, the lower portion of the other end of swing arm 12 is fixedly connected with axle drive shaft 11 (top that S. A. 10 is positioned at axle drive shaft 11), and being flexibly connected between swing arm 12 with S. A. 10 can make swing arm 12 rotating shaft centered by S. A. 10 rotate, one end of supporting seat is fixedly connected with the fuselage of unmanned plane, the position, top of the other end of supporting seat is flexibly connected with S. A. 10, the lower portion of the other end of supporting seat is connected with axle drive shaft 11 slide rail, and when carrying out relative sliding by the connection of this slide rail with supporting seat for ease of axle drive shaft 11, swing arm 12 rotating shaft centered by S. A. 10 can be made to carry out relative rotation with supporting seat, the utility model embodiment is by the top position of S. A. 10 through the other end of swing arm 12, and make the middle part of S. A. 10 be positioned at the inside of swing arm 12 and be flexibly connected with swing arm 12, the end of S. A. 10 is flexibly connected with the position, top of the other end of supporting seat, corresponding, axle drive shaft 11 is through the lower portion of the other end of swing arm 12, and make the middle part of axle drive shaft 11 be positioned at the inside of swing arm 12 and be fixedly connected with swing arm 12, the end of axle drive shaft 11 is fixedly connected with the lower portion of the other end of supporting seat, final realization is when unmanned plane needs flight operation, axle drive shaft 11 is by (can see Fig. 2 with supporting seat relative sliding, now axle drive shaft 11 slides to the right) driving swing arm 12 rotating shaft centered by S. A. 10 to carry out rotating (can see Fig. 2, now swing arm 12 left-hand revolution), making the swing arm 12 in rotating drive alighting gear 13 to carry out reclaiming and be in indentation state (can see Fig. 1, now alighting gear 13 left-hand revolution), realize the unobstructed flight Collecting operation of information collecting device 360 ° be arranged on bottom unmanned aerial vehicle body, when unmanned plane does not need flight operation, axle drive shaft 11 is by (can see Fig. 2 with supporting seat relative sliding, now axle drive shaft 11 slides left) driving swing arm 12 rotating shaft centered by S. A. 10 to carry out rotating (can see Fig. 2, now swing arm 12 clickwise), making the swing arm 12 in rotating drive alighting gear 13 to carry out launching and be in open configuration (can see Fig. 1, now alighting gear 13 clickwise), realize described unmanned plane by the firm support of alighting gear 13 on the ground.
In the utility model embodiment, preferably, the position, top of the other end of swing arm 12 is provided with the first through hole, the aperture of the first through hole and the external diameter of S. A. 10 suitable, and then S. A. 10 is flexibly connected with swing arm 12 through the first through hole, now the middle part of S. A. 10 is in the inside of swing arm 12, the position, top of the other end of supporting seat is provided with third through-hole simultaneously, to offer position corresponding for offer position and the first through hole position above the other end of swing arm 12 of this third through-hole, now corresponding being flexibly connected with supporting seat through third through-hole in the end of S. A. 10, the utility model embodiment passes through middle part and the end portion of Appropriate application S. A. 10, swing arm 12 is made to realize swing arm 12 can relatively rotate relative to S. A. 10 by being flexibly connected with the middle part of S. A. 10, supporting seat realizes S. A. 10 can relatively rotate relative to supporting seat by being flexibly connected with the end portion of S. A. 10, finally achieve the middle part by means of only Appropriate application S. A. 10, end portion can reach supporting seat transfixion, the technique effect rotated is carried out in swing arm 12 relative to supporting seat, there is structure simple, distribute feature that is compact and easy installation.
In the utility model embodiment, preferably, the lower portion of the other end of swing arm 12 is provided with the second through hole, the aperture of the second through hole and the external diameter of axle drive shaft 11 suitable, and then axle drive shaft 11 is fixedly connected with swing arm 12 through the second through hole, now the middle part of axle drive shaft 11 is in the inside of swing arm 12, the lower portion of the other end of supporting seat is provided with chute simultaneously, to offer position in the lower portion of the other end of swing arm 12 corresponding for offer position and second through hole of this chute, now corresponding being connected with supporting seat slide rail through chute in the end of axle drive shaft 11, the utility model embodiment passes through middle part and the end portion of Appropriate application axle drive shaft 11, make swing arm 12 by being fixedly connected with the middle part of axle drive shaft 11, supporting seat is by being connected with the end portion slide rail of axle drive shaft 11, realize when axle drive shaft 11 slides in the chute of supporting seat, driving swing arm 12 rotating shaft centered by S. A. 10 to rotate, and realize swing arm 12 clickwise or left-hand revolution by controlling axle drive shaft 11 slip left or slip to the right in chute, finally reach control alighting gear and be in indentation state or open configuration.
In the utility model embodiment, for ease of the dismounting of supporting seat, easy to maintenance, preferably, supporting seat can comprise: the first strut member 14, second strut member 15, wherein, first strut member 14, second strut member 15 can be square structure and make structure simple, and one end of the first strut member 14 is fixedly connected with the fuselage of unmanned plane, the position, top of the second strut member 15 offers described third through-hole, the lower portion of described second strut member offers above-mentioned chute, first strut member is fixedly connected with the second strut member, and the first strut member 14 and being fixedly connected with between fuselage, being fixedly connected with between the first strut member 14 with the second strut member 15 can be all that bolt is connected, make detachable therebetween, to reach the dismounting of supporting seat, substitute, technique effect easy to maintenance.Corresponding, the utility model embodiment is for ease of the dismounting, easy to maintenance of swing arm 12 or alighting gear 13, and preferably, being fixedly connected with between one end of swing arm 12 and one end of alighting gear 13 is that bolt is connected.
In the utility model embodiment, for ease of supporting seat, swing arm 12 connects fastening therebetween, occur when preventing swing arm 12 from rotating relative to supporting seat loosening, unsteady phenomenon, preferably, the quantity of supporting seat can be 2, and 2 supporting seats are symmetrically distributed in the both sides of swing arm 12, corresponding 2 the chute inside being horizontally installed on 2 supporting seats respectively, end, two ends of axle drive shaft 11, end, two ends corresponding 2 third through-holes through 2 supporting seats respectively of S. A. 10, axle drive shaft 11 is made to drive firm the rotating around S. A. 10 of swing arm 12 when sliding in the chute inside of 2 supporting seats.
It needs to be noted, the connection structure that the utility model embodiment provides, for the connection of alighting gear and unmanned aerial vehicle body, except manually moving alighting gear disturbance S. A. 10 except needing operating personnel and rotating, the utility model embodiment also can set up DC machine and signal receiving device in the inside of the first strut member 14, wherein, DC machine is slided for driving axle drive shaft 11, signal receiving device is used for the driving instruction that Received signal strength harvester (cloud platform control system) is launched, this DC machine is by being electrically connected with signal receiving device, be mechanically connected with axle drive shaft, make when unmanned plane needs flight operation, signal pickup assembly (cloud platform control system) is by launching driving instruction to signal receiving device, signal receiving device controls DC machine after receiving driving instruction and mates operation with axle drive shaft 11 (by worm and gear principle), realize moving to left or moving right of axle drive shaft 11, finally reach Based Intelligent Control alighting gear 13 launch or reclaim operation.
A kind of mechanism connected for alighting gear that the utility model embodiment provides, its beneficial effect is as described below:
1., the utility model is by being fixedly connected with one end with alighting gear 13, one end of swing arm 12, the position, top of the other end of swing arm 12 is flexibly connected with S. A. 10, the lower portion of the other end of swing arm 12 is fixedly connected with axle drive shaft 11, one end of supporting seat is fixedly connected with fuselage, the position, top of the other end of supporting seat is flexibly connected with S. A. 10, the lower portion of the other end of supporting seat is connected with axle drive shaft 11 slide rail, achieve when unmanned plane needs flight operation, axle drive shaft 11 is by driving swing arm 12 rotating shaft centered by S. A. 10 to rotate with supporting seat relative sliding, the swing arm 12 in rotating is made to drive alighting gear 13 carry out reclaiming and be in indentation state, realize the unobstructed flight Collecting operation of information collecting device 360 ° be arranged on bottom unmanned aerial vehicle body, overcome alighting gear 13 in prior art and often block parts of images, video information, and then cause information collecting device to occur the phenomenon of " leakage is adopted ", the information that information collecting device is gathered incomplete defect,
2., the utility model is by arranging the first through hole, second through hole, third through-hole and chute, S. A. 10 is flexibly connected with swing arm 12 through the first through hole, corresponding being flexibly connected with supporting seat through third through-hole in end of S. A. 10, axle drive shaft 11 is fixedly connected with swing arm 12 through the second through hole, corresponding being connected with supporting seat slide rail through chute in end of axle drive shaft 11, make the utility model Appropriate application S. A. 10, the middle part of axle drive shaft 11, end portion can reach supporting seat transfixion, the technique effect rotated is carried out in swing arm 12 relative to supporting seat, there is structure simple, distribute feature that is compact and easy installation,
3., the utility model is by arranging by the first strut member 14, second strut member 15 forms supporting seat, and one end of the first strut member 14 is connected with the fuselage bolt of unmanned plane, third through-hole is offered at the position, top of the second strut member 15, the lower portion of the second strut member offers chute, first strut member is connected with the second strut member bolt, make Appropriate application first strut member 14, while second position, strut member 15 each space, therebetween detachable, there is supporting seat dismounting, replacement, technique effect easy to maintenance;
4., the utility model is by selecting the quantity of supporting seat to be 2, and 2 supporting seats are symmetrically distributed in the both sides of swing arm 12, corresponding 2 the chute inside being horizontally installed on 2 supporting seats respectively, end, two ends of axle drive shaft 11, end, two ends corresponding 2 third through-holes through 2 supporting seats respectively of S. A. 10, axle drive shaft 11 is made to drive firm the rotating around S. A. 10 of swing arm 12 when sliding in the chute inside of 2 supporting seats, achieve supporting seat, swing arm 12 connects more fastening therebetween, occur when preventing swing arm 12 to rotate relative to supporting seat loosening, unsteady phenomenon, have the advantages that safety performance is high.
It should be noted last that, above detailed description of the invention is only in order to illustrate the technical solution of the utility model and unrestricted, although be described in detail the utility model with reference to example, those of ordinary skill in the art is to be understood that, can modify to the technical solution of the utility model or equivalent replacement, and not departing from the spirit and scope of technical solutions of the utility model, it all should be encompassed in the middle of right of the present utility model.
Claims (8)
1., for the mechanism that alighting gear connects, be applied to unmanned plane, described unmanned plane comprises fuselage, information collecting device, and described information collecting device is arranged on the bottom of described fuselage, it is characterized in that, described mechanism comprises:
S. A.;
Axle drive shaft;
Swing arm, one end of described swing arm is fixedly connected with one end of described alighting gear, the other end of described swing arm is flexibly connected with described S. A. respectively, is fixedly connected with described axle drive shaft, described swing arm can be rotated centered by described S. A. in rotating shaft, and described S. A. is positioned at the top of described axle drive shaft;
Supporting seat, one end of described supporting seat is fixedly connected with described fuselage, the other end of described supporting seat is flexibly connected with described S. A. respectively, be connected with described axle drive shaft slide rail, and when described axle drive shaft is connected by described slide rail and described supporting seat carries out relative sliding, described swing arm rotating shaft centered by described S. A. can be made to carry out relative rotation with described supporting seat.
2., as claimed in claim 1 for the mechanism that alighting gear connects, it is characterized in that,
The other end of described swing arm is respectively arranged with the first through hole, the second through hole, and described first through hole is positioned at the top of described second through hole, the aperture of described first through hole and the external diameter of described S. A. suitable, the aperture of described second through hole and the external diameter of described axle drive shaft suitable, described S. A. is flexibly connected with described swing arm through described first through hole, and described axle drive shaft is fixedly connected with described swing arm through described second through hole.
3., as claimed in claim 2 for the mechanism that alighting gear connects, it is characterized in that,
The other end of described supporting seat is respectively arranged with third through-hole and chute, described third through-hole is corresponding with the position of described first through hole, described supporting seat is flexibly connected with described swing arm through described third through-hole, described first through hole by described S. A. successively, described chute is corresponding with the position of described second through hole, the end of described axle drive shaft is horizontal to be connected with described supporting seat slide rail in described chute inside, makes described axle drive shaft drive described swing arm to rotate around described S. A. when sliding in described chute inside.
4., as claimed in claim 3 for the mechanism that alighting gear connects, it is characterized in that, described supporting seat comprises:
First strut member, described first strut member is square structure, and described first strut member is fixedly connected with described fuselage;
Second strut member, described second strut member is square structure, and the position, top of described second strut member offers described third through-hole, the lower portion of described second strut member offers described chute, and described first strut member is fixedly connected with described second strut member.
5., as claimed in claim 3 for the mechanism that alighting gear connects, it is characterized in that,
The quantity of described supporting seat is 2, and 2 described supporting seats are symmetrically distributed in the both sides of described swing arm, corresponding horizontal 2 described chutes at 2 supporting seats are inner respectively in the end, two ends of described axle drive shaft, make described axle drive shaft drive described swing arm to rotate around described S. A. when sliding in the chute inside of 2 described supporting seats.
6., as claimed in claim 1 for the mechanism that alighting gear connects, it is characterized in that,
Being fixedly connected with between one end of described swing arm and one end of described alighting gear is that bolt is connected;
And/or,
The other end of described swing arm is weld with being fixedly connected with between described axle drive shaft.
7., as claimed in claim 1 for the mechanism that alighting gear connects, it is characterized in that,
One end of described supporting seat is that bolt is connected with being fixedly connected with between described fuselage.
8., as claimed in claim 4 for the mechanism that alighting gear connects, it is characterized in that,
Described first strut member is that bolt is connected with being fixedly connected with between described fuselage;
And/or,
Being fixedly connected with between described first strut member with described second strut member is that bolt is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420647947.7U CN204197278U (en) | 2014-10-31 | 2014-10-31 | A kind of mechanism connected for alighting gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420647947.7U CN204197278U (en) | 2014-10-31 | 2014-10-31 | A kind of mechanism connected for alighting gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204197278U true CN204197278U (en) | 2015-03-11 |
Family
ID=52655265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420647947.7U Expired - Fee Related CN204197278U (en) | 2014-10-31 | 2014-10-31 | A kind of mechanism connected for alighting gear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204197278U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104787308A (en) * | 2015-04-08 | 2015-07-22 | 零度智控（北京）智能科技有限公司 | Aircraft undercarriage driving device, aircraft undercarriage and aircraft |
| WO2016155250A1 (en) * | 2015-03-31 | 2016-10-06 | 深圳一电科技有限公司 | Unmanned aerial vehicle system, unmanned aerial vehicle and control method of unmanned aerial vehicle |
| CN106005376A (en) * | 2016-07-13 | 2016-10-12 | 合肥佳讯科技有限公司 | Automatic lifting mechanism applied to UAV (unmanned aerial vehicle) |
| CN106915438A (en) * | 2015-12-25 | 2017-07-04 | 北京臻迪机器人有限公司 | Unmanned plane |
| WO2018095214A1 (en) * | 2016-11-22 | 2018-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle and landing gear device thereof |
-
2014
- 2014-10-31 CN CN201420647947.7U patent/CN204197278U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016155250A1 (en) * | 2015-03-31 | 2016-10-06 | 深圳一电科技有限公司 | Unmanned aerial vehicle system, unmanned aerial vehicle and control method of unmanned aerial vehicle |
| CN104787308A (en) * | 2015-04-08 | 2015-07-22 | 零度智控（北京）智能科技有限公司 | Aircraft undercarriage driving device, aircraft undercarriage and aircraft |
| CN106915438A (en) * | 2015-12-25 | 2017-07-04 | 北京臻迪机器人有限公司 | Unmanned plane |
| CN106005376A (en) * | 2016-07-13 | 2016-10-12 | 合肥佳讯科技有限公司 | Automatic lifting mechanism applied to UAV (unmanned aerial vehicle) |
| CN106005376B (en) * | 2016-07-13 | 2017-11-14 | 合肥佳讯科技有限公司 | A kind of automatic lifting stick mechanism applied to unmanned plane |
| WO2018095214A1 (en) * | 2016-11-22 | 2018-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle and landing gear device thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204197278U (en) | A kind of mechanism connected for alighting gear | |
| CN104590556B (en) | A kind of folding unmanned plane | |
| US10661899B2 (en) | In flight transfer of packages between aerial drones | |
| CN105035339B (en) | Zoom-type unmanned plane | |
| US8370002B2 (en) | Multi-mission remote aerial refueling operator system | |
| CN203996886U (en) | A kind of four axle eight oars aircraft of taking photo by plane | |
| CN105314110A (en) | Unmanned aerial vehicle with umbrella | |
| CN205150264U (en) | Can dismantle unmanned aerial vehicle battery package assembly | |
| CN205022853U (en) | Many rotors flight equipment | |
| CN206243476U (en) | VTOL fixed-wing unmanned plane | |
| CN205045003U (en) | Novel unmanned aerial vehicle camera installing support device | |
| CN205022913U (en) | Carry image signal collection system's flight equipment | |
| CN103531044A (en) | Barrier alarm system for unmanned aerial vehicle | |
| CN206954510U (en) | It is a kind of can VTOL fixed-wing unmanned plane | |
| DE10313279B4 (en) | Device for depositing aerodynamically unstable missiles from a transport aircraft | |
| CN205293061U (en) | Folding assembly | |
| CN205203403U (en) | Power source | |
| CN205186530U (en) | Carry unmanned aerial vehicle of umbrella | |
| CN108557065A (en) | A kind of flight for unmanned plane and road row switching device | |
| CN107150806A (en) | It is a kind of can VTOL fixed-wing unmanned plane | |
| CN205010475U (en) | Unmanned aerial vehicle wing hinged joint structure | |
| CN105704379A (en) | Unmanned aerial vehicle camera system | |
| CN207129144U (en) | A kind of carrier gas unmanned plane | |
| CN103523203A (en) | Front camera cabin of unmanned aerial vehicle | |
| CN205131690U (en) | Built -in flight equipment that has automatically zoom formula signal pickup assembly |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 430000 Hubei province Wuhan Shiqiao Road No. 6 high-tech building Patentee after: EWATT CO., LTD. Address before: 430000 Hubei province Wuhan Shiqiao Road No. 6 high-tech building Patentee before: China Ewatt Technology Co., Ltd. |
|
| C56 | Change in the name or address of the patentee | ||
| CP03 | Change of name, title or address |
Address after: 430000 Hubei province Wuhan City Jiang'an District Lake Street Bridge Road No. 5 Building 1 layer 4 Patentee after: Easy Technology Co Ltd Address before: 430000 Hubei province Wuhan Shiqiao Road No. 6 high-tech building Patentee before: EWATT CO., LTD. |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150311 Termination date: 20181031 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |