CN113202372A - Unmanned cabin and cabin opening and closing method - Google Patents
Unmanned cabin and cabin opening and closing method Download PDFInfo
- Publication number
- CN113202372A CN113202372A CN202110527473.7A CN202110527473A CN113202372A CN 113202372 A CN113202372 A CN 113202372A CN 202110527473 A CN202110527473 A CN 202110527473A CN 113202372 A CN113202372 A CN 113202372A
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- China
- Prior art keywords
- cabin
- frame
- push rod
- door
- rail
- Prior art date
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- Pending
Links
- 238000000034 method Methods 0.000 title claims description 11
- 230000007246 mechanism Effects 0.000 claims abstract description 41
- 238000007789 sealing Methods 0.000 claims description 3
- 230000003014 reinforcing effect Effects 0.000 description 12
- 108010066057 cabin-1 Proteins 0.000 description 3
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/60—Power-operated mechanisms for wings using electrical actuators
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
- E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
- E06B3/32—Arrangements of wings characterised by the manner of movement; Arrangements of movable wings in openings; Features of wings or frames relating solely to the manner of movement of the wing
- E06B3/34—Arrangements of wings characterised by the manner of movement; Arrangements of movable wings in openings; Features of wings or frames relating solely to the manner of movement of the wing with only one kind of movement
- E06B3/42—Sliding wings; Details of frames with respect to guiding
- E06B3/46—Horizontally-sliding wings
- E06B3/4636—Horizontally-sliding wings for doors
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/108—Application of doors, windows, wings or fittings thereof for buildings or parts thereof for hangars
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/13—Application of doors, windows, wings or fittings thereof for buildings or parts thereof characterised by the type of wing
- E05Y2900/132—Doors
Abstract
The invention relates to an unmanned cabin which comprises a cabin body, a cabin door and a driving mechanism, wherein the cabin door is positioned above the cabin body, the driving mechanism is used for driving the cabin door to move relative to the cabin body, the cabin body comprises a cabin body frame and a cabin body panel arranged on the cabin body frame, the cabin door comprises a cabin door frame and a cabin door panel arranged on the cabin door frame, the driving mechanism is arranged between the top of the cabin body frame and the cabin door frame, the driving mechanism comprises a push rod, one end of the push rod is connected to the top of the cabin body frame, the other end of the push rod is connected to the cabin door frame, and the push rod is used for driving the cabin door to move horizontally. The push rod is an electric push rod. According to the unmanned engine room, the push rod is arranged between the cabin body frame and the cabin door frame, so that the cabin door can be horizontally opened and closed, and the unmanned engine room is simple in integral composition structure, low in cost and good in stability.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle cabin based on an electric push rod and a horizontal cabin opening and closing method of the unmanned aerial vehicle cabin.
Background
Along with the development of science and technology in recent years, the continuous maturity of unmanned aerial vehicle technique, unmanned airport helping hand unmanned aerial vehicle makes unmanned aerial vehicle's use scene constantly abundant. The switch cabin system is an important component of the unmanned airport, and the stability of the switch cabin system greatly improves the overall performance of the unmanned airport.
At present, most unmanned engine rooms and the method for opening and closing the engine rooms are in a wing span type, a connecting rod type and the like, and the method for opening the engine rooms is complex and poor in stability.
Disclosure of Invention
In view of the above, in order to overcome the defects of the prior art, the present invention aims to provide an improved unmanned cabin, which can realize horizontal opening and closing of the cabin door and has good stability.
In order to achieve the purpose, the invention adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle cabin, includes the cabin body, is located the hatch door of cabin body top and be used for the drive the hatch door for the actuating mechanism that the cabin body removed, the cabin body includes cabin body frame and sets up cabin body panel on the cabin body frame, the hatch door includes the hatch door frame and sets up the hatch door panel on the hatch door frame, actuating mechanism sets up between the top of cabin body frame and the hatch door frame, actuating mechanism includes the push rod, the one end of push rod is connected the top of cabin body frame, the other end of push rod is connected on the hatch door frame, the push rod is used for the drive hatch door horizontal migration opens the top space that unmanned aerial vehicle took off fast. The push rod is an electric push rod.
According to some preferred implementation aspects of the invention, the driving mechanism further comprises an adapter fixed on the door frame, a fixed seat fixed on the end of the push rod, and a pin for fixing the fixed seat on the end of the push rod. That is, the two ends of one push rod are connected with the fixing seats through pins, one of the fixing seats is fixed on the top of the cabin body frame, the other fixing seat is fixed on the cabin door frame through the adapter, and in some embodiments, the adapter is fixed on one side of the cabin door frame far away from the cabin body.
According to some preferred implementation aspects of the invention, the adapter comprises a bottom plate and two opposite side plates, wherein one side of the bottom plate is fixedly connected with the fixed seat, and two side parts of the other side of the bottom plate are fixed on the door frame.
According to some preferred aspects of the invention, the door frame comprises transverse beams, longitudinal beams and vertical beams arranged perpendicular to each other, the longitudinal beams extending in the same direction as the door moves. Through mutually perpendicular's crossbeam, longeron and founding the roof beam, guaranteed the whole steadiness of frame when control hatch door frame weight is in order conveniently to open and shut.
According to some preferred aspects of the invention, a guiding mechanism for guiding the movement of the door is included, the guiding mechanism comprising a sliding rail, one side of the sliding rail being mounted on the cabin frame and the other side of the sliding rail being mounted on the door frame, the sliding rail comprising a plurality of sections of guide rails cooperating with each other. The guide mechanism formed by the guide rails is arranged to limit the movement of the cabin door, so that the stability of the cabin door during opening and closing is ensured, and the cabin door is opened and closed along the horizontal direction.
According to some preferred aspects of the invention, the sliding track comprises a first section of guide rail, a second section of guide rail and a third section of guide rail which are matched with each other, the second section of guide rail is positioned between the first section of guide rail and the third section of guide rail, one of the first section of guide rail or the third section of guide rail is installed on the cabin door frame, and the rest of the first section of guide rail or the third section of guide rail is installed on the cabin door frame.
According to some preferred embodiment aspects of the present invention, the cross member comprises a first cross member, a second cross member and a third cross member, the first cross member and the second cross member are located in the same horizontal plane, and the second cross member and the third cross member are located in the same vertical plane; the longitudinal beam is positioned between the first cross beam and the second cross beam and is vertical to the cross beams; the vertical beam is positioned at the connecting part of the cross beam and the longitudinal beam. The adapter is arranged on the vertical beam far away from one side of the cabin body. In some embodiments, a reinforcing beam is further provided on the door frame, the reinforcing beam comprising a reinforcing upright beam and a reinforcing longitudinal beam, the reinforcing upright beam being provided between the second cross beam and the third cross beam, and the reinforcing longitudinal beam being provided at an intermediate position between the two longitudinal beams.
According to some preferred implementation aspects of the invention, a mounting beam is further arranged between two vertical beams below the same longitudinal beam, the mounting beam is arranged in the same direction as the longitudinal beam, and the mounting beam is used for mounting the sliding rail. The distance between the slide rail and the push rod is close to each other, so that the consistency and the synchronism of the movement of the slide rail and the push rod are ensured, and the stability of the opening and closing of the cabin door is ensured.
According to some preferred aspects of the invention, the uprights extend down to coincide with the top part of the cabin frame for sealing, while limiting the position of the cabin door when it is closed.
According to some preferred embodiments of the present invention, the top of the cabin body is provided with two opposite door frames and corresponding door panels, the two sides of each door frame are provided with the driving mechanism and the guiding mechanism, and the two door frames move to realize the opening and closing of the doors.
The invention also provides a horizontal cabin opening and closing method of the unmanned cabin, which comprises the following steps: starting a driving mechanism, wherein a push rod in the driving mechanism pushes the cabin door to move horizontally outwards relative to the cabin body, so that cabin opening is realized; after the unmanned aerial vehicle falls into the cabin body, the push rod in the driving mechanism retracts to drive the cabin door to move horizontally inwards relative to the cabin body, so that the cabin is closed. The push rod is arranged between the cabin body frame and the cabin door frame, so that the horizontal opening and closing of the cabin door can be realized.
Due to the adoption of the technical scheme, compared with the prior art, the invention has the beneficial effects that: according to the unmanned engine room, the push rod is arranged between the cabin body frame and the cabin door frame, so that the cabin door can be horizontally opened and closed, and the unmanned engine room is simple in integral composition structure, low in cost and good in stability.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
FIG. 1 is a perspective view of an unmanned cabin closing in the preferred embodiment of the present invention;
FIG. 2 is a perspective view of an unmanned aircraft cabin in a preferred embodiment of the invention;
FIG. 3 is a schematic perspective view of the unmanned aircraft cabin with a cabin door panel removed during cabin opening according to the preferred embodiment of the invention;
FIG. 4 is an enlarged view of a portion of FIG. 3;
FIG. 5 is a schematic structural diagram of a guiding mechanism and a driving mechanism of the unmanned aerial vehicle cabin in the preferred embodiment of the invention;
in the drawings: the cabin comprises a cabin body-1, a cabin door-2, a driving mechanism-3, a push rod-31, an adapter seat-32, a fixed seat-33, a guide mechanism-4, a first section of guide rail-41, a second section of guide rail-42, a third section of guide rail-43, a cabin body frame-51, a cabin body panel-52, a cabin door frame-61, a cabin door panel-62, a longitudinal beam-71, a vertical beam-72, a mounting beam-73, a first cross beam-81, a second cross beam-82, a third cross beam-83, a reinforced vertical beam-91 and a reinforced longitudinal beam-92.
Detailed Description
In order to make those skilled in the art better understand the technical solution of the present invention, the technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the drawings in the embodiment of the present invention, and it is obvious that the described embodiment is only a part of the embodiment of the present invention, and not a whole embodiment. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example one
As shown in fig. 1 to 5, the unmanned aerial vehicle cabin in the present embodiment includes a cabin body 1, a cabin door 2 located above the cabin body 1, a driving mechanism 3 for driving the cabin door 2 to move relative to the cabin body 1, and a guide mechanism 4 for guiding the movement of the cabin door 2. The cabin 1 includes a cabin frame 51 and a cabin panel 52 disposed on the cabin frame 51, and the hatch 2 includes a hatch frame 61 and a hatch panel 62 disposed on the hatch frame 61. In this embodiment, two opposite door frames 61 and corresponding door panels 62 are disposed at the top of the cabin body 1, a driving mechanism 3 and a guiding mechanism 4 are disposed on both sides of each door frame 61, and the two door frames 61 move to open and close the doors 2. The two door panels 62 have their top plates inclined, with the end closer to each other being higher in height and the end farther from each other being lower in height.
As shown in fig. 2 to 5, the driving mechanism 3 is disposed between the top of the cabin frame 51 and the cabin door frame 61, the driving mechanism 3 includes a push rod 31, an adapter 32 fixed on the cabin door frame 61, a fixing seat 33 fixed on the end of the push rod 31, and a pin for fixing the fixing seat 33 on the end of the push rod 31, one end of the push rod 31 is connected to the top of the cabin frame 51, the other end of the push rod 31 is connected to the cabin door frame 61, and the push rod 31 is used for driving the horizontal movement of the cabin door 2. The push rod 31 in the present embodiment is an electric push rod 31. As shown in fig. 3 to 5, the two end portions of one push rod 31 are connected to the fixing seats 33 through pins, one of the fixing seats 33 is fixed to the top of the cabin frame 51, the other fixing seat 33 is fixed to the cabin door frame 61 through the adapter 32, and the adapter 32 is fixed to one side of the cabin door frame 61 away from the cabin 1.
As shown in fig. 5, the guiding mechanism 4 includes a sliding rail, the sliding rail includes a first section of guide rail 41, a second section of guide rail 42 and a third section of guide rail 43, the first section of guide rail 41 is mounted on the cabin frame 51, the second section of guide rail 42 is located between the first section of guide rail 41 and the third section of guide rail 43, and the third section of guide rail 43 is mounted on the cabin door frame 61. One side and the cabin body frame 51 of slide rail are connected, and the opposite side and the hatch door frame 61 of slide rail are connected, and through setting up guiding mechanism 4 that a plurality of guide rails formed, carry on spacingly to the removal of hatch door 2, stability when having guaranteed hatch door 2 to open and shut along the horizontal direction for hatch door 2.
As shown in fig. 3 and 4, the door frame 61 comprises transverse beams, longitudinal beams 71, vertical beams 72, reinforcing beams and mounting beams 73 for mounting sliding rails, which are arranged perpendicular to each other, and the longitudinal beams 71 extend in the same direction as the moving direction of the door 2. By means of the mutually perpendicular cross beams, longitudinal beams 71 and uprights 72 the overall stability of the door frame 61 is ensured while controlling the weight of the frame to facilitate opening and closing.
Specifically, the cross beams in this embodiment include a first cross beam 81, a second cross beam 82, and a third cross beam 83, where the first cross beam 81 and the second cross beam 82 are located in the same horizontal plane, and the second cross beam 82 and the third cross beam 83 are located in the same vertical plane; the longitudinal beam 71 is located between the first cross beam 81 and the second cross beam 82 and perpendicular to the cross beams; the vertical beams 72 are located at the junction of the cross beams and the longitudinal beams 71. The adapter 32 is mounted on an upright beam 72 on the side remote from the cabin 1. The reinforcing beam includes a reinforcing upright beam 91 and a reinforcing longitudinal beam 92, the reinforcing upright beam 91 is disposed at an intermediate position between the second cross beam 82 and the third cross beam 83, and the reinforcing longitudinal beam 92 is disposed at an intermediate position between the two longitudinal beams 71. The mounting beam 73 is positioned between the two vertical beams 72 below the same longitudinal beam 71, and the mounting beam 73 and the longitudinal beam 71 are arranged in the same direction. The distance between the sliding rail and the push rod 31 is close to each other, so that the consistency and the synchronism of the movement of the sliding rail and the push rod 31 are ensured, and the stability of the opening and closing of the cabin door 2 is ensured. As shown in fig. 3 and 4, the uprights 72 in this embodiment extend downwardly to coincide with the top part of the cabin frame 51 for sealing purposes, while limiting the position of the door 2 when it is closed.
To further enhance the stability of the door frame 61 and the smoothness of the opening of the door 2, two sets of uprights 72, two in each case, are provided in this embodiment between the two ends of the second cross member 82 and the third cross member 83. Meanwhile, the adapter 32 in this embodiment includes a bottom plate and two opposite side plates, wherein one side of the bottom plate is fixedly connected to the fixing seat 33, and two side portions of the other side of the bottom plate are respectively fixed to the two vertical beams 72 in one set. The two vertical plates on the bottom plate are positioned between the two vertical beams 72 in one group, and the outer distance of the two side plates is the same as the inner distance of the two vertical beams 72 in one group so as to fix the side plates on the vertical beams 72, as shown in fig. 4 and 5. Through such setting, on the one hand make the power vertical action of push rod on the bottom plate of adapter, strengthened the stability when the hatch door horizontal opening closes, on the other hand has strengthened the connection of each part in the frame, has promoted the steadiness.
Example two
The present embodiment provides a method for horizontally opening and closing an unmanned cabin according to embodiment 1, including the steps of: starting the driving mechanism 3, and pushing a push rod 31 in the driving mechanism 3 to push the cabin door 2 to move horizontally outwards relative to the cabin body 1 so as to open the cabin; after the unmanned aerial vehicle falls into the cabin body 1, the push rod 31 in the driving mechanism 3 retracts to drive the cabin door 2 to move horizontally inwards relative to the cabin body 1, and cabin closing is achieved. By providing the push rod 31 between the cabin body frame 51 and the cabin door frame 61, the horizontal opening and closing of the cabin door 2 can be achieved.
In this embodiment, the method for horizontally opening and closing the unmanned cabin specifically includes the following steps:
1) when the unmanned aerial vehicle outside the cabin needs to fall into the cabin body 1, or the unmanned aerial vehicle in the cabin body 1 needs to fly out of the cabin body 1, the driving mechanism 3 is started, the push rod 31 extends outwards, the cabin door frame 61 is pushed to move outwards, and the cabin door 2 is driven to move outwards relative to the cabin body 1 horizontally, so that the cabin opening is realized.
2) When the unmanned aerial vehicle outside the cabin completely falls into the cabin body 1, or the unmanned aerial vehicle inside the cabin body 1 completely flies out of the cabin body 1, the driving mechanism 3 is started again, the push rod 31 retracts inwards, the cabin door frame 61 is driven to move outwards, and then the cabin door 2 is driven to move inwards relative to the horizontal direction of the cabin body 1, so that the cabin closing is realized.
The horizontal of hatch door opens and shuts not only can increase the whole steadiness of device and with the stability of the process of opening and shutting, and for other modes of opening and shutting, the level opens and shuts and can effectively reduce the latency of opening and shutting and the space that the opening and shutting will occupy.
The above embodiments are merely illustrative of the technical concept and features of the present invention, and the purpose thereof is to enable those skilled in the art to understand the content of the present invention and implement the invention, and not to limit the scope of the invention, and all equivalent changes or modifications made according to the spirit of the present invention should be covered by the scope of the present invention.
Claims (10)
1. An unmanned cabin comprises a cabin body, a cabin door positioned above the cabin body and a driving mechanism for driving the cabin door to move relative to the cabin body, it is characterized in that the cabin comprises a cabin frame and a cabin panel arranged on the cabin frame, the hatch comprises a hatch frame and a hatch panel arranged on the hatch frame, the driving mechanism is arranged between the top of the cabin frame and the hatch frame, the driving mechanism comprises a push rod, an adapter fixed on the cabin door frame, a fixed seat fixed at the end part of the push rod and a pin used for fixing the fixed seat at the end part of the push rod, one end of the push rod is connected to the top of the cabin body frame, the other end of the push rod is connected to the cabin door frame, and the push rod is used for driving the cabin door to move horizontally.
2. The unmanned aerial vehicle cabin of claim 1, wherein the adapter comprises a bottom plate and two opposite side plates, wherein one side of the bottom plate is fixedly connected with the fixing seat, and two side portions of the other side of the bottom plate are fixed on the cabin door frame.
3. Unmanned nacelle according to claim 1, wherein the door frame comprises transverse beams, longitudinal beams and vertical beams arranged perpendicular to each other, the longitudinal beams extending in the same direction as the door is moved.
4. The unmanned aerial vehicle of claim 3, comprising a guide mechanism for guiding movement of the door, the guide mechanism comprising a slide rail, one side of the slide rail being mounted to the cabin frame and the other side of the slide rail being mounted to the door frame.
5. The unmanned aerial vehicle of claim 4, wherein the rail comprises a first section of rail, a second section of rail, and a third section of rail that mate with each other, the second section of rail being positioned between the first section of rail and the third section of rail, one of the first section of rail or the third section of rail being mounted to the cabin frame, the remaining one of the first section of rail or the third section of rail being mounted to the cabin door frame.
6. The unmanned nacelle of claim 4, wherein the cross-beams comprise a first cross-beam, a second cross-beam, and a third cross-beam, the first and second cross-beams lying in a same horizontal plane, the second and third cross-beams lying in a same vertical plane; the longitudinal beam is positioned between the first cross beam and the second cross beam and is vertical to the cross beams; the vertical beam is positioned at the connecting part of the cross beam and the longitudinal beam.
7. The unmanned aerial vehicle cabin of claim 6, wherein a mounting beam is further arranged between two vertical beams below the same longitudinal beam, the mounting beam and the longitudinal beam are arranged in the same direction, and the mounting beam is used for mounting the sliding rail.
8. The unmanned nacelle of claim 6, wherein the upright beams extend downwardly to coincide with a top portion of the nacelle frame for sealing.
9. The unmanned aerial vehicle of claim 4, wherein the top of the cabin body is provided with two opposite cabin door frames and corresponding cabin door panels, the two sides of each cabin door frame are provided with the driving mechanism and the guiding mechanism, and the two cabin door frames move to realize the opening and closing of the cabin doors.
10. A method for horizontally opening and closing an unmanned aerial vehicle cabin according to any one of claims 1 to 9, comprising the steps of: starting a driving mechanism, wherein a push rod in the driving mechanism pushes the cabin door to move horizontally outwards relative to the cabin body, so that cabin opening is realized; after the unmanned aerial vehicle falls into the cabin body, the push rod in the driving mechanism retracts to drive the cabin door to move horizontally inwards relative to the cabin body, so that the cabin is closed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110527473.7A CN113202372A (en) | 2021-05-14 | 2021-05-14 | Unmanned cabin and cabin opening and closing method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110527473.7A CN113202372A (en) | 2021-05-14 | 2021-05-14 | Unmanned cabin and cabin opening and closing method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113202372A true CN113202372A (en) | 2021-08-03 |
Family
ID=77031217
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110527473.7A Pending CN113202372A (en) | 2021-05-14 | 2021-05-14 | Unmanned cabin and cabin opening and closing method |
Country Status (1)
| Country | Link |
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| CN (1) | CN113202372A (en) |
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| CN110206469A (en) * | 2019-07-02 | 2019-09-06 | 中国核电工程有限公司 | A kind of shield gasket door and control method |
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| KR102175596B1 (en) * | 2020-08-07 | 2020-11-09 | 주식회사 새마 | Unmanned Mobile Drone Self-charging Station and its Control Method |
| CN212172046U (en) * | 2020-04-09 | 2020-12-18 | 中科灵动航空科技成都有限公司 | Unmanned aerial vehicle transport vechicle cabin door system and unmanned aerial vehicle transport vechicle |
| CN212837300U (en) * | 2020-07-30 | 2021-03-30 | 深圳市华之翼科技有限公司 | Novel automatic cabin door opening and closing mechanism for unmanned airport |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180155032A1 (en) * | 2016-04-29 | 2018-06-07 | United Parcel Service Of America, Inc. | Methods for picking up a parcel via an unmanned aerial vehicle |
| CN207145212U (en) * | 2017-08-21 | 2018-03-27 | 奥龙汽车有限公司 | A kind of novel on-vehicle water pump installs pull platform |
| CN209586075U (en) * | 2018-10-26 | 2019-11-05 | 四川红帆特种设备工程有限公司 | A kind of more open type electric controlled doors |
| CN209938989U (en) * | 2019-02-27 | 2020-01-14 | 深圳洛可可工业设计有限公司 | Unmanned aerial vehicle space station |
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| CN212837300U (en) * | 2020-07-30 | 2021-03-30 | 深圳市华之翼科技有限公司 | Novel automatic cabin door opening and closing mechanism for unmanned airport |
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