CN112009691A - Article loading structure for unmanned aerial vehicle device - Google Patents
Article loading structure for unmanned aerial vehicle device Download PDFInfo
- Publication number
- CN112009691A CN112009691A CN202010929847.3A CN202010929847A CN112009691A CN 112009691 A CN112009691 A CN 112009691A CN 202010929847 A CN202010929847 A CN 202010929847A CN 112009691 A CN112009691 A CN 112009691A
- Authority
- CN
- China
- Prior art keywords
- frame
- unmanned aerial
- aerial vehicle
- vehicle device
- seat
- 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.)
- Withdrawn
Links
- 230000001681 protective effect Effects 0.000 claims abstract description 13
- 238000000034 method Methods 0.000 claims description 7
- 230000006872 improvement Effects 0.000 description 4
- 230000002146 bilateral effect Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses an article loading structure for an unmanned aerial vehicle device, which comprises a frame, a support block, a protective frame, a connecting column, a placing component, a side frame, a control switch and a power line.
Description
Technical Field
The invention relates to the related field of unmanned aerial vehicles, in particular to an article loading structure for an unmanned aerial vehicle device.
Background
The unmanned plane is called as an unmanned plane for short, and is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device; unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parachute-wing aircraft and the like; when being used for the goods delivery, install article delivery structure on the unmanned aerial vehicle usually and fix the goods.
The structure that prior art unmanned aerial vehicle device article loaded the structure is simple, and the size of putting the installation is adjusted to the size of inconvenient according to the big or small size of goods when reprinting article, makes article have great gap when reprinting, causes unmanned aerial vehicle to rock at unmanned aerial vehicle flight in-process easily, has certain potential safety hazard.
Disclosure of Invention
Accordingly, to address the above-described deficiencies, the present invention provides an article loading structure for an unmanned aerial vehicle device.
The invention is realized in such a way that an article loading structure for an unmanned aerial vehicle device is constructed, the device comprises a frame, support blocks, a protective frame, connecting columns, a placing component, side frames, a control switch and a power line, wherein the support blocks are vertically fixed on the left side and the right side of the bottom of the frame, the bottom of each support block is fixed with the protective frame, the connecting columns are vertically fixed on four ends of the top of the frame, the side frame is fixedly connected on the left side of the top of the frame, the control switch is arranged on the right front side of the bottom of the frame, the power line is arranged on the right side of the front part of the frame, the placing component is fixedly connected to the inner side of the frame, the placing component comprises a rectangular frame seat, a cover plate, a power structure, a sliding chute and a clamping frame, the power structure is fixedly connected on the left side of the rectangular, the clamping frame penetrates through the inner side of the sliding groove, and the bottom of the clamping frame is connected with the power structure.
Preferably, the side frame comprises a first upright column, a cross rod and a second upright column, the first upright column is fixedly connected to the left rear side of the top of the frame, the top side of the front portion of the first upright column is fixed to the second upright column through the cross rod, and the bottom of the second upright column is fixed to the left front side of the top of the frame.
Preferably, the protection frame is provided with two to two protection frames are arranged in the middle of the frame in a bilateral symmetry mode, and the front side and the rear side of the protection frame are provided with chamfers inclining outwards.
Preferably, the power structure includes rectangle seat, mount pad, servo motor, the body of rod, threaded rod and folding leg, the rectangle seat right flank is fixed mutually with the rectangle frame seat, the inboard middle part of rectangle seat leads to the mount pad and transversely estimates fixedly connected with servo motor, servo motor right side output is connected with the body of rod, body of rod right-hand member face integrated into one piece threaded rod, threaded rod top right side is connected with the folding leg.
Preferably, the middle side of the right side of the rectangular seat is provided with a round opening, and the left side of the rod body penetrates through the inner side of the round opening and is rotatably connected with the round opening.
Preferably, the number of the clamping frames is four, and the four clamping frames penetrate through the inner side of the sliding groove and are in transverse sliding fit with the sliding groove.
Preferably, the clamping frame comprises a rear vertical rod, a connecting rod frame and a front vertical rod, the top side of the front part of the rear vertical rod is fixed with the front vertical rod through the connecting rod frame, and the bottoms of the rear vertical rod and the front vertical rod are connected with the folding frame.
Preferably, the folding leg includes support frame, internal thread seat, preceding crossbeams and back crossbeams, the inboard middle part of support frame rotates with preceding crossbeams and back crossbeams to be connected in preceding crossbeams and back crossbeams left side, preceding crossbeams top front side is connected with preceding pole setting, preceding pole setting top rear side is connected with the back pole setting.
Preferably, the internal thread seat and the threaded rod are on the same horizontal plane, and the threaded rod penetrates through the inner side of the internal thread seat to be matched with the internal thread seat.
Preferably, the material used for the front cross frame and the rear cross frame is stainless steel.
Preferably, the rear upright stanchion, the connecting pole frame and the front upright stanchion are all made of aluminum alloy materials.
The invention has the following advantages: the present invention provides an article loading structure for an unmanned aerial vehicle device by improvement, compared with the same type of equipment, having the following improvements:
the method has the advantages that: the invention relates to an article loading structure for an unmanned aerial vehicle device, which is characterized in that a placing component is optimally arranged, a servo motor is used as a power source, a rod body drives a threaded rod to rotate, the threaded rod drives a support frame to move in the horizontal direction through matching with an internal thread seat, so that the support frame drives a front cross frame and a rear cross frame to be mutually unfolded to enable four clamping frames to transversely slide in a sliding groove, the distance between the four clamping frames is further adjusted, so that the goods can be installed and limited according to the size of different goods, the problem that the unmanned aerial vehicle flies unstably due to the shaking of the goods is avoided, the use safety is improved, the problem that the article loading structure of the unmanned aerial vehicle device in the prior art is simple in structure, the size of the installation and the placement is not conveniently adjusted according to the size of the goods during transferring of the goods, a larger gap exists in the goods during transferring, and the unmanned aerial vehicle is, has certain potential safety hazard.
The method has the advantages that: according to the article loading structure for the unmanned aerial vehicle device, the two protection frames are symmetrically arranged at the left and right sides of the middle of the frame, the chamfers inclining towards the outside are arranged on the front side and the rear side of each protection frame, so that an unmanned aerial vehicle can be protected when landing, the round opening is formed in the right side of the rectangular seat, the left side of the rod body penetrates through the inner side of the round opening and is rotatably connected with the rod body, and the rod body can be supported and rotated conveniently.
The method has the advantages that: the four clamping frames penetrate through the inner side of the sliding groove and are in sliding fit with the sliding groove in the transverse direction, the distance between the clamping frames can be adjusted conveniently according to the size of an object, the object is placed conveniently, the internal thread seat and the threaded rod are on the same horizontal plane, the threaded rod penetrates through the inner side of the internal thread seat and is matched with the internal thread seat, and the internal thread seat is driven to move in the horizontal direction conveniently.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic illustration of the sideframe construction of the present invention;
FIG. 3 is a schematic structural view of a placement module of the present invention;
FIG. 4 is a schematic structural view of the power structure of the present invention;
fig. 5 is a schematic structural view of the folding leg of the present invention.
Wherein: the device comprises a frame-1, a support block-2, a protective frame-3, a connecting column-4, a placing component-5, a side frame-6, a control switch-7, a power line-8, a rectangular frame seat-51, a cover plate-52, a power structure-53, a chute-54, a clamping frame-55, a first upright post-61, a cross bar-62, a second upright post-63, a rectangular seat-531, a mounting seat-532, a servo motor-533, a rod body-534, a threaded rod-535, a folding frame-536, a rear upright post-551, a connecting rod frame-552, a front upright post-553, a support frame-5361, an internal threaded seat-5362, a front cross frame-5363 and a rear cross frame-5364.
Detailed Description
The present invention will be described in detail with reference to fig. 1 to 5, and the technical solutions in the embodiments of the present invention will be clearly and completely described, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. 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.
The first embodiment is as follows:
referring to fig. 1 and 2, the present invention relates to an article loading structure for an unmanned aerial vehicle device, which comprises a frame 1, support blocks 2, a protective frame 3, a connecting column 4, a placing component 5, side frames 6, a control switch 7 and a power cord 8, wherein the left and right sides of the bottom of the frame 1 are vertically fixed with the support blocks 2, the bottoms of the support blocks 2 are fixed with the protective frame 3, four ends of the top of the frame 1 are vertically fixed with the connecting column 4, the left side of the top of the frame 1 is fixedly connected with the side frame 6, the right front side of the bottom of the frame 1 is provided with the control switch 7, the power cord 8 is arranged on the right side of the front of the frame 1, the placing component 5 is fixedly connected to the inner side of the frame 1, the side frames 6 comprise a first upright column 61, a cross bar 62 and a second upright column 63, the first upright column 61 is fixedly connected to the left and rear side of the top of the frame 1, is convenient for protecting the object.
Referring to fig. 3, according to the article loading structure for the unmanned aerial vehicle device of the present invention, the placing assembly 5 includes a rectangular frame base 51, a cover plate 52, a power structure 53, a sliding groove 54 and a clamping frame 55, the left side of the rectangular frame base 51 is fixedly connected with the power structure 53, four ends of the top of the power structure 53 are fixed to the cover plate 52 through bolts, the sliding groove 54 is disposed at the front and rear sides of the top of the rectangular frame base 51, the clamping frame 55 penetrates through the inner side of the sliding groove 54, and the bottom of the clamping frame 55 is connected to the power structure 53, the clamping frame 55 includes a rear vertical rod 551, a connecting rod frame 552 and a front vertical rod 553, the top side of the front portion of the rear vertical rod 551 is fixed to the front vertical rod 553 through the connecting rod frame 552, and the bottoms of the rear vertical rod 551 and the front vertical rod 553 are both connected to the folding frame 536, so as to.
Referring to fig. 4, according to the article loading structure for the unmanned aerial vehicle device of the present invention, the power structure 53 includes a rectangular base 531, a mounting base 532, a servo motor 533, a rod body 534, a threaded rod 535, and a folding rack 536, the right side of the rectangular base 531 is fixed to the rectangular frame base 51, the servo motor 533 is horizontally connected to the middle of the inner side of the rectangular base 531 through the mounting base 532, the right output end of the servo motor 533 is connected to the rod body 534, the threaded rod 535 is integrally formed on the right end surface of the rod body 534, the right side of the top of the threaded rod 535 is connected to the folding rack 536, and the servo motor 533 is used as a power source to control the threaded rod 535 to rotate to adjust the.
Referring to fig. 5, the folding rack 536 of the present invention includes a supporting frame 5361, an internal thread seat 5362, a front cross frame 5363 and a rear cross frame 5364, the internal thread seat 5362 is fixedly connected to the bottom of the supporting frame 5361, the middle of the inner side of the supporting frame 5361 is rotatably connected to the front cross frame 5363 and the rear cross frame 5364, the front side of the top of the front cross frame 5363 is connected to the front upright 553, the rear side of the top of the front upright 553 is connected to the rear upright 551, so as to adjust the positions of the front upright 553 and the rear upright 551.
Example two:
the invention relates to an article loading structure for an unmanned aerial vehicle device, two protective frames 3 are arranged, the two protective frames 3 are arranged in the middle of a frame 1 in a bilateral symmetry way, meanwhile, chamfers inclining towards the outside are arranged on the front side and the rear side of the protective frame 3, so that the unmanned aerial vehicle can conveniently protect objects when landing, a round opening is formed in the middle of the right part of the rectangular seat 531, the left side of the rod body 534 penetrates through the inner side of the round opening and is rotatably connected with the round opening, so that the rod body 534 can be conveniently supported and rotated, four clamping frames 55 are arranged, and the four clamping frames 55 penetrate through the inner side of the sliding chute 54 and are in sliding fit with the sliding chute in the transverse direction, so that the distance between the clamping frames can be adjusted conveniently according to the size of an object, the object can be placed conveniently, the internal thread seat 5362 and the threaded rod 535 are on the same horizontal plane, and the threaded rod 535 runs through the inner side of the internal threaded seat 5362 to be matched with the internal threaded seat 5362, so as to drive the internal threaded seat 5362 to move in the horizontal direction.
The invention provides an article loading structure for an unmanned aerial vehicle device through improvement, and the working principle is as follows;
firstly, the design is fixedly installed at the bottom of the unmanned aerial vehicle through a connecting column 4, and then a power line 8 is connected with a power supply inside the unmanned aerial vehicle to use the design;
secondly, according to the size of the article to be transferred, the user starts the servo motor 533 through the control switch 7, the servo motor 533 drives the rod body 534 to rotate after being started, the rod body 534 drives the threaded rod 535 to rotate, and the threaded rod 535 drives the support frame 5361 to move in the horizontal direction through matching with the internal thread seat 5362;
thirdly, the supporting frame 5361 moves to enable the front cross frame 5363 and the rear cross frame 5364 to be unfolded mutually to drive the four clamping frames 55 to slide transversely in the sliding grooves 54, so that the four connecting rod frames 552 are separated mutually under the action of the front upright 553 and the rear upright 551, and further the distance between the inner sides of the four connecting rod frames 552 is adjusted according to the size of goods;
fourthly, the articles to be loaded are respectively placed and fixed inside the four connecting rod racks 552.
The invention provides an article loading structure for an unmanned aerial vehicle device through improvement, a placing component 5 is optimally arranged, a servo motor 533 is used as a power source, a threaded rod 535 is driven to rotate through a rod body 534, the threaded rod 535 is driven to drive a support frame 5361 to move in the horizontal direction through matching with an internal threaded seat 5362, so that the support frame 5361 drives a front cross frame 5363 and a rear cross frame 5364 to mutually expand to enable four clamping frames 55 to transversely slide in a sliding groove 54, the distance between the four clamping frames 55 is further adjusted, so that the cargo can be installed and limited according to the sizes and sizes of different cargos, the problem that the unmanned aerial vehicle flies unstably due to cargo shaking is avoided, the use safety is improved, the problem that the structure of the article loading structure of the unmanned aerial vehicle device in the prior art is simple, the installation and placement sizes are not convenient to adjust according to the sizes and sizes of the cargos, the problem that the unmanned aerial vehicle is easy to shake in the flying process of the unmanned aerial vehicle and has certain potential safety hazard is caused because a large gap exists in the process of transferring articles; protect frame 3 to be provided with two, and two protect frame 3 and set up at frame 1 middle part bilateral symmetry, it all is provided with the chamfer to the lateral inclination to protect 3 front and back both sides of frame simultaneously, be convenient for protect article when unmanned aerial vehicle descends, rectangle seat 531 right part side is opened and is equipped with the round mouth, and body of rod 534 left side runs through the round mouth inboard and is connected rather than rotating, be convenient for support the rotation to body of rod 534, card frame 55 is provided with four altogether, and four card frames 55 all run through spout 54 inboard rather than transverse sliding fit, be convenient for adjust the distance between according to the size of article, be favorable to placing article, interior screw base 5362 and threaded rod 535 are on same horizontal plane, and threaded rod 535 runs through interior screw base 5362 inboard and cooperatees with it, be convenient for drive interior screw base 5362 and move on.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described, and the standard parts used in the present invention are all available on the market, the special-shaped parts can be customized according to the description and the accompanying drawings, the specific connection mode of each part adopts the conventional means of bolt and rivet, welding and the like mature in the prior art, the machinery, parts and equipment adopt the conventional type in the prior art, and the circuit connection adopts the conventional connection mode in the prior art, and the details are not described herein.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (10)
1. An article loading structure for an unmanned aerial vehicle device comprises a frame (1), support blocks (2), a protective frame (3), connecting columns (4), side frames (6), a control switch (7) and a power line (8), wherein the support blocks (2) are vertically fixed on the left side and the right side of the bottom of the frame (1), and the bottoms of the support blocks (2) are fixed with the protective frame (3);
the method is characterized in that: still including putting subassembly (5), it is inboard in frame (1) to place subassembly (5), it includes rectangle frame seat (51), cover plate (52), power structure (53), spout (54) and card frame (55) to place subassembly (5), rectangle frame seat (51) left side fixed connection has power structure (53), four ends in power structure (53) top are fixed mutually with cover plate (52) through the bolt, both sides around rectangle frame seat (51) top are seted up in spout (54), card frame (55) run through in spout (54) inboard to card frame (55) bottom is connected with power structure (53).
2. An article loading structure for an unmanned aerial vehicle device according to claim 1, wherein: four vertical spliced poles (4) of being fixed with in frame (1) top, frame (1) top left side fixedly connected with side bearer (6), frame (1) bottom right front side is provided with control switch (7), power cord (8) set up in frame (1) front portion right side.
3. An article loading structure for an unmanned aerial vehicle device according to claim 1, wherein: the side frame (6) comprises a first upright post (61), a cross rod (62) and a second upright post (63), the first upright post (61) is fixedly connected to the left rear side of the top of the frame (1), the top side of the front part of the first upright post (61) is fixed with the second upright post (63) through the cross rod (62), and the bottom of the second upright post (63) is fixed with the left front side of the top of the frame (1).
4. An article loading structure for an unmanned aerial vehicle device according to claim 1, wherein: the two protective frames (3) are arranged symmetrically in the left and right directions in the middle of the frame (1), and chamfers inclining towards the outside are arranged on the front side and the rear side of each protective frame (3).
5. An article loading structure for an unmanned aerial vehicle device according to claim 1, wherein: power structure (53) are including rectangle seat (531), mount pad (532), servo motor (533), the body of rod (534), threaded rod (535) and folding leg (536), rectangle seat (531) right flank is fixed mutually with rectangle frame seat (51), fixedly connected with servo motor (533) are transversely estimated to lead to mount pad (532) in the middle part of rectangle seat (531) inboard, servo motor (533) right side output is connected with the body of rod (534), the body of rod (534) right-hand member face integrated into one piece threaded rod (535), threaded rod (535) top right side is connected with folding leg (536).
6. An article loading structure for an unmanned aerial vehicle device according to claim 5, wherein: the middle side of the right part of the rectangular seat (531) is provided with a round opening, and the left side of the rod body (534) penetrates through the inner side of the round opening to be connected with the round opening in a rotating mode.
7. An article loading structure for an unmanned aerial vehicle device according to claim 1, wherein: the number of the clamping frames (55) is four, and the four clamping frames (55) penetrate through the inner side of the sliding groove (54) and are in transverse sliding fit with the sliding groove.
8. An article loading structure for an unmanned aerial vehicle device according to claim 1, wherein: the clamping frame (55) comprises a rear upright post (551), a connecting rod frame (552) and a front upright post (553), the top side of the front part of the rear upright post (551) is fixed with the front upright post (553) through the connecting rod frame (552), and the bottoms of the rear upright post (551) and the front upright post (553) are connected with the folding frame (536).
9. An article loading structure for an unmanned aerial vehicle device according to claim 5, wherein: the folding rack (536) comprises a support frame (5361), an internal thread seat (5362), a front cross rack (5363) and a rear cross rack (5364), wherein the internal thread seat (5362) is fixedly connected to the middle of the bottom of the support frame (5361), the middle of the inner side of the support frame (5361) is rotatably connected with the front cross rack (5363) and the rear cross rack (5364), the front side of the top of the front cross rack (5363) is connected with a front upright (553), and the rear side of the top of the front upright (553) is connected with a rear upright (551).
10. An article loading structure for an unmanned aerial vehicle device according to claim 9, wherein: the internal thread seat (5362) and the threaded rod (535) are on the same horizontal plane, and the threaded rod (535) penetrates through the inner side of the internal thread seat (5362) to be matched with the internal thread seat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010929847.3A CN112009691A (en) | 2020-09-07 | 2020-09-07 | Article loading structure for unmanned aerial vehicle device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010929847.3A CN112009691A (en) | 2020-09-07 | 2020-09-07 | Article loading structure for unmanned aerial vehicle device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112009691A true CN112009691A (en) | 2020-12-01 |
Family
ID=73515488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010929847.3A Withdrawn CN112009691A (en) | 2020-09-07 | 2020-09-07 | Article loading structure for unmanned aerial vehicle device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112009691A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112758330A (en) * | 2020-12-25 | 2021-05-07 | 安徽翼讯飞行安全技术有限公司 | Unmanned aerial vehicle commodity circulation goods linkage of high group spare |
| CN113002922A (en) * | 2021-03-10 | 2021-06-22 | 缪雷 | Transportation layer board equipment for large-scale aviation aircraft |
-
2020
- 2020-09-07 CN CN202010929847.3A patent/CN112009691A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112758330A (en) * | 2020-12-25 | 2021-05-07 | 安徽翼讯飞行安全技术有限公司 | Unmanned aerial vehicle commodity circulation goods linkage of high group spare |
| CN113002922A (en) * | 2021-03-10 | 2021-06-22 | 缪雷 | Transportation layer board equipment for large-scale aviation aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN112009691A (en) | Article loading structure for unmanned aerial vehicle device | |
| US6494404B1 (en) | Passenger airplane container system | |
| CN105173100A (en) | Unmanned plane cloud deck and unmanned plane | |
| CN206466156U (en) | The nose-gear load mechanism of duct aircraft | |
| CN206984414U (en) | A kind of deployable and collapsible fixed-wing unmanned plane twin shaft head | |
| CN204686401U (en) | Main driving air bag screw automatic tightening assembly bench | |
| CN108832258A (en) | A kind of folding device of the motor-driven large-scale antenna front radar of vehicle-mounted height | |
| US5163806A (en) | Airline food transportation system | |
| CN204264319U (en) | Hanging rack of bike | |
| CN108545005A (en) | A kind of logistics management courier packages distribute vehicle | |
| CN112520040A (en) | Unmanned aerial vehicle and unmanned aerial vehicle system for logistics transportation | |
| CN207450273U (en) | A kind of collision prevention of unmanned plane during flying device | |
| CN213535142U (en) | Portable unmanned aerial vehicle berths platform device | |
| CN208053637U (en) | A kind of logistics unmanned plane | |
| CN215554168U (en) | Carry thing unmanned aerial vehicle of article is lightly got to convenience | |
| CN110979727A (en) | Aircraft tail cone transportation bracket | |
| CN210503209U (en) | Civil aviation passenger plane safety seat | |
| CN115973416B (en) | Heavy-load anti-interference unmanned aerial vehicle | |
| CN202225803U (en) | Wheelchair accommodating device | |
| CN110963066A (en) | Splicing type luggage consigning device for airport | |
| CN220391536U (en) | Unmanned aerial vehicle carries detection device | |
| CN210212773U (en) | Unmanned aerial vehicle and delivery system | |
| CN220762602U (en) | Material rack for storing automobile spare parts | |
| CN219989500U (en) | Multifunctional intelligent unmanned aerial vehicle | |
| CN217199494U (en) | Rudder packing box |
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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20201201 |
|
| WW01 | Invention patent application withdrawn after publication |