CN109110133A - A kind of plural serial stage shipping unmanned aerial vehicle body - Google Patents
A kind of plural serial stage shipping unmanned aerial vehicle body Download PDFInfo
- Publication number
- CN109110133A CN109110133A CN201811045474.2A CN201811045474A CN109110133A CN 109110133 A CN109110133 A CN 109110133A CN 201811045474 A CN201811045474 A CN 201811045474A CN 109110133 A CN109110133 A CN 109110133A
- Authority
- CN
- China
- Prior art keywords
- control room
- power compartment
- cargo chamber
- aerial vehicle
- unmanned aerial
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Abstract
The present invention relates to a kind of plural serial stage shipping unmanned aerial vehicle bodies, including control room, power compartment, cargo chamber and positioning mechanism, control room, power compartment and cargo chamber are airtight cavity structure, wherein control room, the series connection of power compartment, wherein control room, power compartment rear end are connected with each other by positioning mechanism, control room, power compartment lower end surface pass through positioning mechanism respectively and cargo chamber upper surface is connected with each other, and cargo chamber includes bearing keel, directive slide track, carrying boxboard and positioning pin.One aspect of the present invention can effectively meet the needs of the normal shipping carrying operation of unmanned machine equipment; on the other hand it can effectively realize; it is required according to transport type of goods, structure etc.; cargo component is adjusted flexibly; greatly improve flexibility, convenience and the versatility of freight operation; to improve the reliability of unmanned plane freight operation, and reduce operating cost.
Description
Technical field
The present invention relates to a kind of unmanned aerial vehicle bodies, are exactly a kind of plural serial stage shipping unmanned aerial vehicle bodies.
Background technique
Carried and transported is carried out to cargo using unmanned plane, is one of the key areas of current unmanned plane equipment application, but
It is found in actual use, for current unmanned machine equipment when carrying out freight operation, the airframe structure for bearing goods is often
It is relatively fixed, although the needs of freight operation can be met to a certain degree, often easily due to the features such as cargo size, structure
Fuselage is caused effectively not to be loaded operation to cargo, to seriously affect the flexibility of unmanned plane freight operation just
Victory, while also resulting in when carrying out freight operation using unmanned plane, it generally requires to be equipped with a variety of different types of structure fuselages
Unmanned plane to meet the needs of freight operation, to also lead to unmanned plane freight operation, the cost is relatively high, therefore is directed to
This status, there is an urgent need to develop a kind of completely new unmanned aerial vehicle body structures, to meet the needs of actual use.
Summary of the invention
In view of the shortcomings of the prior art, the present invention provides a kind of plural serial stage shipping unmanned aerial vehicle body, the invention
Structure is simple, flexible and convenient to use, and versatility is good, and bearing capacity is strong, on the one hand can effectively meet the normal shipping of unmanned machine equipment
The needs for carrying operation, on the other hand can effectively realize, required according to transport type of goods, structure etc., cargo hold knot is adjusted flexibly
Structure greatly improves flexibility, convenience and the versatility of freight operation, to improve the reliable of unmanned plane freight operation
Property, and reduce operating cost.
To achieve the goals above, the present invention is to realize by the following technical solutions:
A kind of plural serial stage shipping unmanned aerial vehicle body, including control room, power compartment, cargo chamber and positioning mechanism, control
Room, power compartment and cargo chamber processed are airtight cavity structure, wherein control room, the series connection of power compartment, and are located at shipping
Right above room, control room, the lower end of power compartment and rear end are evenly distributed with several positioning mechanisms, cargo chamber upper surface, lower end surface, preceding
End face and rear end face are all provided at least four location structures, and wherein control room, power compartment rear end are mutually interconnected by positioning mechanism
It connects, and sets width between control room, power compartment rear end face as 1-10 millimeters of external series gap, under control room, power compartment
End face is distributed within the scope of same plane, and horizontal by 0 ° -60 ° angles, control room, power compartment lower end surface difference
It is connected with each other by positioning mechanism and cargo chamber upper surface, cargo chamber at least two, passes through localization machine between two neighboring cargo chamber
Structure is connected with each other, and cargo chamber includes bearing keel, directive slide track, carrying boxboard and positioning pin, and bearing keel is open column shape frame
Frame structure, directive slide track is several, is separately mounted to bearing keel the inner surface and the outer surface, and carrying boxboard is distinguished by directive slide track
It is connect with bearing keel the inner surface and the outer surface, and constitutes airtight cavity structure, bearing keel outer surface and interior with bearing keel
The bearing box spacing between plates on surface is 1.1-2.5 times of bearing keel height, and positioning pin is several, is evenly arranged on directive slide track, institute
It is connected with each other between the directive slide track stated and carrying boxboard by positioning pin.
Further, elastic insert is set in the external series gap.
Further, the positioning mechanism is any in electromagnetically body, electromagnetism pin, hanging ring, claw, hanging buckle and sliding rail
One or more share.
Further, the cargo chamber upper surface and lower end surface are all provided at least one traction rope, and the cargo chamber is logical
Traction rope is crossed to be connected with each other with control room adjacent thereto, power compartment and cargo chamber respectively.
Further, the traction rope end is connected with each other by rolling-up mechanism and shipping outdoor face.
Further, mutual by several elastic cushion blocks between the carrying boxboard of described bearing keel the inner surface and the outer surface
Connection.
Further, the directive slide track is hinged with bearing keel outer surface.
The configuration of the present invention is simple, flexible and convenient to use, versatility is good, and bearing capacity is strong, on the one hand can effectively meet nobody
The needs of the normal shipping carrying operation of machine equipment, on the other hand can effectively realize, be required according to transport type of goods, structure etc.,
Cargo component is adjusted flexibly, greatly improves flexibility, convenience and the versatility of freight operation, to improve unmanned plane goods
The reliability of industry is operated, and reduces operating cost.
Detailed description of the invention
The following describes the present invention in detail with reference to the accompanying drawings and specific embodiments.
Fig. 1 is schematic structural view of the invention；
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to
Specific embodiment, the present invention is further explained.
A kind of plural serial stage shipping unmanned aerial vehicle body as described in Figure 1, including control room 1, power compartment 2, cargo chamber 3
And positioning mechanism 4, control room 1, power compartment 2 and cargo chamber 3 are airtight cavity structure, wherein control room 1, power carry
Room 2 is connected, and is located at right above cargo chamber 3, and control room 1, the lower end of power compartment 2 and rear end are evenly distributed with several positioning mechanisms 4,
3 upper surface of cargo chamber, lower end surface, front end face and rear end face are all provided at least four location structures 4, wherein control room 1, power carrying
2 rear end of room is connected with each other by positioning mechanism 4, and sets width between control room 1,2 rear end face of power compartment as 1-10 millimeters
External series gap 5, control room 1,2 lower end surface of power compartment are distributed within the scope of same plane, and are pressed from both sides horizontal by 0 ° -60 °
Angle, control room 1,2 lower end surface of power compartment pass through positioning mechanism 4 respectively and 3 upper surface of cargo chamber is connected with each other, cargo chamber 3
At least two, it is connected with each other by positioning mechanism 4 between two neighboring cargo chamber 3.
In the present embodiment, the cargo chamber 3 includes bearing keel 31, directive slide track 32, carrying boxboard 34 and positioning pin
33, bearing keel 31 is open column shape frame structure, and directive slide track 32 is several, is separately mounted to 31 inner surface of bearing keel and outer
Surface, carrying boxboard 34 is connect with 31 the inner surface and the outer surface of bearing keel respectively by directive slide track 32, and and bearing keel
Spacing is 31 height of bearing keel between the carrying boxboard 34 of 31 composition airtight cavity structures, 31 outer surface of bearing keel and inner surface
1.1-2.5 times, positioning pin 33 is several, is evenly arranged on directive slide track 32, the directive slide track 32 and carrying boxboard 34 between lead to
Cross the interconnection of positioning pin 33.
In the present embodiment, elastic insert 6 is set in the external series gap 5.
In the present embodiment, the positioning mechanism 4 is in electromagnetically body, electromagnetism pin, hanging ring, claw, hanging buckle and sliding rail
Any one or a few is shared.
In the present embodiment, 3 upper surface of cargo chamber and lower end surface are all provided at least one traction rope 7, the shipping
Room 3 is connected with each other with control room 1 adjacent thereto, power compartment 2 and cargo chamber 3 respectively by traction rope 7.
In the present embodiment, 7 end of traction rope is connected with each other by rolling-up mechanism 8 and 3 outer surface of cargo chamber.
In the present embodiment, pass through several elastic cushions between the carrying boxboard 34 of described 31 the inner surface and the outer surface of bearing keel
Block 9 is connected with each other.
In the present embodiment, the directive slide track 32 is hinged with 31 outer surface of bearing keel.
The present invention in specific implementation, first as needed divides control room, power compartment, cargo chamber and positioning mechanism
It does not carry out assembling and then completes control room, the installation positioning of power compartment, and the flight system that will be used to control unmanned plane first
System is installed in control room, and the power mechanism for driving unmanned plane during flying is installed in power compartment, is finally made according to shipping
Cargo chamber and control room, power compartment are carried out installation positioning, assembly of the invention can be completed by the needs of industry.
When carrying out freight operation, first according to article structure to be lifted determine cargo chamber specifically used quantity and each goods
It transports room and connection relationship is installed, be then attached each cargo chamber by positioning mechanism, can be as needed in connection, by each goods
Fortune room assemble on the direction being parallel to the horizontal plane and matches with the enterprising luggage in direction of horizontal plane, can also at the same with level
It assembles on the parallel direction in face and matches with the enterprising luggage in direction of horizontal plane, make to greatly improve cargo chamber installation
The flexibility of industry separately can be as needed in assembling process, the bearing box of contact surface position when connecting to two neighboring cargo chamber
Plate is removed, and is interconnected to realize between two neighboring cargo chamber, is improved the bearing capacity to cargo and is improved cargo space
The flexibility of adjustment to meet the needs of different cargo carrying transports, and greatly improves unmanned plane and carries out cargo transport
Flexibility and reliability.
The configuration of the present invention is simple, flexible and convenient to use, versatility is good, and bearing capacity is strong, on the one hand can effectively meet nobody
The needs of the normal shipping carrying operation of machine equipment, on the other hand can effectively realize, be required according to transport type of goods, structure etc.,
Cargo component is adjusted flexibly, greatly improves flexibility, convenience and the versatility of freight operation, to improve unmanned plane goods
The reliability of industry is operated, and reduces operating cost.
It should be understood by those skilled in the art that the present invention is not limited to the above embodiments.Above-described embodiment and explanation
It is merely illustrated the principles of the invention described in book.Without departing from the spirit and scope of the present invention, the present invention also has
Various changes and modifications.These changes and improvements all fall within the protetion scope of the claimed invention.The claimed scope of the invention
It is defined by the appending claims and its equivalent thereof.
Claims (7)
1. a kind of plural serial stage shipping unmanned aerial vehicle body, it is characterised in that: the plural serial stage fuselage shipping unmanned plane includes
Control room, power compartment, cargo chamber and positioning mechanism, the control room, power compartment and cargo chamber are closed chamber
Body structure, wherein the series connection of the control room, power compartment, and be located at right above cargo chamber, the control room, power are held
The lower end and rear end for carrying room are evenly distributed with several positioning mechanisms, and cargo chamber upper surface, lower end surface, front end face and the rear end face are all provided with
At least four location structures, wherein the control room, power compartment rear end are connected with each other by positioning mechanism, and described
Width is set between control room, power compartment rear end face as 1-10 millimeters of external series gap, the control room, power compartment
Lower end surface is distributed within the scope of same plane, and horizontal by 0 ° -60 ° angles, under the control room, power compartment
End face passes through positioning mechanism respectively and cargo chamber upper surface is connected with each other, the cargo chamber at least two, two neighboring shipping
It being connected with each other between room by positioning mechanism, the cargo chamber includes bearing keel, directive slide track, carries boxboard and positioning pin,
The bearing keel is open column shape frame structure, and the directive slide track is several, is separately mounted to bearing keel inner surface
And outer surface, the carrying boxboard are connect respectively by directive slide track with bearing keel the inner surface and the outer surface, and with carrying
The bearing box spacing between plates of keel composition airtight cavity structure, the bearing keel outer surface and inner surface is that bearing keel is high
1.1-2.5 times of degree, the positioning pin is several, is evenly arranged on directive slide track, leads between the directive slide track and carrying boxboard
Cross positioning pin interconnection.
2. a kind of plural serial stage shipping unmanned aerial vehicle body according to claim 1, it is characterised in that: the external series gap
Inside set elastic insert.
3. a kind of plural serial stage shipping unmanned aerial vehicle body according to claim 1, it is characterised in that: the positioning mechanism
For in electromagnetically body, electromagnetism pin, hanging ring, claw, hanging buckle and sliding rail any one or a few share.
4. a kind of plural serial stage shipping unmanned aerial vehicle body according to claim 1, it is characterised in that: on the cargo chamber
End face and lower end surface are all provided at least one traction rope, the cargo chamber by traction rope respectively with control room adjacent thereto,
Power compartment and cargo chamber are connected with each other.
5. a kind of plural serial stage shipping unmanned aerial vehicle body according to claim 4, it is characterised in that: the traction rope end
End is connected with each other by rolling-up mechanism and shipping outdoor face.
6. a kind of plural serial stage shipping unmanned aerial vehicle body according to claim 1, it is characterised in that: the bearing keel
It is connected with each other between the carrying boxboard of the inner surface and the outer surface by several elastic cushion blocks.
7. a kind of plural serial stage shipping unmanned aerial vehicle body according to claim 1, it is characterised in that: the directive slide track
It is hinged with bearing keel outer surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811045474.2A CN109110133A (en) | 2018-09-07 | 2018-09-07 | A kind of plural serial stage shipping unmanned aerial vehicle body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811045474.2A CN109110133A (en) | 2018-09-07 | 2018-09-07 | A kind of plural serial stage shipping unmanned aerial vehicle body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109110133A true CN109110133A (en) | 2019-01-01 |
Family
ID=64858239
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811045474.2A Pending CN109110133A (en) | 2018-09-07 | 2018-09-07 | A kind of plural serial stage shipping unmanned aerial vehicle body |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109110133A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060108477A1 (en) * | 2004-11-23 | 2006-05-25 | Helou Elie Jr | Cargo aircraft |
| CN204586616U (en) * | 2015-01-20 | 2015-08-26 | 梁迎新 | Mobile shipping railway carriage or compartment |
| CN205602087U (en) * | 2015-12-23 | 2016-09-28 | 湖南云顶智能科技有限公司 | Unmanned aerial vehicle fuselage and unmanned aerial vehicle |
| CN106081112A (en) * | 2016-07-12 | 2016-11-09 | 于卫华 | Unmanned vehicle intelligence acceptance goods device and implementation |
| CN205971861U (en) * | 2016-07-28 | 2017-02-22 | 顺丰科技有限公司 | Unmanned aerial vehicle cargo hold |
| CN107651203A (en) * | 2017-10-31 | 2018-02-02 | 河南理工大学 | One kind is based on unmanned plane imaging mapping system plummer and application method |
| CN107719691A (en) * | 2017-08-28 | 2018-02-23 | 浙江大学 | A kind of conformal frock of the rib of large aircraft |
| CN107813939A (en) * | 2017-12-15 | 2018-03-20 | 南京中研专利技术开发有限公司 | It is a kind of that there is anticollision and be conveniently adjusted the unmanned plane pallet of storage area |
| CN107813938A (en) * | 2017-12-12 | 2018-03-20 | 南京市雨花台区创新创业法治宣传与法律服务中心 | A kind of unmanned plane is used can be according to the carrying apparatus of the big minor adjustment of article |
| CN207617959U (en) * | 2017-09-04 | 2018-07-17 | 陶文英 | A kind of box shipping unmanned plane |
-
2018
- 2018-09-07 CN CN201811045474.2A patent/CN109110133A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060108477A1 (en) * | 2004-11-23 | 2006-05-25 | Helou Elie Jr | Cargo aircraft |
| CN101102931A (en) * | 2004-11-23 | 2008-01-09 | E·小埃洛 | Cargo aircraft |
| CN204586616U (en) * | 2015-01-20 | 2015-08-26 | 梁迎新 | Mobile shipping railway carriage or compartment |
| CN205602087U (en) * | 2015-12-23 | 2016-09-28 | 湖南云顶智能科技有限公司 | Unmanned aerial vehicle fuselage and unmanned aerial vehicle |
| CN106081112A (en) * | 2016-07-12 | 2016-11-09 | 于卫华 | Unmanned vehicle intelligence acceptance goods device and implementation |
| CN205971861U (en) * | 2016-07-28 | 2017-02-22 | 顺丰科技有限公司 | Unmanned aerial vehicle cargo hold |
| CN107719691A (en) * | 2017-08-28 | 2018-02-23 | 浙江大学 | A kind of conformal frock of the rib of large aircraft |
| CN207617959U (en) * | 2017-09-04 | 2018-07-17 | 陶文英 | A kind of box shipping unmanned plane |
| CN107651203A (en) * | 2017-10-31 | 2018-02-02 | 河南理工大学 | One kind is based on unmanned plane imaging mapping system plummer and application method |
| CN107813938A (en) * | 2017-12-12 | 2018-03-20 | 南京市雨花台区创新创业法治宣传与法律服务中心 | A kind of unmanned plane is used can be according to the carrying apparatus of the big minor adjustment of article |
| CN107813939A (en) * | 2017-12-15 | 2018-03-20 | 南京中研专利技术开发有限公司 | It is a kind of that there is anticollision and be conveniently adjusted the unmanned plane pallet of storage area |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2387527A (en) | Cargo airplane | |
| US9738372B2 (en) | Low profile cargo handling system | |
| CN103895867B (en) | Flying wing with side cargo hold | |
| CN103693396B (en) | Track conveying device | |
| US11884196B2 (en) | Multi-functional cargo transfer vehicle and method | |
| CN210011885U (en) | Fixed wing commodity circulation unmanned aerial vehicle | |
| CN109110133A (en) | A kind of plural serial stage shipping unmanned aerial vehicle body | |
| CN110001968A (en) | A kind of heavy-lift helicopter freight transport system layout | |
| CN108860601A (en) | A kind of device and method of small-sized fixed-wing unmanned plane modularization load cabin | |
| CN102498040B (en) | For the method for installation system in airframe | |
| CN108945464B (en) | Cargo transport unmanned aerial vehicle material air-drop operation bearing cabin | |
| CN109131896A (en) | A kind of logistics aircraft and cargo hold and its automatic butt, the control system of separation and control method | |
| CN213008694U (en) | Light conveyor body | |
| US3108698A (en) | Sectional air cushion cargo floor | |
| CN109132607B (en) | Luggage handling facilities and luggage movement system | |
| US8931986B2 (en) | End stop device, cargo loading system and aircraft | |
| CN207162050U (en) | Indication control board General Mobile jacking equipment | |
| CN207810473U (en) | A kind of transmission device and luggage conveying vehicle equipped with handler | |
| US2463346A (en) | Transport airplane with interchangeable cargo holding units | |
| CN206417207U (en) | A kind of new unmanned plane cargo hold | |
| CN206704558U (en) | A kind of small-sized fixed-wing unmanned plane load cabin modular unit | |
| CN206914636U (en) | A kind of dual-purpose unmanned plane | |
| CN204526957U (en) | A kind of airframe transport trolley | |
| CN216581092U (en) | Luggage tracking device of bulk cargo loader | |
| CN106379528A (en) | Modular passenger-cargo dual-purpose aircraft |
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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190101 |