CN206797692U - Can handling goods aircraft fuselage loading cabin - Google Patents
Can handling goods aircraft fuselage loading cabin Download PDFInfo
- Publication number
- CN206797692U CN206797692U CN201720340530.XU CN201720340530U CN206797692U CN 206797692 U CN206797692 U CN 206797692U CN 201720340530 U CN201720340530 U CN 201720340530U CN 206797692 U CN206797692 U CN 206797692U
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- CN
- China
- Prior art keywords
- attachment means
- carbon fiber
- fuselage
- loading cabin
- freight container
- 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
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- Packaging Of Machine Parts And Wound Products (AREA)
Abstract
The utility model proposes can handling goods aircraft fuselage loading cabin, including：Fuselage (1) and loading cabin (2), the loading cabin (2) is arranged at the lower section of fuselage (1), it is fixedly connected with fuselage (1), the present apparatus has that lighter weight, bearing capacity are larger, can realize fast assembling-disassembling, goods and materials and air-drop are rapidly loaded, the advantages that different configuration flight replaceable simultaneously for different situations.
Description
Technical field
The utility model belongs to technical grade vehicle technology field, particularly can handling goods aircraft fuselage loading
Cabin.
Background technology
With the development of technology, developed rapidly in recent years using aircraft, all kinds of course of new aircraft emerge in an endless stream, hundred
Flower full cries.But also there are many problems when using aircraft, especially for the aircraft of load-carrying class, volume itself
It is huger, structure is complex, easily damage, on the other hand, due to the deadweight problem of aircraft, its load-carrying is also limited
System, meanwhile, para-cargo is not easy to.
Utility model content
In order to solve the above problems, the utility model provide can handling goods aircraft fuselage loading cabin.
Concrete technical scheme is as follows：
Can handling goods aircraft fuselage loading cabin, including：Fuselage (1) and loading cabin (2), the loading cabin (2) set
The lower section of fuselage (1) is placed in, is fixedly connected with fuselage (1)；
The fuselage (1) includes head connector (3), main wing attachment means (4) and empennage attachment means (5), described
Main wing attachment means (4) are fixed between head connector (3) and empennage attachment means (5) by carbon fiber pipe, the machine
Head attachment means (3) are arranged at the front end of fuselage (1), and the empennage attachment means (5) are arranged at the rear end of fuselage (1), described
Cabin is set between head connector (3) and empennage attachment means (5)；
The loading cabin (2) includes freight container, front-wheel (6) and undercarriage (7), the freight container and is arranged at cabin
Underface, the main wing attachment means (4) are fixedly connected by carbon fiber sheet with the bottom of freight container, the undercarriage (7)
Including support bar (8) and rear undercarriage wheel (9), the support bar (8) passes through eccentric coupling device (10) with rear undercarriage wheel (9)
Connection, the support bar (8) passes perpendicularly through the carbon fiber sheet between main wing attachment means (4) and freight container bottom, before described
Wheel (6) is arranged at the front end of freight container by steering unit for front wheels (11), and the bottom of the freight container sets load carrier
(12), one end of the load carrier (12) is connected by carbon fiber pipe with freight container bearing, the load carrier (12)
The other end is with freight container by snapping connection.
Preferably, the empennage attachment means (5) include carbon fiber workpiece, and the number of the carbon fiber workpiece is more than
Equal to 2.
Preferably, the projection of the main wing attachment means (4) is coincide with the neck on carbon fiber sheet.
Preferably, the projection of the main wing attachment means (4) is hollow-core construction, the right angle of the main wing attachment means (4)
Place sets intercommunicating pore.
Preferably, the carbon fiber pipe and head connector (3), main wing attachment means (4) and empennage attachment means (5)
Connected mode for bonding or fiber band fix.
Preferably, the eccentric coupling device (10) is connected with rear undercarriage wheel (9) bearing.
Preferably, the steering unit for front wheels (11) is connected with front-wheel (6) bearing.
Preferably, the steering unit for front wheels (11) is arranged at the front end of freight container by carbon fiber sheet.
Preferably, the load carrier (12) is connected with carbon fiber pipe bearing.
Relative to prior art, it is described in the utility model can handling goods aircraft fuselage loading cabin have it is following excellent
Gesture：
The utility model proposes can handling goods aircraft fuselage loading cabin, lighter weight, bearing capacity are larger, energy
Fast assembling-disassembling is enough realized, is rapidly loaded goods and materials and air-drop, simultaneously for the replaceable different configuration flights of different situations.
Brief description of the drawings
Fig. 1 be the utility model proposes can handling goods aircraft fuselage loading cabin schematic diagram.
Description of reference numerals：
The empennage attachment means of 1 fuselage, 2 loading cabin, 3 head connector, 4 main wing attachment means 5
The eccentric coupling device of undercarriage wheel 10 after the support bar 9 of 6 front-wheel, 7 undercarriage 8
The load carrier of 11 steering unit for front wheels 12
Embodiment
The technical solution of the utility model is further described below in conjunction with embodiment.It should be appreciated that herein
The embodiment of description only to explain the utility model, is not used to limit the utility model.
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ",
The orientation or position relationship of the instruction such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of description the utility model and simplifies description, rather than instruction
Or imply that signified device or element must have specific side, with specific azimuth configuration and operation, therefore it is not intended that
To limitation of the present utility model.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can be mechanical connection or electrical connection；Can be directly connected to, can also be indirectly connected by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, on being understood by concrete condition
State concrete meaning of the term in the utility model.
Describe the utility model in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
Fig. 1 be the utility model proposes can handling goods aircraft fuselage loading cabin schematic diagram, including fuselage (1)
With loading cabin (2), the loading cabin (2) is arranged at the lower section of fuselage (1), is fixedly connected with fuselage (1)；Fuselage (1) includes machine
Head attachment means (3), main wing attachment means (4) and empennage attachment means (5), head connector (3), main wing attachment means
(4) set gradually in order from the front end of fuselage (1) to rear end with empennage attachment means (5), main wing attachment means (4) pass through carbon
Fibre pipe is fixed between head connector (3) and empennage attachment means (5), and carbon fiber pipe is stuck in main wing attachment means (4)
In following neck, and fixed with adhesive and fiber band, adhesive can use 502 glue, and fiber band can be drawn with Kev, and main wing connects
The carbon fiber pipe of connection device (4) above can also be fixed in main wing attachment means (4) with adhesive and fiber band, main wing connection
The outside in the face of device (4) vertically downward is connected with carbon fiber sheet, projection and the card on carbon fiber sheet of main wing attachment means (4)
Groove coincide, and is fixed together.Meanwhile the projection of main wing attachment means (4) is hollow-core construction, the right angle of main wing attachment means (4)
Place is respectively provided with intercommunicating pore, can be inserted into wing in the hollow-core construction of projection, while fixes wing through intercommunicating pore with bolt, institute
The front end that head connector (3) is arranged at fuselage (1) is stated, can be in head connector (3) engine installed above and spiral shell
Oar is revolved, the empennage attachment means (5) are arranged at the rear end of fuselage (1), including carbon fiber workpiece, of carbon fiber workpiece
Number is more than or equal to 2, and manhole is set among carbon fiber workpiece, and this through hole can allow the carbon fiber pipe of connection empennage to be worn
Cross, and play a part of fixed support, the carbon fiber pipe being connected with main wing attachment means (4) also connects with empennage attachment means (5)
Connect, and connected mode is similar.Cabin is set between the head connector (3) and empennage attachment means (5), the cabin by
Carbon fiber pipe is surrounded and formed.
The loading cabin (2) includes freight container, front-wheel (6) and undercarriage (7), the freight container and is arranged at cabin
Underface, surrounded and formed by carbon fiber pipe, and fixed structure is set on larger facing, such as increased carbon fiber pipe, allow
Overall endurance increase, the main wing attachment means (4) are fixedly connected with the bottom of freight container by carbon fiber sheet, risen and fallen
Frame (7) includes support bar (8) and rear undercarriage wheel (9), and support bar (8) passes through eccentric coupling device with rear undercarriage wheel (9)
(10) connect, eccentric coupling device (10) is connected with rear undercarriage wheel (9) bearing, and support bar (8) passes perpendicularly through main wing connection dress
The carbon fiber sheet between (4) and freight container bottom is put, the front-wheel (6) is arranged at load-carrying box by steering unit for front wheels (11)
The front end of body, steering unit for front wheels (11) are arranged at the front end of freight container, carbon fiber sheet and freight container by carbon fiber sheet
It is fixedly connected, carbon fiber sheet is connected with steering unit for front wheels (11) bearing, and steering unit for front wheels (11) connects with front-wheel (6) bearing
Connect, the bottom of the freight container sets load carrier (12), the load carrier (12) by more transverse directions carbon fiber pipe and
The carbon fiber pipe connection of more longitudinal directions combines, carbon fiber pipe used number can go flexibly to become according to actual load-bearing
Dynamic, in the utility model, horizontal carbon fiber pipe used is 3, and longitudinal carbon fiber pipe is 1, the load carrier (12)
One end be connected by carbon fiber pipe with freight container bearing, load carrier (12) and carbon fiber pipe, carbon fiber pipe and load-carrying box
The connected mode of body be bearing connection, the other end of the load carrier (12) with freight container by snapping connection, if need
When wanting para-cargo, open buckle, load carrier (12) around carbon fiber pipe rotate and under, cargo dropping is gone out.
In summary, the utility model proposes can handling goods aircraft fuselage loading cabin, lighter weight, carrying energy
Power is larger, can realize fast assembling-disassembling, is rapidly loaded goods and materials and air-drop, flies simultaneously for the replaceable different configurations of different situations
OK.
Embodiment above is preferred embodiment of the present utility model, is not thereby limited of the present utility model special
Sharp protection domain.Those skilled in the art belonging to any the utility model, it is disclosed in the utility model not departing from
The equivalent structure and the conversion of equivalent step done on the premise of spirit and scope to content of the present utility model each falls within this reality
Within new claimed the scope of the claims.
Claims (9)
1. can handling goods aircraft fuselage loading cabin, it is characterised in that including：Fuselage (1) and loading cabin (2), the load
Cargo hold (2) is arranged at the lower section of fuselage (1), is fixedly connected with fuselage (1)；
The fuselage (1) includes head connector (3), main wing attachment means (4) and empennage attachment means (5), the main wing
Attachment means (4) are fixed between head connector (3) and empennage attachment means (5) by carbon fiber pipe, and the head connects
Connection device (3) is arranged at the front end of fuselage (1), and the empennage attachment means (5) are arranged at the rear end of fuselage (1), the head
Cabin is set between attachment means (3) and empennage attachment means (5)；
The loading cabin (2) includes freight container, front-wheel (6) and undercarriage (7), the freight container be arranged at cabin just under
Side, the main wing attachment means (4) are fixedly connected by carbon fiber sheet with the bottom of freight container, and the undercarriage (7) includes
Support bar (8) and rear undercarriage wheel (9), the support bar (8) are connected with rear undercarriage wheel (9) by eccentric coupling device (10)
Connect, the support bar (8) passes perpendicularly through the carbon fiber sheet between main wing attachment means (4) and freight container bottom, the front-wheel
(6) front end of freight container is arranged at by steering unit for front wheels (11), the bottom of the freight container sets load carrier
(12), one end of the load carrier (12) is connected by carbon fiber pipe with freight container bearing, the load carrier (12)
The other end is with freight container by snapping connection.
2. it is according to claim 1 can handling goods aircraft fuselage loading cabin, it is characterised in that empennage connection
Device (5) includes carbon fiber workpiece, and the number of the carbon fiber workpiece is more than or equal to 2.
3. it is according to claim 1 can handling goods aircraft fuselage loading cabin, it is characterised in that main wing connection
The projection of device (4) is coincide with the neck on carbon fiber sheet.
4. it is according to claim 3 can handling goods aircraft fuselage loading cabin, it is characterised in that main wing connection
The projection of device (4) is hollow-core construction, and the right angle of the main wing attachment means (4) sets intercommunicating pore.
5. it is according to claim 1 can handling goods aircraft fuselage loading cabin, it is characterised in that the carbon fiber pipe
Consolidate with the connected mode of head connector (3), main wing attachment means (4) and empennage attachment means (5) for bonding or fiber band
It is fixed.
6. it is according to claim 1 can handling goods aircraft fuselage loading cabin, it is characterised in that the eccentric connection
Device (10) is connected with rear undercarriage wheel (9) bearing.
7. it is according to claim 1 can handling goods aircraft fuselage loading cabin, it is characterised in that the front-wheel steer
Device (11) is connected with front-wheel (6) bearing.
8. it is according to claim 7 can handling goods aircraft fuselage loading cabin, it is characterised in that the front-wheel steer
Device (11) is arranged at the front end of freight container by carbon fiber sheet.
9. it is according to claim 1 can handling goods aircraft fuselage loading cabin, it is characterised in that the load carrier
(12) it is connected with carbon fiber pipe bearing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720340530.XU CN206797692U (en) | 2017-03-31 | 2017-03-31 | Can handling goods aircraft fuselage loading cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720340530.XU CN206797692U (en) | 2017-03-31 | 2017-03-31 | Can handling goods aircraft fuselage loading cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206797692U true CN206797692U (en) | 2017-12-26 |
Family
ID=60731552
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720340530.XU Expired - Fee Related CN206797692U (en) | 2017-03-31 | 2017-03-31 | Can handling goods aircraft fuselage loading cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206797692U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045549A (en) * | 2017-12-31 | 2018-05-18 | 上海牧羽航空科技有限公司 | A kind of tiltrotor with separable function pod |
| CN111434579A (en) * | 2019-01-11 | 2020-07-21 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle tail boom quick assembly disassembly structure |
-
2017
- 2017-03-31 CN CN201720340530.XU patent/CN206797692U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045549A (en) * | 2017-12-31 | 2018-05-18 | 上海牧羽航空科技有限公司 | A kind of tiltrotor with separable function pod |
| CN111434579A (en) * | 2019-01-11 | 2020-07-21 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle tail boom quick assembly disassembly structure |
| CN111434579B (en) * | 2019-01-11 | 2022-09-09 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle tail-stay quick assembly disassembly structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171226 Termination date: 20190331 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |