CN110001968A - A kind of heavy-lift helicopter freight transport system layout - Google Patents
A kind of heavy-lift helicopter freight transport system layout Download PDFInfo
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- CN110001968A CN110001968A CN201910216363.1A CN201910216363A CN110001968A CN 110001968 A CN110001968 A CN 110001968A CN 201910216363 A CN201910216363 A CN 201910216363A CN 110001968 A CN110001968 A CN 110001968A
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- 238000004806 packaging method and process Methods 0.000 claims abstract description 6
- 230000032258 transport Effects 0.000 claims description 48
- 238000000034 method Methods 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 3
- 230000011218 segmentation Effects 0.000 claims description 2
- 230000008901 benefit Effects 0.000 abstract description 5
- 208000020442 loss of weight Diseases 0.000 abstract description 3
- 238000005457 optimization Methods 0.000 abstract description 3
- 239000004744 fabric Substances 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/18—Floors
- B64C1/20—Floors specially adapted for freight
-
- 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
- B64D9/003—Devices for retaining pallets or freight containers
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Loading Or Unloading Of Vehicles (AREA)
- Ship Loading And Unloading (AREA)
Abstract
The invention belongs to air-cargo system technical fields, are related to a kind of heavy-lift helicopter freight transport system layout.Present invention combination heavy helicopter cargo component and multi-user's demand analysis result, layout is optimized to heavy helicopter freight transport system, under the premise of guaranteeing that various functions are realized with transportation safety, to the guiding device installed on machine, transmitting device, mooring device, restraint device, control device and self-loading-unloading device etc. have carried out adaptability design, realize the optimum balance of system function optimization and loss of weight, so that the type is to packaging cargo, bulk goods, vehicle arrangement, the shipment of the shipment objects such as personnel's transport has better adaptability, it is wider to load object range, it is greatly improved the transport capacity of carrier aircraft.The present invention is designed using 463L standards system, has good compatibility with other transporter freight transport systems, it is contemplated that on following multiple types with good application prospect, profit margin and market prospects are considerable, and economic benefit is good.
Description
Technical field
The invention belongs to air-cargo system technical fields, are related to a kind of heavy-lift helicopter freight transport system layout.
Background technique
Heavy-lift helicopter refers to that take-off weight is greater than 20 tons of transport helicopter, civilian aspect, due to heavy duty transport
Helicopter maneuverability is strong, carrying capacity is big, can by way of containing conveying people, vehicle equipment and packaging/bulk goods,
Great function has all been played in all previous major natural disasters；Military aspect is used as transport chain end important transportation tool,
It plays an important role in terms of equipment transport, material supply.
Still without the heavy helicopter of independent development, domestic only heavy helicopter is Russian type in China at present, but
The type freight transport system is relatively simple, and the efficiency of loading and unloading is poor, does not meet China's national situation needs, though and U.S.'s heavy helicopter has had
Kind goods traffic equipment, but due to model structure difference, mating freight transport system is not suitable for China's heavy helicopter cargo hold.
Summary of the invention
The object of the invention: present invention combination heavy helicopter cargo component and multi-user's demand analysis are as a result, to heavy type
Layout is optimized in helicopter freight transport system, the optimum balance of system function optimization and loss of weight is realized, so that the type is to collection
The shipment of the shipment objects such as loading object, bulk goods, vehicle arrangement, personnel's transport has better adaptability, loads object model
It encloses more extensively, is greatly improved the transport capacity of carrier aircraft.
A kind of technical solution of the present invention: heavy-lift helicopter freight transport system layout, which is characterized in that according to user demand
Analysis is as a result, heavy helicopter freight transport system object of transport mainly includes packaging cargo, bulk goods, the vehicle of 463L standards system
Equipment, weaponry, personnel, loading and transport for object of transport have been carried out heavy helicopter freight transport system layout and have been set
Meter, while also having fully considered the compatibility with other type through transports, specific layout is as follows:
A) four column mooring devices (6) are arranged symmetrically on cargo deck (11), each column mooring device (6) is according to aircaft configuration
Determine that arrangement spacing and bearing capacity value, two column mooring device (6) of outermost are arranged in below cargo hold guiding device (5)；
B) 4 column transmitting devices (3), transmitting device (3) point are arranged symmetrically on cargo deck (11) and sloping platform floor (12)
Section is installed in aircraft cargo bay floor (11) and sloping platform floor (12) groove；
C) using cargo deck (11) center line as line of symmetry, left and right one column cargo hold guiding device (5) of each arrangement, sloping platform floor
(12) one column sloping platform guiding device (7) of each arrangement in left and right；
D) more than one piece restraint device (8) are installed inside two column cargo hold guiding devices (5)；
E) the internal restraint device (8) of cargo hold guiding device (5) and movable pressing board (9) are all made of automatically controlled mode and realize stretching
With withdrawal, the control device (4) by being installed on cargo hold side wall is controlled；
F) cargo hold front end is arranged symmetrically stop device (2) by line of symmetry of floor center line, arrangement quantity and load value, root
It is determined according to object is loaded；
G) control device (4) of tray (15) arrangement control restraint device (8), with symmetrical two pairs of restraint devices 8
For a control unit, control device (4) position is between two units；
H) self-loading-unloading device (1) is arranged in cargo hold front end, the device using automatically controlled driving method work, when manual loading/
When unloading is difficult, it can be used self-loading-unloading device as auxiliary device, drawn or pulled to object is loaded.
Two column mooring device (6) slewing area of outside is 1/4 ball, when installation space is wider, can also be filled guiding
It sets and is staggeredly arranged with mooring device.
The transmitting device (3) is in use, transport plane is upward, the transmission for cargo；When not used, by its transport plane
Overturning downwards, is flushed with airplane floor, is loaded for vehicle arrangement etc..
The stop device (2) shares two states, and loading cargo, it is in tip-up state, for the stop of cargo, dress
After the completion of load, the state of turning down is placed it in, is located at airplane floor lower face.
Cargo hold guiding device (5) end realizes the restraint of cargo vertical direction using movable pressing board (9), loads cargo
In the process, control movable pressing board is withdrawn, and avoids colliding with tray；After the completion of loading, control movable pressing board (9) is placed in stretching
State, the restraint for cargo vertical direction.
When aircraft cargo bay floor (11) space is limited, cloth mooring device (6) can be combined with cargo hold guiding device (5)
It sets.
When restraint device (8) working condition, internal restraint component stretches out restraint face, the course (13) for cargo
And the restraint of inverse course (14)；When off working state, restraint component is withdrawn.
The cargo hold guiding device (5), sloping platform guiding device (7) restraint interplanar distance carry out really according to object size is loaded
It is fixed, guiding device main function lateral, vertical direction restraint when being the guiding and air transportion when passing in and out cabin for tray.
The invention has the advantages that: the present invention to combine heavy helicopter cargo component and multi-user's demand analysis as a result, right
Layout is optimized in heavy helicopter freight transport system, under the premise of guaranteeing that various functions are realized with transportation safety, is based on appointing
Business type and ratio rationally design device configurations, to the guiding device, transmitting device, mooring device, limit installed on machine
Dynamic device, control device and self-loading-unloading device etc. have carried out adaptability design, realize system function optimization and loss of weight most
Good balance, so that the type has more the shipment of the shipment objects such as packaging cargo, bulk goods, vehicle arrangement, personnel's transport
Good adaptability, loading object range is wider, is greatly improved the transport capacity of carrier aircraft.The present invention is based on heavy helicopter goods
Cabin structure is laid out design, has fully considered a variety of common loading objects of heavy helicopter, and for different loading objects into
Adaptability design is gone, the application of the invention can effectively improve loading and unloading efficiency, shorten the aircraft floor residence time, have good
Economic benefit.The present invention is designed using 463L standards system, is had with other transporter freight transport systems good compatible
Property, it is contemplated that on following multiple types with good application prospect, profit margin and market prospects are considerable, and economic benefit is good
It is good.
Detailed description of the invention
Fig. 1 heavy-lift helicopter is laid out main view
Wherein: 1- self-loading-unloading device, 2- stop device, 3- transmitting device, 4- control device, 5- cargo hold guiding device, 6-
Mooring device, 7- sloping platform guiding device, 8- restraint device, 9- movable pressing board
Fig. 2 heavy-lift helicopter is laid out right view
Fig. 3 mooring device 6 of the present invention, 8 partial enlarged view of restraint device
Fig. 49 partial enlarged view of movable pressing board of the present invention
Specific embodiment
The following further describes the present invention with reference to the drawings:
As shown in Figure 1, according to user requirements analysis as a result, heavy helicopter freight transport system object of transport mainly includes 463L
The packaging cargo of standards system, bulk goods, vehicle arrangement, weaponry, personnel etc., the present invention are directed to the loading of object of transport
And heavy helicopter freight transport system layout designs have been carried out in transport, while also having been fully considered compatible with other type through transports
Property, specific layout character are as follows:
A) four column mooring devices 6 are arranged symmetrically on cargo deck 11, each column mooring device 6 determines cloth according to aircaft configuration
Spacing and bearing capacity value are set, when airplane floor space is limited, arrangement, outermost mooring device 6 can be combined with guiding device
Two column mooring devices 6 are arranged in below side rails, and 6 slewing area of mooring device is 1/4 ball, under the premise of assurance function performance,
The advantages of with saving space, reducing system weight；When installation space is wider, guiding device and mooring device can be also staggered
Arrangement.
B) 4 column transmitting devices 4 are arranged symmetrically on cargo deck and sloping platform floor, the segmentation of transmitting device 4 is installed on aircraft
In 12 groove of cargo deck 11 and sloping platform floor, in use, 4 transport plane of transmitting device is upward, the transmission for cargo；Do not have to
When, its transport plane is overturn downwards, is flushed with airplane floor, is loaded for vehicle arrangement etc..
C) using cargo deck center line as line of symmetry, a column continous way is respectively arranged on cargo deck 11 and sloping platform floor 12 or so
Guiding device, guiding device restraint interplanar distance are determined according to object size is loaded, and guiding device main function is for goods
Lateral, vertical direction restraint when guiding and air transportion when disk passes in and out cabin.
D) more than one piece restraint device 8 is installed inside two column guiding devices, when working condition, restraint component stretches out restraint face,
For the course of cargo and the restraint in stemming direction；When off working state, restraint component is withdrawn.
It e) is to prevent from causing to touch with cargo hold guiding device 5 during 16 loading and unloading of cargo hold side wall due to aircraft ground angle
It hits, 5 end of cargo hold guiding device realizes the restraint of cargo vertical direction using movable pressing board, and during loading cargo, control is lived
Dynamic pressure plate is withdrawn, and avoids colliding with tray；After the completion of loading, control movable pressing board is placed in stretching state, hangs down for cargo
Histogram to restraint.
F) restraint device 8 inside cargo hold guiding device 5 and movable pressing board 9 are all made of automatically controlled mode and realize stretching and receive
It returns, the control device 4 by being installed on cargo hold side wall 15 is controlled；
G) cargo hold front end is arranged symmetrically stop device 2, arrangement quantity and load value by line of symmetry of floor center line, according to
Object is loaded to determine；Stop device 2 shares two states, and loading cargo, it is in tip-up state, for the stop of cargo, loads
After the completion, the state of turning down is placed it in, airplane floor lower face is located at；
H) control device 4 of the arrangement of tray 15 control restraint device 8 and movable pressing board 9, with symmetrical two pairs of air transportions
Lock is a control unit, and 4 position of control device is between two units；
I) self-loading-unloading device 1 is arranged in cargo hold front end, which is worked using automatically controlled driving method, as manual loading/unload
When carrying difficult, it can be used self-loading-unloading device as auxiliary device, drawn or pulled to object is loaded.
Embodiment:
A) cargo hold guiding device 5 and sloping platform guiding device 7 are symmetrically arranged in cargo hold two using 11 center line of floor as line of symmetry
Side；
B) cargo hold guiding device 5 has been internally integrated restraint device 8, which is controlled using automatically controlled mode, and tray 16 loads
After in place, its work can be controlled by control device 4, to realize the restraint in tray course 13 and inverse 14 direction of course；
C) when loading and unloading tray 15, transmitting device 3 is dug to upward state；Other objects such as loading and unloading vehicle equipment
When product, transmitting device 3 is turned down, is flushed with floor；
When d) loading tray 15, end stop device is set into 2 stop in tip-up state, for 16 course direction 13 of tray；
When not needing using end stop device 2, down state is placed it in；
When e) loading tray 15, movable pressing board 9 is withdrawn by control device 4, after the completion of loading, passes through control device 4
Movable pressing board 9 is stretched out, realizes the restraint of 16 vertical direction of cargo hold side wall；
F) control device 4 of cargo hold side wall arrangement restraint device and movable pressing board, with symmetrical two pairs of restraint devices I
For a control unit, 4 position of control device is between two units；
G) when manual handling carries difficult, the traction and dragging of cargo are realized using self-loading-unloading device 1, which is driven using electricity
Flowing mode is controlled by dedicated control device；
H) four column mooring devices 6 are installed on cargo deck, be tethered at a little as loading, for vehicle, equipment, facility etc.
It is tethered at.As shown in Fig. 1 Fig. 3, II is position and the structure of mooring device 6 and restraint device 8.
Claims (8)
1. a kind of heavy-lift helicopter freight transport system layout, which is characterized in that according to user requirements analysis as a result, heavy type is gone straight up to
Machine freight transport system object of transport mainly include the packaging cargo of 463L standards system, bulk goods, vehicle arrangement, weaponry,
Personnel, loading and transport for object of transport have carried out heavy helicopter freight transport system layout designs, while also fully considering
Compatibility with other type through transports, specific layout are as follows:
A) four column mooring devices (6) are arranged symmetrically on cargo deck (11), each column mooring device (6) is determined according to aircaft configuration
Arrange that spacing and bearing capacity value, two column mooring device (6) of outermost are arranged in below cargo hold guiding device (5)；
B) 4 column transmitting devices (3), transmitting device (3) segmentation peace are arranged symmetrically on cargo deck (11) and sloping platform floor (12)
Loaded in aircraft cargo bay floor (11) and sloping platform floor (12) groove；
C) using cargo deck (11) center line as line of symmetry, left and right one column cargo hold guiding device (5) of each arrangement, sloping platform floor (12)
Left and right one column sloping platform guiding device (7) of each arrangement；
D) more than one piece restraint device (8) are installed inside two column cargo hold guiding devices (5)；
E) the internal restraint device (8) of cargo hold guiding device (5) and movable pressing board (9) are all made of automatically controlled mode and realize stretching and receive
It returns, the control device (4) by being installed on cargo hold side wall is controlled；
F) cargo hold front end is arranged symmetrically stop device (2) by line of symmetry of floor center line, arrangement quantity and load value, according to dress
Object is carried to determine；
G) control device (4) of tray (15) arrangement control restraint device (8), with symmetrical two pairs of restraint devices 8 for one
A control unit, control device (4) position is between two units；
H) self-loading-unloading device (1) is arranged in cargo hold front end, which is worked using automatically controlled driving method, when manual loading/unloading
When difficult, it can be used self-loading-unloading device as auxiliary device, drawn or pulled to object is loaded.
2. a kind of heavy-lift helicopter freight transport system layout as described in claim 1, which is characterized in that the outside two arranges
Mooring device (6) slewing area is that guiding device and mooring device can also be staggeredly arranged by 1/4 ball when installation space is wider.
3. a kind of heavy-lift helicopter freight transport system layout as described in claim 1, which is characterized in that the transmitting device
(3) transmission in use, transport plane is upward, for cargo；When not used, its transport plane is overturn downwards, with airplane floor
It flushes, is loaded for vehicle arrangement etc..
4. a kind of heavy-lift helicopter freight transport system layout as described in claim 1, which is characterized in that the stop device
(2) two states are shared, loading cargo, it is in tip-up state, for the stop of cargo, after the completion of loading, places it in and turns down
State is located at airplane floor lower face.
5. a kind of heavy-lift helicopter freight transport system layout as described in claim 1, which is characterized in that the cargo hold guiding
Device (5) end realizes the restraint of cargo vertical direction using movable pressing board (9), during loading cargo, controls movable pressing board
It withdraws, avoids colliding with tray；After the completion of loading, control movable pressing board (9) is placed in stretching state, is used for cargo Vertical Square
To restraint.
6. a kind of heavy-lift helicopter freight transport system layout as described in claim 1, which is characterized in that the cargo deck
(11) when space is limited, arrangement can mooring device (6) be combined with cargo hold guiding device (5).
7. a kind of heavy-lift helicopter freight transport system layout as described in claim 1, which is characterized in that the restraint device
(8) when working condition, internal restraint component stretches out restraint face, for the course (13) of cargo and the restraint of inverse course (14)；
When off working state, restraint component is withdrawn.
8. a kind of heavy-lift helicopter freight transport system layout as described in claim 1, which is characterized in that the cargo hold guiding
Device (5), sloping platform guiding device (7) restraint interplanar distance are determined according to object size is loaded, and guiding device main function is
Lateral, vertical direction restraint when guiding and air transportion when passing in and out cabin for tray.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910216363.1A CN110001968A (en) | 2019-03-20 | 2019-03-20 | A kind of heavy-lift helicopter freight transport system layout |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910216363.1A CN110001968A (en) | 2019-03-20 | 2019-03-20 | A kind of heavy-lift helicopter freight transport system layout |
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| Publication Number | Publication Date |
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| CN110001968A true CN110001968A (en) | 2019-07-12 |
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| CN201910216363.1A Pending CN110001968A (en) | 2019-03-20 | 2019-03-20 | A kind of heavy-lift helicopter freight transport system layout |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111846241A (en) * | 2020-07-29 | 2020-10-30 | 中航电测仪器股份有限公司 | Portable external-hanging shelter cargo transportation device and method for helicopter |
| CN112380618A (en) * | 2020-10-30 | 2021-02-19 | 中国直升机设计研究所 | Rapid design method for internal shape of passenger cargo compartment of transport helicopter |
| CN114056553A (en) * | 2021-12-03 | 2022-02-18 | 航天神舟飞行器有限公司 | Medium-sized freight unmanned helicopter system |
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| CN114056553A (en) * | 2021-12-03 | 2022-02-18 | 航天神舟飞行器有限公司 | Medium-sized freight unmanned helicopter system |
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Application publication date: 20190712 |
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