CN106428601A - Method for greatly increasing number of aircrafts picked up by aircraft carrier - Google Patents
Method for greatly increasing number of aircrafts picked up by aircraft carrier Download PDFInfo
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- CN106428601A CN106428601A CN201510602993.4A CN201510602993A CN106428601A CN 106428601 A CN106428601 A CN 106428601A CN 201510602993 A CN201510602993 A CN 201510602993A CN 106428601 A CN106428601 A CN 106428601A
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
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Abstract
The invention relates to a method for greatly increasing the number of aircrafts picked up by an aircraft carrier. The method is characterized in that a double-layer hangar structure or a multi-layer hanger structure is adopted, and a technical scheme of combining a broadside type aircraft elevator and an in-broad type aircraft elevator mechanism is matched for use, so that under the premise that the situation that the carrier-based aircrafts in the hangar is safely, smoothly, accurately, conveniently and quickly transported to a flight deck is guaranteed, the number of the aircrafts picked up by the aircraft carrier can be substantially increased.
Description
Technical field
The present invention relates to a kind of improve the method that aircraft carrier carries number of aircraft.
Background technology
Aircraft carrier is the symbol of big country's strength, and the performance of aircraft carrier and advanced degree are the bodies of a national science and technology strength
Existing, however, aircraft carrier manufacturing cost is expensive, using complexity, people are desirable on relatively small aircraft carrier carrying more work
War aircraft, relatively to improve the fighting capacity of aircraft carrier optimal in structure.It has been proposed that parked using double-deck flight-deck more flying
Machine, the requirement that this mode does not obviously account for flight-deck is how high, and double-deck flight-deck takes off landing pipe
Reason is complicated., using multilamellar hangar in order to increase carrier aircraft quantity, but modern aircraft carrier is all using outboard aircraft lifting and landing for the aircraft carrier having in the past
Machine, in the case of using multilamellar store structure, if flight-deck water surface elevation position is certain, and outboard aircraft elevator
Require to reach flight-deck from minus two layers of hangar, then the minimum altitude of outboard aircraft elevator is just by tactile water；If minus two layers
Hangar is placed on traditional hangar normal height position, and outboard aircraft elevator requires to reach flight-deck from minus two layers of hangar,
So flight-deck just will exceed the height of a hangar than traditional aircraft carrier；Therefore, if require to keep the knot of modern aircraft carrier again
Structure, the outboard aircraft elevator conveying aircraft mode again keeping traditional is constant, is highly difficult.
Content of the invention
It is an object of the invention to inventing a kind of structure that can keep modern aircraft carrier, and traditional outboard aircraft can be kept
Elevator delivery aircraft mode is constant, can increase substantially the method that aircraft carrier carries number of aircraft again.
The technical solution adopted for the present invention to solve the technical problems is that one kind increases substantially aircraft carrier and carries aircraft
The method of quantity, using double-deck or multilamellar store structure, cooperation adds inboard formula aircraft elevator using topside formula aircraft elevator
Technical scheme, is characterized in that：Using double-deck or multilamellar store structure, between negative one layer hangar and flight-deck, adopt a kind of hydraulic pressure
Magnetic suspension aircraft carrier topside formula aircraft elevator, and adopt a kind of hydraulic pressure magnetcisuspension from lowermost layer hangar to negative one layer hangar
Floating aircraft carrier inboard formula aircraft elevator is connected；Negative one layer hangar aircraft is directly entered outboard aircraft elevator and serves flight first
Plate, the aircraft of layers below hangar is transported to negative one layer hangar by inboard formula aircraft elevator and enters back into outboard aircraft elevator
Serve flight-deck.
The invention has the beneficial effects as follows：
1st, using double-deck or multilamellar hangar, aircraft carrier can be increased substantially and carry number of aircraft；
2nd, inboard formula aircraft elevator technical scheme is added using topside formula aircraft elevator, conventional airplane can be kept to convey
Mode is constant, and user of service can implement to hold substantially not change original working mode, the continuity of method easy to use
Easily.
3rd, topside formula aircraft elevator and inboard formula aircraft elevator are all lifted using hydraulic pressure magnetic suspension carrier-based aircraft
Machine technology, even if deposit in the aircraft of bottom hangar it is also possible to quickly aircraft be served aircraft deck.
4th, hydraulic pressure magnetic suspension carrier-based aircraft elevator than traditional cable wire hoisting type elevator run more steadily, reliable and
Safety, safeguards simpler.
If 5 adopt hydraulic pressure magnetic suspension carrier-based aircraft elevator technology reconstruction aircraft carrier goods and materials and ammunition hoist, its
Travelling speed and efficiency will have several times and improve, and not have the complicated hoist engine-wire rope structure equipment of that set of conventional elevator,
Save deck space and area.
Brief description
The invention will be further described with reference to the accompanying drawings and examples.
Fig. 1, Fig. 2 and Fig. 3 are that one kind of the present invention adopts three layers of hangar, using a kind of hydraulic pressure magnetic suspension aircraft carrier inboard
Aircraft elevator by negative one layer, minus two layers be connected with minus three layers of hangar, then use cooperatively a kind of hydraulic pressure magnetic suspension aircraft carrier
Topside formula aircraft elevator conveys the structural representation of each layer hangar aircraft, wherein：
Fig. 1 is that carrier-borne aircraft has been transported to negative one layer hangar first by a kind of hydraulic pressure magnetic suspension aircraft carrier inboard aircraft elevator
Structural representation during plate.
In Fig. 1,001, carrier-borne aircraft；110th, negative one layer hangar deck；111st, the warship side of a ship；112nd, warship side of a ship opening；113rd, negative one layer
Hangar aircraft delivery track；210th, topside formula aircraft elevator structure body panel；211st, topside formula aircraft elevator vertical structure
Part；212nd, mounting structure；213rd, oil cylinder guide rail；300th, hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator；310th, the side of a ship
Side formula aircraft elevator hoistable platform；311st, topside formula aircraft elevator hoistable platform aircraft delivery track；312nd, topside formula flies
Machine elevator leads boots；400th, hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator；410th, inboard formula aircraft elevator lifting
Platform；411st, inboard formula aircraft elevator hoistable platform aircraft delivery track；420th, inboard formula aircraft elevator hoistable platform rotation
Turn platform；421st, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track；422nd, inboard formula aircraft elevator
Hoistable platform rotation platform center of rotation；423rd, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track wheel
Fixed block.
Fig. 2 is that carrier-borne aircraft has been transported to minus two layers of hangar first by a kind of hydraulic pressure magnetic suspension aircraft carrier inboard aircraft elevator
Structural representation during plate, in figure shows oil cylinder guide rail and leads the structure of the elevator such as boots.
In Fig. 2,001, carrier-borne aircraft；111st, the warship side of a ship；120th, minus two layers of hangar deck；410th, inboard formula aircraft elevator lifting
Platform；411st, inboard formula aircraft elevator hoistable platform aircraft delivery track；420th, inboard formula aircraft elevator hoistable platform rotation
Turn platform；421st, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track；422nd, inboard formula aircraft elevator
Hoistable platform rotation platform center of rotation；423rd, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track wheel
Fixed block；430th, inboard formula aircraft elevator vertical structure part；431st, mounting structure；440th, oil cylinder guide rail；460th, boots are led.
Fig. 3 is the A-A view of Fig. 1, and the structure that this structural representation have expressed negative one layer, minus two layers and minus three layers of hangar is closed
It is, and a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator and a kind of hydraulic pressure magnetic suspension aircraft carrier inboard formula fly
The installation site relation of machine elevator, simultaneously emphasis have expressed the knot of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator
Structure.
In Fig. 3,001, carrier-borne aircraft；110th, negative one layer hangar deck；111st, the warship side of a ship；112nd, warship side of a ship opening；113rd, negative one layer
Hangar aircraft delivery track；120th, minus two layers of hangar deck；130th, minus three layers of hangar deck；210th, topside formula aircraft elevator knot
Framework platform；310th, topside formula aircraft elevator hoistable platform；311st, topside formula aircraft elevator hoistable platform aircraft conveyor track
Road；400th, hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator；410th, inboard formula aircraft elevator hoistable platform；411st, the side of a ship
Interior formula aircraft elevator hoistable platform aircraft delivery track；420th, inboard formula aircraft elevator hoistable platform rotation platform；421、
Inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track；422nd, inboard formula aircraft elevator hoistable platform rotation
Platform center of rotation；430th, inboard formula aircraft elevator vertical structure part；431st, mounting structure；440th, oil cylinder guide rail；450、
Rodless piston；460th, boots are led.
Fig. 4 is the schematic diagram of magnetic suspension system structural principle of the present invention and hydraulic system principle figure.
In Fig. 4,410, inboard formula aircraft elevator hoistable platform；440th, oil cylinder guide rail；450th, rodless piston；451st, piston
Magnet；452nd, Magnet fixing body；453rd, piston Magnet roller；454th, connector；460th, boots are led；461st, lead boots Magnet；462nd, magnetic
Ferrum fixing body；463rd, lead boots Magnet roller；600th, hydraulic system；601st, oil pump；602nd, overflow valve；603rd, reversal valve；610th, oil
Case；620th, cooling system；630th, flow control system.
Fig. 5 is that the another kind of the present invention adopts double-deck or multilamellar hangar, using a kind of hydraulic pressure magnetic suspension aircraft carrier inboard
Negative one layer is connected by aircraft elevator with other each layer hangars, then uses cooperatively a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula
Aircraft elevator conveys the structural representation of each layer hangar aircraft, and in figure depicts two XISHI wire frames, and what left frame was expressed is
Negative one layer hangar deck (110) is provided with a set of negative one layer hangar rotation platform (500) schematic diagram by warship side of a ship opening (112) place,
Right frame expression is that inboard formula aircraft elevator hoistable platform (410) carries carrier-borne aircraft (001) and is in other each layer hangar first
The position view of plate (120).
In Fig. 5,001, carrier-borne aircraft；110th, negative one layer hangar deck；112nd, warship side of a ship opening；113rd, negative one layer hangar aircraft is defeated
Send track (even topside formula elevator hoistable platform)；114th, negative one layer hangar aircraft delivery track (even inboard formula elevator lifting
Platform)；120th, minus two layers of hangar deck；310th, topside formula aircraft elevator hoistable platform；311st, topside formula aircraft elevator liter
Fall platform aircraft delivery track；410th, inboard formula aircraft elevator hoistable platform；411st, inboard formula aircraft elevator hoistable platform
Aircraft delivery track；500th, negative one layer hangar rotation platform；510th, negative one layer hangar rotation platform aircraft delivery track；520th, bear
One layer of hangar rotation platform center of rotation；530th, wheel fixed block.
Fig. 6 is that the another kind of the present invention adopts double-deck or multilamellar hangar, using a kind of hydraulic pressure magnetic suspension aircraft carrier inboard
Each layer hangar is connected by through type aircraft elevator with flight-deck, and aircraft is stopped at structural representation during flight-deck.
In Fig. 6,001, carrier-borne aircraft；100th, flight-deck；400th, hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator；
410th, inboard formula aircraft elevator hoistable platform；420th, inboard formula aircraft elevator hoistable platform rotation platform；421st, inboard formula
Aircraft elevator hoistable platform rotation platform aircraft delivery track；422nd, inboard formula aircraft elevator hoistable platform rotation platform rotation
Turn center；423rd, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track wheel fixed block.
Specific embodiment
Fig. 1, Fig. 2 and Fig. 3 are a kind of a kind of real of method increasing substantially aircraft carrier carrying number of aircraft of the present invention
Apply a structural representation.
The technical solution adopted for the present invention to solve the technical problems is, using double-deck or multilamellar store structure, Ke Yi great
The big carrying quantity increasing carrier-borne aircraft；Adopt a kind of hydraulic pressure magnetic suspension aircraft carrier inboard aircraft elevator by negative one layer hangar with
And layers below hangar is connected, then coordinate using a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator, Ke Yifang
Just, safely, quickly hangar aircraft is served flight-deck.
Method-negative one layer machine that a kind of aircraft carrier hangar aircraft is rapidly feeding aircraft elevator is also applied in the present invention
The method that storehouse rotation platform coordinates aircraft delivery track, this method can be by hangar aircraft safety, accurately and rapidly feeding topside
Formula aircraft elevator hoistable platform.
Fig. 1 is in an embodiment of the present invention, and carrier-borne aircraft is conveyed by hydraulic pressure magnetic suspension aircraft carrier inboard aircraft elevator
Arrive structural representation during negative one layer hangar deck.
In Fig. 1, about the structure of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator：Topside formula aircraft elevator is tied
Framework platform (210), topside formula aircraft elevator vertical structure part (211)；Mounting structure (212), oil cylinder guide rail (213),
Hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator (300), topside formula aircraft elevator hoistable platform (310), topside formula
Boots (312) etc. led by aircraft elevator hoistable platform aircraft delivery track (311), topside formula aircraft elevator, refer to patent Shen
Please data " a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator "；Relevant negative one layer hangar aircraft delivery track
(113) structure refers to Application Data " a kind of method that aircraft carrier hangar aircraft is rapidly feeding aircraft elevator ".
Fig. 2 is in an embodiment of the present invention, and carrier-borne aircraft is conveyed by hydraulic pressure magnetic suspension aircraft carrier inboard aircraft elevator
Arrive structural representation during minus two layers of hangar deck, in figure shows oil cylinder guide rail and leads the structure of the elevator such as boots.
In Fig. 2,001, carrier-borne aircraft；111st, the warship side of a ship；120th, minus two layers of hangar deck；410th, inboard formula aircraft elevator lifting
Platform；411st, inboard formula aircraft elevator hoistable platform aircraft delivery track；420th, inboard formula aircraft elevator hoistable platform rotation
Turn platform；421st, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track；422nd, inboard formula aircraft elevator
Hoistable platform rotation platform center of rotation；423rd, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track wheel
Fixed block；430th, inboard formula aircraft elevator vertical structure part；431st, mounting structure；440th, oil cylinder guide rail；460th, boots are led.
Fig. 3 is the A-A view of Fig. 1, and the structure that this structural representation have expressed negative one layer, minus two layers and minus three layers of hangar is closed
It is, and a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator and a kind of hydraulic pressure magnetic suspension aircraft carrier inboard formula fly
The installation site relation of machine elevator, simultaneously emphasis have expressed the knot of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator
Structure.
In Fig. 3,001, carrier-borne aircraft；110th, negative one layer hangar deck；111st, the warship side of a ship；112nd, warship side of a ship opening；113rd, negative one layer
Hangar aircraft delivery track；120th, minus two layers of hangar deck；130th, minus three layers of hangar deck；210th, topside formula aircraft elevator knot
Framework platform；310th, topside formula aircraft elevator hoistable platform；311st, topside formula aircraft elevator hoistable platform aircraft conveyor track
Road；400th, hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator；410th, inboard formula aircraft elevator hoistable platform；411st, the side of a ship
Interior formula aircraft elevator hoistable platform aircraft delivery track；420th, inboard formula aircraft elevator hoistable platform rotation platform；421、
Inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track；422nd, inboard formula aircraft elevator hoistable platform rotation
Platform center of rotation；430th, inboard formula aircraft elevator vertical structure part；431st, mounting structure；440th, oil cylinder guide rail；450、
Rodless piston；460th, boots are led.
In Fig. 3, topside formula aircraft elevator structure body panel (210), topside formula aircraft elevator hoistable platform (310),
Topside formula aircraft elevator hoistable platform aircraft delivery track (311), its structure is not belonging to the application protection domain, refers to specially
Sharp application materials " a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator " and " a kind of aircraft carrier hangar aircraft is quick
The method sending into aircraft elevator ".
In Fig. 3, rodless piston (450) is upper to pass through connector, in top or the bottom of rodless piston, or top and under
Portion, has been arranged as required to piston Magnet and its Magnet roller, and its concrete structure refers to Fig. 4.
Fig. 4 is the schematic diagram of magnetic suspension system structural principle of the present invention and hydraulic system principle figure.
In Fig. 4,410, inboard formula aircraft elevator hoistable platform；440th, oil cylinder guide rail；450th, rodless piston；451st, piston
Magnet；452nd, Magnet fixing body；453rd, piston Magnet roller；454th, connector；460th, boots are led；461st, lead boots Magnet；462nd, magnetic
Ferrum fixing body；463rd, lead boots Magnet roller；600th, hydraulic system；601st, oil pump；602nd, overflow valve；603rd, reversal valve；610th, oil
Case；620th, cooling system；630th, flow control system.
Can be seen that a kind of method increasing substantially aircraft carrier carrying number of aircraft from Fig. 1, Fig. 2, Fig. 3 and Fig. 4,
Using double-deck or multilamellar store structure, cooperation adds inboard formula aircraft elevator technical scheme using topside formula aircraft elevator, its
Feature is：
Using double-deck or multilamellar store structure, between negative one layer hangar and flight-deck, adopt a kind of hydraulic pressure magnetic suspension aviation
Mother ship carrier topside formula aircraft elevator, and adopt a kind of hydraulic pressure magnetic suspension aircraft carrier from lowermost layer hangar to negative one layer hangar
Inboard formula aircraft elevator is connected；Negative one layer hangar aircraft is directly entered outboard aircraft elevator and serves flight-deck, following
The aircraft of layer hangar is transported to negative one layer hangar by inboard formula aircraft elevator and enters back into outboard aircraft elevator serves flight
Deck.
A kind of method increasing substantially aircraft carrier carrying number of aircraft as above, a kind of its hydraulic pressure magnetic used
Inboard formula aircraft elevator hoistable platform aircraft is provided with the hoistable platform of suspension aircraft carrier inboard formula aircraft elevator defeated
Send track (411) and inboard formula aircraft elevator hoistable platform rotation platform (420)；Inboard formula aircraft elevator hoistable platform rotation
Turn be provided with platform (420) inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track (421), inboard formula fly
Machine elevator hoistable platform rotation platform center of rotation (422) and inboard formula aircraft elevator hoistable platform rotation platform aircraft
Delivery track wheel fixed block (423)；Connection hoistable platform aircraft delivery track (411) is provided with negative one layer hangar deck
Negative one layer hangar aircraft delivery track (113) with hoistable platform rotation platform aircraft delivery track (421).
Increase substantially aircraft carrier in one of the above and carry a kind of hydraulic pressure magnetcisuspension used in the method for number of aircraft
Floating aircraft carrier inboard formula aircraft elevator, by hydraulic system (600), hangar vertical structure part (430), oil cylinder guide rail (440)
With inboard formula aircraft elevator hoistable platform (410) composition, it is characterized in that：This aircraft elevator is applied to bilayer or multilamellar hangar
Structure, more than lowermost layer hangar deck, each layer hangar deck is provided with the opening of elevator hoistable platform operation, this opening position
In at topside formula aircraft elevator warship side of a ship opening；Vertical structure part (430) is erected at lowermost layer hangar deck and negative one layer
Between hangar deck, two corresponding side surface of negative one layer hangar deck opening, in addition two side faces be aircraft enter hoistable platform position
Put；The structure being connected when being installed with oil cylinder guide rail (440) is had on vertical structure part；
Oil cylinder guide rail (440) cylinder body makes of nonmagnetic substance, is provided with rodless piston (450), no bar in oil cylinder guide rail
Piston Magnet (451) and piston Magnet roller (453) are provided with piston；The upper/lower terminal of oil cylinder guide rail (440) and hydraulic pressure system
System is connected, and is used as power by hydraulic system (600) and promotes rodless piston to run up and down in oil cylinder guide rail；
It is provided with inboard formula aircraft elevator hoistable platform (410) and lead boots (460)；Lead boots (460) and be arranged on oil cylinder and lead
The outside of rail (440) can be run up and down along the outer surface of oil cylinder guide rail；Lead to be provided with boots and lead boots Magnet (461) and lead boots magnetic
Ferrum roller (463)；
Lead boots Magnet (461) and the corresponding installation of piston Magnet (451) and heteropole is attracting, all lead boots Magnet (461) and live
The captivation summation (Fa) that between plug Magnet (451), institute must produce is inboard formula aircraft elevator hoistable platform (410) deadweight, load
The summation (Ga ') of lotus (aircraft must be calculated with maximum take-off weight) and various down force is multiplied by safety coefficient (Ga) again；
When hydraulic system promotes rodless piston to run up and down or stop in oil cylinder guide rail, just drive inboard formula aircraft elevator lifting
Platform (410) is followed it and is run up and down or stop.
One of the above hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator, when needs design is dedicated for personnel, force
When the hydraulic pressure magnetic suspension inboard formula personnel of device ammunition or the conveying of other goods and materials or goods and materials conveying elevator, the planar shaped of hoistable platform
Shape and size can be according to the concrete condition flexible design in place, and vertical structure part is according to the profile of hoistable platform and work need
Arrange, the traffic coverage of elevator hoistable platform can be arbitrarily devised between the aircraft carrier bottom to flight-deck, the speed of service
Can be arbitrarily devised between Ultra-Low Speed elevator and the speed of super high speed elevator, may be designed as variable-speed operation elevator form.
Hydraulic system belongs to conventional system, is designed without what special feature, has several lime lights here：
1) setting of hydraulic system pressure and flow, is the speed of service according to hoistable platform and Ga calculates and obtains.
2) lead boots Magnet (461) and the design of piston Magnet (451) needs close fit test to carry out, to obtain best effective
Fruit is it is ensured that the realization of Fa.
3) piston Magnet roller (453) and to lead boots Magnet roller (463) be that a set of safe operation ensures spare and accessory parts, design will
Conscientiously, need test, to obtain optimum efficiency more simultaneously.
Successfully key is two to a kind of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator：
1) all lead between boots Magnet (461) and piston Magnet (451) the captivation summation (Fa) that must produce guarantee have
Standby lifting Ga.
One reference data is provided here：The captivation of modern nd-fe-b magnet be enough to pick up about 640 times of its own weight
Object.
According to this reference data it is assumed that Ga is 150000Kg, then all lead boots Magnet (461) and piston Magnet
(451) theoretical gross weight should be：
150000÷640≈235Kg
The gap factor leading between boots Magnet and piston Magnet is taken to be 0.75, installation site coefficient is 0.7, then Ke Yi great
Cause show that the actual amount all leading boots Magnet (461) and piston Magnet (451) is：
235Kg÷0.75÷0.7≈480Kg
It is averagely allocated to every oil cylinder guide rail with 480Kg and lead boots Magnet and piston it is possible to draw in every oil cylinder guide rail
The weight of Magnet.
Lead the weight of boots Magnet and piston Magnet in single oil cylinder guide rail, be oil cylinder guide rail and lead boots design important according to
According to such as：Certain aircraft carrier hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator is designed with 10 oil cylinder guide rails, then single
The weight leading boots Magnet in oil cylinder guide rail with piston Magnet is accomplished by 480Kg ÷ 10=48Kg, if tied using as shown in Figure 4
Structure, the weight of piston Magnet is exactly probably 16Kg, will balance below：Which type of, with the oil cylinder of many imperial palaces warp, section, adopt
Several piston Magnet, how piston Magnet is arranged, leads how boots Magnet designs, how to arrange ....
2) lift of hydraulic system be enough to lift Ga it is believed that, Normal hydraulic engineer can complete this work.
Because design of Hydraulic System belongs to conventional system here, structure design falls within conventional structure design, and here is not
Many elaborations.
It needs to be noted that hydraulic pressure magnetic suspension system promotes the such knot of same hoistable platform for using many guide rails
Structure, has the advantage of uniqueness.
If it is known that being pushed away with 10 mechanical type pushing meanss, because its structure is fixed, it is difficult to accomplish every thrust dress
Put uniform force；
If adopting cable wire hoisting structure as conventional airplane elevator, because its every cable wire is flexible structure, no
But lifting is unstable, and cannot make its uniform force：When aircraft just goes up hoistable platform, near the hoist cable of this one end on deck
Stress is big, and other end stress is little；With the movement position change of aircraft, each stress also changes therewith, even if reaching fixing point
Position, each hoist cable stress also cannot be uniform；Belong to flexible structure because hoist cable lifts by crane, discontinuity, when hoistable platform runs
Just unstable, safety is also poor.
We are looking to be lifted by crane aircraft elevator hoistable platform with hydraulic pressure magnetic suspension system.Assume that we use 10 oil cylinders
Guide rail is used as power, the piston Magnet in each oil cylinder guide rail all corresponding thereto to lead boots Magnet tightly attracting, so that oil cylinder is led
Rail and hoistable platform are combined into the sliding motion system of a set of " quasi- rigid structure ", and that is, hoistable platform can be with the nothing in oil cylinder guide rail
Bar piston runs up and down and stops.
It is known that the captivation between permanent magnet will not suddenly disappear it might even be possible to keep its attraction for a long time
Power, guarantees the reliability combining between hoistable platform and oil cylinder guide rail and safety；On the other hand, in hydraulic system,
Although fluid can flow, hydraulic oil is Incoercibility, this guarantees hoistable platform with no bar in oil cylinder guide rail
Piston runs and the reliability stopped and safety up and down.
How we, to analyze 10 oil cylinder guide rails, are lifted to hoistable platform uniform stressed below.
10 oil cylinder guide rails are arranged in the left and right sides of elevator hangar deck opening by us, 5, every side, fore-and-aft direction
Pass in and out the position of hoistable platform for aircraft, we are respectively labeled as to the rodless piston in 10 oil cylinder guide rails：A1、B1、C1、
D1, E1 and A2, B2, C2, D2, E2, wherein A1 with A2, E1 with E2 position are corresponding.Assume that aircraft has just enter into hoistable platform, weight pressure
On A1 and A2, then, the piston Magnet on A1, A2 and B1, B2 will tightly hold its corresponding lead boots Magnet it is ensured that lifting
Platform does not move down position；And the piston Magnet of E1 and E2 position also can tightly hold its corresponding lead boots Magnet, do not allow it
Do not move up position, here it is the uniqueness of Magnet centripetal attraction characteristic, no matter you are to which direction to apply active force, it all can
Power in the opposite direction is balanced each other with you it is ensured that hoistable platform is remained substantially stationary with the relative position of rodless piston；Equally, liquid
Pressure system also has this characteristic here：When the external force direction that rodless piston is subject to is downward, hydraulic system will with pressure with
Its balance；When the external force direction that rodless piston is subject to upwards when, hydraulic system can balance (flow commutation) with pressure with it, also may be used
(when hoistable platform is stopped, liquor stream is closed, when fluid does not flow) is balanced it is ensured that lifting is flat with it with the suction of vacuum
Platform is remained substantially stationary with the relative position of rodless piston.It can be seen that, no matter how position on hoistable platform for the aircraft changes,
10 guide rail fuel tanks all " conscious " can use up the effort of oneself it is ensured that hoistable platform is stable, safe operation.
Certainly, in design system flow, need the rational speed of service determining aircraft elevator hoistable platform.Hydraulic pressure
The speed of service of magnetic suspension aircraft carrier inboard formula aircraft elevator can realize the speed of traditional aircraft carrier elevator 0.5M/s,
The high speed of achievable 2M/s or even 5M/s.The speed of service of aircraft elevator hoistable platform is the important tactical qualities of aircraft carrier, is
Strive for the important indicator of air battle time, should carefully determine as needed during design.
Each layer hangar aircraft can safely, steadily, be quickly transported to negative one layer hangar in addition it is also necessary to quickly serve below
Topside formula elevator hoistable platform, could serve flight-deck as early as possible and take off.Traditional approach is that manually operation makes airplane tail group
Be aligned warship side of a ship opening, then it is sent into hoistable platform.This operation, quality is unstable, and speed is slow, and operating personnel's working strength is big.
It is provided with inboard formula on a kind of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator hoistable platform of the present invention
Aircraft elevator hoistable platform rotation platform (420), inboard formula aircraft elevator hoistable platform rotation platform (420) is provided with
Inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track (421), the rotation of inboard formula aircraft elevator hoistable platform
Turn platform center of rotation (422) and inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track wheel fixed block
(423)；Rotation platform can drive aircraft to rotate to required angle position by center of rotation " O "；When in hoistable platform
When aircraft reaches negative one layer hangar deck position, rotation rotation platform (420) just can adjust rapidly the location fix of aircraft, makes
Airplane tail group is directed at warship side of a ship opening, carries out rapidly the preparation entering outboard aircraft elevator hoistable platform.
Fig. 5 is that the another kind of the present invention adopts double-deck or multilamellar hangar, using a kind of hydraulic pressure magnetic suspension aircraft carrier inboard
Negative one layer is connected by aircraft elevator with other each layer hangars, then uses cooperatively a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula
Aircraft elevator conveys the structural representation of each layer hangar aircraft, and in figure depicts two XISHI wire frames, and what left frame was expressed is
Negative one layer hangar deck (110) is provided with a set of negative one layer hangar rotation platform (500) schematic diagram by warship side of a ship opening (112) place,
Right frame expression is that inboard formula aircraft elevator hoistable platform (410) carries carrier-borne aircraft and is in other each layer hangar decks
(120) position view.
Fig. 5 is existed with a kind of hydraulic pressure magnetic suspension aircraft carrier inboard aircraft elevator difference of Fig. 1, Fig. 2 and Fig. 3 expression
In：Elevator is not in alignment with negative one layer hangar warship side of a ship opening in the opening of hangar, but deviate from certain distance, elevator simultaneously
Rotation platform is not had on hoistable platform；After the aircraft of negative one layer layers below hangar rises to negative one layer hangar position, move
To negative one layer hangar rotation platform, enter back into topside formula aircraft elevator and serve flight-deck.The scheme aircraft transporting velocity of Fig. 5
Slowly, management also inconvenience, but it can save hangar deck area valuable in a large number, and which kind of scheme concrete aircraft carrier adopts, and root
Select to determine according to concrete condition.
Fig. 6 is another method increasing substantially aircraft carrier carrying number of aircraft of the present invention, and one kind is using double-deck
Or multilamellar hangar, using a kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator by each layer hangar and flight-deck
One of technical scheme schematic diagram being connected, Fig. 6 is the structural representation that carrier-borne aircraft is stopped at during flight-deck, is stopped at other each layers
Schematic diagram during hangar such as Fig. 2, modular construction is shown in Fig. 4.
In Fig. 6,001, carrier-borne aircraft；100th, flight-deck；400th, hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator；
410th, inboard formula aircraft elevator hoistable platform；420th, inboard formula aircraft elevator hoistable platform rotation platform；421st, inboard formula
Aircraft elevator hoistable platform rotation platform aircraft delivery track；422nd, inboard formula aircraft elevator hoistable platform rotation platform rotation
Turn center；423rd, inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track wheel fixed block.
A kind of method increasing substantially aircraft carrier carrying number of aircraft, using a kind of hydraulic pressure magnetic suspension aircraft carrier side of a ship
Interior through type aircraft elevator technical scheme, is characterized in that：Using monolayer, double-deck or multilamellar store structure, from lowermost layer hangar
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator is adopted to be connected between flight-deck；The warship of each layer hangar
Carrier aircraft is directly entered inboard through type aircraft elevator hoistable platform in each layer hangar, flat by the lifting of through type aircraft elevator
Platform directly serves flight-deck.
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator technical scheme, both can implement multilamellar machine
Storehouse, improves the quantity that aircraft carrier carries aircraft to greatest extent, and can each layer hangar aircraft of safe and simple, quick conveying extremely fly
Row deck.
Fig. 6 and Fig. 1 scheme difference：A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator technical side
Case is that directly each layer hangar carrier-borne aircraft is served flight-deck, need not first deliver to negative one layer hangar, then with topside formula aircraft lifting and landing
Machine cooperates work that is to say, that eliminating this huge engineering project of topside formula aircraft elevator, including warship side of a ship opening, greatly
Type hydraulic cylinder, various pulley assembly, many require strict hoist cable etc., the lifting of a lot of suspension cable types will be can't see in hangar
Equipment and supporting hydraulic test；A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator technical scheme also needs
Want a set of fluid power system, but, it can be installed on any suitable position of aircraft carrier, as long as hydraulic oil pipe is guided to lifting
Oil cylinder guide rail both may be used.
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator technical scheme and traditional aircraft carrier topside
The comparison of formula aircraft elevator technical scheme：
The sharpest edges of topside formula aircraft elevator technical scheme are exactly not in flight-deck upper shed, particularly do not need
In the centre position opening of flight-deck, without compromising on the intensity of flight-deck, the integral arrangement of flight-deck will not be hindered；But
It is that topside formula aircraft elevator technical scheme, since it is desired that warship side of a ship opening, but destroys the bulk strength of the warship side of a ship.
In addition, if it is female with traditional aircraft carrier topside formula aircraft elevator technical scheme and a kind of hydraulic pressure magnetic suspension aviation
Warship inboard through type aircraft elevator technical scheme compares, its hoist cable type structure no matter safety, reliability, stability,
Operability, maintainability aspect, or speed of service aspect, are all cannot be with a kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type
Aircraft elevator technical scheme is comparable；If traditional aircraft carrier topside formula aircraft elevator technical scheme multilamellar to be realized
Store structure is highly difficult, even if having devised multilamellar store structure it is also necessary to other layer of aircraft is first delivered to negative one layer machine
Storehouse, enters back into topside formula aircraft elevator, then serves flight-deck, really less, slowly, poor, take, be unworthy！
I.e. using a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator technical scheme and a kind of hydraulic pressure magnetic suspension
Aircraft carrier inboard through type aircraft elevator technical scheme compares, and it is hung in safety, reliability, stability aspect and the side of a ship
Interior through type aircraft elevator technical scheme is suitable, but its operability, maintainability aspect, integrated operation speed aspect, still not
As through type aircraft elevator technical scheme, the maximum gap or warship side of a ship needs opening and each layer aircraft must first deliver to negative one certainly
Layer hangar, enter back into topside formula aircraft elevator, then serve flight-deck, be equally less, slowly, poor, expense, be unworthy！
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator technical scheme and traditional aircraft carrier inboard
The comparison of formula aircraft elevator technical scheme：
Traditional aircraft carrier inboard formula aircraft elevator is usually provided in the middle of flight-deck, big to deck strength infringement, no
Use beneficial to flight-deck integral arrangement, it is also difficult to realize multilamellar store structure, cable wire lifts by crane for a lot of hydraulic pressure, pulley arrangement
Not only unstable, and speed is very slow, such as adopt 3 layers of hangar, 7 meters every layer, its speed 0.5M/s, single up once will 42
Second；
Hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator may be provided at the ground any easy to use of hangar
Side, hydraulic control system also can be arranged in the idle place of hangar, and the speed of service is fast, up to 2～3M/s, is traditional aircraft carrier
The several times of aircraft elevator；As normal domestic man lift, each layer hangar can be connected to realize multilamellar hangar knot
Structure；Most of all, the structure of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator be in each layer hangar deck and
Take off and coupled together with " vertical structure part " between deck, the structure of " vertical structure part " not still installation oil cylinder guide rail,
It is also each layer deck, including " the vertical structure part " of hangar deck and flight-deck aperture position strength structure reinforcement structure, can
Make deck opening position will not make intensity that impact is greatly lowered because of opening to use, also will not be as traditional aircraft carrier inboard formula
Need like that at aircraft elevator deck opening to increase too many strength enhancing structure steel.
Feature, traditional topside formula aircraft elevator and the inboard formula aircraft elevator Yin Qian of comprehensive various aircraft elevators
Quan Xing, stability, the speed of service, maintainability, deck space using etc. everyway undesirable, only " all use " and
, so will be eliminated；Instead will be the hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft lifting and landing of latest generation
The combination such one of machine, hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator and aircraft carrier rail mounted aircraft induction system
Set technical scheme, or the hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator technical scheme of latest generation.
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator, by vertical structure part, oil cylinder guide rail, lifting
Platform and hydraulic system composition, is characterized in that：This elevator is applied to single or multiple lift store structure, opens as deck determining
The position of mouth, is designed with " the hole structure " placing hoistable platform on lowermost layer hangar deck, and " hole structure " will guarantee that lifting is flat
When platform drop to this deck, hoistable platform is consistent with altitude above deck, and the carrier-borne aircraft that " hole structure " also determines in hangar simultaneously enters
The locality going out hoistable platform is two corresponding surfaces of aircraft carrier direction of advance；
With " hole structure " corresponding position, have on each layer hangar deck and flight-deck more than lowermost layer hangar deck
Hoistable platform deck opening, the deck of opening surrounding is provided with intensity and toughness ruggedized construction；
From above lowermost layer hangar deck " hole structure " to flight-deck, the two of carrier-borne aircraft non-turnover hoistable platform
In individual corresponding sides, it is each provided with some vertical structure parts；Vertical structure part is the mounting structure of oil cylinder guide rail, is also lifting
The vertical direction structural member of Platform Deck opening strength rigidity ruggedized construction；
Oil cylinder guide rail had not only played the effect of oil cylinder but also had played the effect of track, and cylinder body makes of nonmagnetic substance, the nothing in cylinder body
Piston Magnet and piston Magnet roller are provided with bar piston；It is provided with oil cylinder guide rail and be connected with vertical structure part during installation
Installation connecting element；
Hoistable platform is up and down to transport the supporting body of aircraft to flight-deck or from flight-deck to hangar from hangar, lifting
It is provided with platform and lead boots；Lead boots nonmagnetic substance to make, lead to be provided with boots and lead boots Magnet and lead boots roller；
Lead the installation corresponding with piston Magnet of boots Magnet and heteropole is attracting, using the attraction led between boots Magnet and piston Magnet
Power makes the aircraft on hoistable platform and its hoistable platform move up and down with rodless piston and stop.
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator, is characterized in that as above：By even Access node component, in cylinder body can the top of rodless piston, bottom or upper-lower position install cover piston Magnet and itsPiston Magnet
Roller.
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator, is characterized in that as above：Lifting is flat
Aircraft rotation platform is provided with platform, rotation platform is provided with aircraft delivery track, on delivery track, setting organism is fixed
Device.
A kind of through type aircraft elevator design of hydraulic pressure magnetic suspension aircraft carrier inboard, method of manufacture and use thereof and other liquid
Pressure magnetic suspension carrier-based aircraft elevator is identical, and here no longer illustrates, only illustrates a bit here：When aircraft elevator is for many
During layer hangar, oil cylinder guide rail needs docking to extend, and designer needs comprehensively to examine in each side such as structure, intensity, leakproof, maintenances
Consider.
A kind of aircraft carrier that increases substantially carries the method for number of aircraft, a kind of hydraulic pressure magnetic suspension aircraft carrier topside formula
A kind of method that aircraft elevator and aircraft carrier hangar aircraft are rapidly feeding aircraft elevator, three patent application documents are mutual
In conjunction with according to the required size depositing aircraft, the number of plies of appropriate design hangar and size layout it is possible to make one 80,000 tons
The aircraft carrier of level carries the aircraft carrying quantity being equivalent to 10 ton aircraft carriers or even surmounts, and the aircraft ratio of each layer hangar can be made to use
Traditional topside formula aircraft elevator system is safer, more steadily, more accurately, faster mode is transported to flight-deck, also may be used
The aircraft making flight-deck is safer, more steadily, more accurately, faster return hangar, by the tactics improving my army's aircraft carrier
Performance plays positive role.
It is noted that hydraulic pressure magnetic suspension lifting machine technology is used for the defeated of personnel, weapons and ammunitions and other materials of aircraft carrier
Send, not only can be more safer than conventional elevator, more steady, more accurate, more rapid, also can save many preciousness decks for aircraft carrier
Space；If setting up a set of hydraulic pressure magnetic suspension lifting machine between from aircraft carrier deck of cellar to flight-deck, aircraft carrier personnel, force can be made
The transporting velocity of device ammunition and other materials improves 300～500% than conventional elevator！And its comfort level is just as doing
It is the same that express elevator is taken in public building.
Claims (8)
1. a kind of method increasing substantially aircraft carrier carrying number of aircraft, using double-deck or multilamellar store structure, cooperation is adopted
Add inboard formula aircraft elevator technical scheme with topside formula aircraft elevator, it is characterized in that：Using double-deck or multilamellar store structure,
A kind of hydraulic pressure magnetic suspension aircraft carrier topside formula aircraft elevator is adopted between negative one layer hangar and flight-deck, and from lowermost layer
Hangar adopts a kind of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator to be connected between negative one layer hangar；Negative one layer hangar
Aircraft is directly entered outboard aircraft elevator and serves flight-deck, and the aircraft of layers below hangar passes through inboard formula aircraft elevator
It is transported to negative one layer hangar and enters back into outboard aircraft elevator and serve flight-deck.
2. as claimed in claim 1 a kind of increase substantially aircraft carrier carry number of aircraft method, it is characterized in that：Its institute
It is provided with inboard formula aircraft elevator on a kind of hoistable platform of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator
Hoistable platform aircraft delivery track (411) and inboard formula aircraft elevator hoistable platform rotation platform (420)；Inboard formula aircraft liter
Inboard formula aircraft elevator hoistable platform rotation platform aircraft delivery track is provided with fall machine hoistable platform rotation platform (420)
(421), inboard formula aircraft elevator hoistable platform rotation platform center of rotation (422) and inboard formula aircraft elevator hoistable platform
Rotation platform aircraft delivery track wheel fixed block (423)；Connection hoistable platform aircraft is provided with negative one layer hangar deck
The negative one layer hangar aircraft delivery track of delivery track (411) and hoistable platform rotation platform aircraft delivery track (421)
(113).
3. a kind of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator, by hydraulic system (600), hangar vertical structure part
(430), oil cylinder guide rail (440) and inboard formula aircraft elevator hoistable platform (410) composition, is characterized in that：This aircraft elevator
It is applied to bilayer or multilamellar store structure, each layer hangar deck is provided with elevator hoistable platform more than lowermost layer hangar deck
The opening running, this opening is located at topside formula aircraft elevator warship side of a ship opening；Vertical structure part (430) is erected at minimum
Layer hangar deck and negative one layer hangar deck between, two corresponding side surface of negative one layer hangar deck opening, in addition two side faces are winged
Machine enters the position of hoistable platform；The structure being connected when being installed with oil cylinder guide rail (440) is had on vertical structure part；
Oil cylinder guide rail (440) cylinder body makes of nonmagnetic substance, is provided with rodless piston (450), rodless piston in oil cylinder guide rail
On be provided with piston Magnet (451) and piston Magnet roller (453)；The upper/lower terminal of oil cylinder guide rail (440) and hydraulic system phase
Even, being used as power by hydraulic system (600) promotes rodless piston to run up and down in oil cylinder guide rail；
It is provided with inboard formula aircraft elevator hoistable platform (410) and lead boots (460)；Lead boots (460) and be arranged on oil cylinder guide rail
(440) outside can be run up and down along the outer surface of oil cylinder guide rail；Lead to be provided with boots and lead boots Magnet (461) and lead boots Magnet
Roller (463)；
Lead boots Magnet (461) and the corresponding installation of piston Magnet (451) and heteropole is attracting, when hydraulic system promotes rodless piston in oil
When running up and down or stop in cylinder guide rail, just drive inboard formula aircraft elevator hoistable platform (410) follow its run up and down or
Stop.
4. a kind of hydraulic pressure magnetic suspension aircraft carrier inboard formula aircraft elevator as claimed in claim 3, is characterized in that：This hydraulic pressure
Magnetic suspension inboard aircraft elevator dedicated for personnel, weapons and ammunitions or other goods and materials conveying when, the planar shaped of hoistable platform
Shape and size can be according to the concrete condition flexible design in place, and vertical structure part is according to the profile of hoistable platform and work need
Arrange, the traffic coverage of elevator hoistable platform can be arbitrarily devised between the aircraft carrier bottom to flight-deck, the speed of service
Can be arbitrarily devised between Ultra-Low Speed elevator and the speed of super high speed elevator, may be designed as variable-speed operation elevator form.
5. a kind of method increasing substantially aircraft carrier carrying number of aircraft, using a kind of hydraulic pressure magnetic suspension aircraft carrier inboard
Through type aircraft elevator technical scheme, is characterized in that：Using monolayer, double-deck or multilamellar store structure, from lowermost layer hangar to
A kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator is adopted to be connected between flight-deck；Each layer hangar carrier-borne
Machine is directly entered inboard through type aircraft elevator hoistable platform in each layer hangar, straight by through type aircraft elevator hoistable platform
Pick flight-deck.
6. a kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator is flat by vertical structure part, oil cylinder guide rail, lifting
Platform and hydraulic system composition, is characterized in that：This elevator is applied to single or multiple lift store structure, is used as deck opening determining
Position, lowermost layer hangar deck is designed with place hoistable platform " hole structure ", " hole structure " hoistable platform to be guaranteed
When droping to this deck, hoistable platform is consistent with altitude above deck, and " hole structure " also determines the carrier-borne aircraft turnover in hangar simultaneously
The locality of hoistable platform is two corresponding surfaces of aircraft carrier direction of advance；
With " hole structure " corresponding position, have lifting on each layer hangar deck and flight-deck more than lowermost layer hangar deck
Platform Deck opening, the deck of opening surrounding is provided with intensity and toughness ruggedized construction；
From above lowermost layer hangar deck " hole structure " to flight-deck, two in carrier-borne aircraft non-turnover hoistable platform right
Answer on side, be each provided with some vertical structure parts；Vertical structure part is the mounting structure of oil cylinder guide rail, is also hoistable platform
The vertical direction structural member of deck opening intensity and toughness ruggedized construction；
Oil cylinder guide rail had not only played the effect of oil cylinder but also had played the effect of track, and cylinder body makes of nonmagnetic substance, and the no bar in cylinder body is lived
Piston Magnet and piston Magnet roller are installed beyond the Great Wall；The peace being connected with vertical structure part during installation is provided with oil cylinder guide rail
Load fitting；
Hoistable platform is up and down to transport the supporting body of aircraft, hoistable platform to flight-deck or from flight-deck to hangar from hangar
On be provided with and lead boots；Lead boots nonmagnetic substance to make, lead to be provided with boots and lead boots Magnet and lead boots roller；
Lead the installation corresponding with piston Magnet of boots Magnet and heteropole is attracting, made using leading the captivation between boots Magnet and piston Magnet
Aircraft on hoistable platform and its hoistable platform moves up and down with rodless piston and stops.
7. a kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator as claimed in claim 6, is characterized in that：Logical
Cross connection member, in cylinder body, in the top of rodless piston, bottom or upper-lower position, many set piston Magnet and its piston can be installed
Magnet roller.
8. a kind of hydraulic pressure magnetic suspension aircraft carrier inboard through type aircraft elevator as claimed in claim 6, is characterized in that：Rise
It is provided with aircraft rotation platform on fall platform, rotation platform is provided with aircraft delivery track, delivery track arranges organism
Fixing device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510602993.4A CN106428601A (en) | 2015-09-11 | 2015-09-11 | Method for greatly increasing number of aircrafts picked up by aircraft carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510602993.4A CN106428601A (en) | 2015-09-11 | 2015-09-11 | Method for greatly increasing number of aircrafts picked up by aircraft carrier |
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| Publication Number | Publication Date |
|---|---|
| CN106428601A true CN106428601A (en) | 2017-02-22 |
Family
ID=58093978
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510602993.4A Pending CN106428601A (en) | 2015-09-11 | 2015-09-11 | Method for greatly increasing number of aircrafts picked up by aircraft carrier |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107554809A (en) * | 2017-09-11 | 2018-01-09 | 荆门创佳机械科技有限公司 | Aircraft carrier hoistable platform based on linear electric motors driving |
| KR20230026809A (en) | 2021-08-18 | 2023-02-27 | 양동규 | Ship |
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| GB413773A (en) * | 1933-02-07 | 1934-07-26 | Charles Frobisher | Improvements in and relating to elevated centrally pivoted rotating aerodromes or airport landing grounds |
| US4084215A (en) * | 1977-02-25 | 1978-04-11 | The United States Of America As Represented By The Secretary Of The Navy | Strobe light having reduced electromagnetic radiation |
| CN2592511Y (en) * | 2002-06-24 | 2003-12-17 | 郭宏斌 | Aircraft carrie with extra-high availability factor |
| CN2782555Y (en) * | 2004-12-21 | 2006-05-24 | 傅德俐 | Aircraft carrier |
| CN103303488A (en) * | 2013-07-08 | 2013-09-18 | 谯世龙 | Airplane catapult system accelerated by magnetic suspension power platform deck for aircraft carrier |
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2015
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB413773A (en) * | 1933-02-07 | 1934-07-26 | Charles Frobisher | Improvements in and relating to elevated centrally pivoted rotating aerodromes or airport landing grounds |
| US4084215A (en) * | 1977-02-25 | 1978-04-11 | The United States Of America As Represented By The Secretary Of The Navy | Strobe light having reduced electromagnetic radiation |
| CN2592511Y (en) * | 2002-06-24 | 2003-12-17 | 郭宏斌 | Aircraft carrie with extra-high availability factor |
| CN2782555Y (en) * | 2004-12-21 | 2006-05-24 | 傅德俐 | Aircraft carrier |
| CN103303488A (en) * | 2013-07-08 | 2013-09-18 | 谯世龙 | Airplane catapult system accelerated by magnetic suspension power platform deck for aircraft carrier |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107554809A (en) * | 2017-09-11 | 2018-01-09 | 荆门创佳机械科技有限公司 | Aircraft carrier hoistable platform based on linear electric motors driving |
| KR20230026809A (en) | 2021-08-18 | 2023-02-27 | 양동규 | Ship |
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