CN107685844A - Multi-functional aircraft carrier - Google Patents
Multi-functional aircraft carrier Download PDFInfo
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- CN107685844A CN107685844A CN201710562408.1A CN201710562408A CN107685844A CN 107685844 A CN107685844 A CN 107685844A CN 201710562408 A CN201710562408 A CN 201710562408A CN 107685844 A CN107685844 A CN 107685844A
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- plate
- underriding
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- lower decks
- hull
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G11/00—Aircraft carriers
-
- 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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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Auxiliary Methods And Devices For Loading And Unloading (AREA)
Abstract
The present invention relates to a kind of multi-functional aircraft carrier, belong to ship domain, including hull, upper deck and lower decks are set from top to bottom on hull, upper deck is fixedly connected with lower decks both sides by ship wall, upper deck and lower decks head end are upturned, flight range is respectively provided with upper deck and lower decks and shuts down region, the flight range position of upper deck and lower decks corresponds to up and down, dive mouth on being set on upper deck, upper underriding mouth edge is hinged over underriding plate, upper underriding plate and upper underriding mouth dimensional fits, can interception guided missile to a certain extent attack, and it is not easy to be found；With upper and lower two layers of flight-deck, it is damaged even if upper strata flight-deck and does not also interfere with the takeoff and landing of aircraft, while bigger space is reserved to upper strata flight-deck.
Description
Technical field
The present invention relates to a kind of multi-functional aircraft carrier, belong to ship domain.
Background technology
Aircraft carrier, referred to as " aircraft carrier ", it is a kind of large-scale water surface naval vessels using carrier-borne aircraft as primary armament, warship can be provided
The takeoff and landing of carrier aircraft.Aircraft carrier is one of most huge, weapon that most complicated, power is most strong in the world.It generally possesses
Huge flight-deck and warship island, warship island are seated starboard mostly.It is usually the core naval vessel of an aircraft-carrier battle group, fleet
In other warships provide protection and supply for it, and aircraft carrier then provides air umbrella and long-range strike.But the inferior position of aircraft carrier
It is also obvious that aircraft carrier is sufficiently bulky, easily it is found, mobility is poor, is easily found and is attacked；Once the flight of aircraft carrier
Deck is damaged, and other aircrafts will be unable to land, and loss is huge；When meeting with huge stormy waves, the stability of aircraft carrier can receive shadow
Ring, and then cause flight-deck to play pendulum, the especially nightlanding that lands to fighter plane causes very big difficulty；Although aircraft carrier is all
With run-up device, but for the big fighter plane of large aircraft, extension bullet amount, because weight is big, run-up device can not carry
For enough thrust, its difficulty of taking off is caused；The flight-deck of fighter plane takeoff and landing should be provided on aircraft carrier, again
It is provided for temporarily stopping the warship island of aircraft, the space that fighter plane is used for takeoff and landing is limited, also increases driving for pilot
Sail difficulty.
The content of the invention
Deficiency of the prior art, the technical problem to be solved in the present invention are more than：A kind of multi-functional aircraft carrier is provided,
With protection network, can interception guided missile to a certain extent attack, and be not easy to be found；With upper and lower two layers of flight-deck,
It is damaged even if upper strata flight-deck and does not also interfere with the takeoff and landing of aircraft, while is reserved to upper strata flight-deck bigger
Space, when meeting with huge stormy waves, aircraft carrier can connect other escort vessels, reduce influence of the stormy waves to aircraft carrier, navigation light from
Protection network directive flight-deck, is not easy to be found by enemy；Acceleration is provided during by aircraft gravity to aircraft run-up, is improved winged
Initial velocity when machine takes off, be advantageous to take off.
Multi-functional aircraft carrier of the present invention, including hull, upper deck and lower decks, upper first are set from top to bottom on hull
Plate is fixedly connected with lower decks both sides by ship wall, and upper deck and lower decks head end are upturned, on upper deck and lower decks
It is respectively provided with flight range and shuts down region, the flight range position of upper deck and lower decks corresponds to up and down, is set on upper deck
Underriding mouth, upper underriding mouth edge are hinged over underriding plate, upper underriding plate and upper underriding mouth dimensional fits, and upper underriding plate end, which is fixed, matches somebody with somebody
Plywood, matching board are fixed on underriding plate bottom surface, and matching board both sides bar that is articulated and connected one end, the connecting rod other end is hinged on
On the piston rod of upper hydraulic cylinder, the piston rod of upper hydraulic cylinder coordinates in sliding sleeve, and sliding sleeve is fixed on upper deck bottom surface, upper liquid
Cylinder pressure is fixed on upper deck bottom surface, sets nutation to blurt out on lower decks, and nutation is blurted out the be hinged lower underriding platform in edge, nutation
Rush platform and nutation is blurted out dimensional fits, hull both sides set escort vessel, and escort vessel deck is concordant with deck in ship structure, on escort vessel
Fixing tightwire in fixation, cable wire end connection protection network are fixedly connected with hydrogen balloon on protection network, hydrogen balloon by protection network pull-up,
Protection network is located above hull.
Operation principle and process：
Including hull, upper deck and lower decks are set from top to bottom, upper deck and lower decks both sides pass through ship wall on hull
It is fixedly connected, upper deck and lower decks head end are upturned, and flight range and parking area are respectively provided with upper deck and lower decks
The flight range position of domain, upper deck and lower decks corresponds to up and down, the mouth that dives is set on upper deck, upper underriding mouth edge is hinged
Upper underriding plate, upper underriding plate and upper underriding mouth dimensional fits, upper underriding plate end secure fit plate, matching board are fixed on underriding
On plate bottom surface, matching board both sides bar that is articulated and connected one end, the connecting rod other end is hinged on the piston rod of hydraulic cylinder, upper liquid
The piston rod of cylinder pressure coordinates in sliding sleeve, and sliding sleeve is fixed on upper deck bottom surface, and upper hydraulic cylinder is fixed on upper deck bottom surface
On, set nutation to blurt out on lower decks, nutation edge of blurting out is hinged nutation punching, and nutation punching and nutation are blurted out dimensional fits,
Fighter plane dives downwards from upper underriding plate, accelerates in the effect of acceleration of gravity, then falls on nutation punching, then from Xia Jia
Plate takes off, and improves the initial velocity that fighter plane takes off, and beneficial to taking off, reduces accident.With upper and lower two layers of flight-deck, i.e.,
Upper strata flight-deck is damaged and also do not interfere with the takeoff and landing of aircraft, while reserve to upper strata flight-deck bigger
Space, hull both sides set escort vessel, and upper fixing tightwire, cable wire end connection protection network, protection network are fixed on escort vessel
On be fixedly connected with hydrogen balloon, by protection network pull-up, protection network is located above hull hydrogen balloon, and protection network can block to a certain extent
The attack of guided missile is cut, and is not easy to be found.
Both sides upper and lower ends are respectively mounted sprocket wheel on the inside of ship wall, and the sprocket wheel of homonymy is connected by chain drive, sprocket wheel and lifting
Motor 37 is connected, and lifting motor is fixed on lower decks, including lifter plate, and lifter plate both ends are fixed on chain, upper first
The position that lifter plate is corresponded on plate sets lift span, and lift span coordinates with lifter plate, and fighter plane can be by lifter plate in Shang Jia
Transported between plate and lower decks, improve operational efficiency, while lift span coordinates with lifter plate, does not interfere with the smooth of upper deck
Degree.
Lifter plate both sides inclined-plane is in ramped shaped, and the inside edge of lift span is the inclined-plane being engaged with lifter plate slope, is prevented
Gap is only left between lifter plate and lift span, causes fighter plane to jolt, while after lifter plate drops to lower decks, slope can
To facilitate aircraft to be driven off from lifter plate.
Invisible coating is coated on protection network, can absorbing radar wave, avoid being found, setting signal on protection network lower surface
Lamp, signal lamp are pointed into upper deck, and the fighter plane that can give to land provides guide, will be exploded after guided missile contact protection network,
Protection network can play a part of interception guided missile, prevent that guided missile from directly destroying hull, stationary airfoil on protection network, if wind-force mistake
Greatly, can be sailed with the wind using aerofoil, aerofoil plays a part of sail.
Including run-up motor, run-up machine shaft is connected by infinitely variable transmission and transfer roller, and transfer roller is arranged on lower first
On plate bottom surface, be wound with rope on transfer roller, cable end fixed hook sets mounting hole on lower decks, in mounting hole installation slide
Wheel, pulley upper end are not higher than lower decks upper surface, and rope is hooked in airplane tail group after bypassing pulley by linking up with.
Lower underriding platform includes cell board, and cell board edge sets breach, and the indentation, there of cell board sets pin, adjacent
Cell board head and the tail it is be hinged, including connecting plate, bar hole, pin insertion bar hole are set on connecting plate, connecting plate coordinates in phase
The indentation, there of adjacent cell board, connecting plate do not protrude from the side of cell board, the thickness of connecting plate and the consistency of thickness of cell board, under
The piston rod of lower hydraulic cylinder is hinged on the cell board bottom surface of underriding platform head end, lower hydraulic cylinder is fixed on hull.
Hull afterbody is hinged tripod, tripod end fixed hook, fixes link in the front end of other naval vessels, hook with
Link coordinates, and hook realizes the end to end of hull and other naval vessels after hooking on link.
Lower decks tail end both sides vertical columns, guide rail is fixed on column, rack is set on working face of guide rail, including is extended
Plate, the installation of extension plate end both sides extend gear, extend gear and coordinate in guide rail and engaged with rack, on extension plate bottom surface
It is fixed to extend motor, extend motor and extension plate bottom fixation balloon, air bag tracheae are connected with extending gear drive by belt pulley
Connect air pump.
The possessed compared with prior art beneficial effect of the present invention is：
Multi-functional aircraft carrier of the present invention, the mouth that dives is set on upper deck, upper underriding mouth edge is hinged over underriding plate,
Upper underriding plate and upper underriding mouth dimensional fits, upper underriding plate end secure fit plate, matching board are fixed on underriding plate bottom surface
On, matching board both sides bar that is articulated and connected one end, the connecting rod other end is hinged on the piston rod of hydraulic cylinder, the work of upper hydraulic cylinder
Stopper rod coordinates in sliding sleeve, and sliding sleeve is fixed on upper deck bottom surface, and upper hydraulic cylinder is fixed on upper deck bottom surface, lower decks
Upper setting nutation is blurted out, and nutation edge of blurting out is hinged nutation punching, and nutation punching and nutation are blurted out dimensional fits, and fighter plane is from upper
Underriding plate dives downwards, accelerates in the effect of acceleration of gravity, then falls on nutation punching, then taken off from lower decks, carried
The initial velocity that high fighter plane takes off, beneficial to taking off, reduces accident.With upper and lower two layers of flight-deck, even if upper strata flies
Row deck is damaged and does not also interfere with the takeoff and landing of aircraft, while bigger space, ship are reserved to upper strata flight-deck
Body both sides set escort vessel, and escort vessel deck is concordant with deck in ship structure, can escort aircraft landing in Emergency time
On warship, aircraft can be transferred to from the deck of aircraft carrier on escort vessel, fixed upper fixing tightwire, the connection of cable wire end on escort vessel
Protection network, hydrogen balloon is fixedly connected with protection network, hydrogen balloon is by protection network pull-up, and protection network is located above hull, and protection network can
With the attack of interception guided missile to a certain extent, and it is not easy to be found.
Both sides upper and lower ends are respectively mounted sprocket wheel on the inside of ship wall, and the sprocket wheel of homonymy is connected by chain drive, sprocket wheel and lifting
Motor 37 is connected, and lifting motor is fixed on lower decks, including lifter plate, and lifter plate both ends are fixed on chain, upper first
The position that lifter plate is corresponded on plate sets lift span, and lift span coordinates with lifter plate, and fighter plane can be by lifter plate in Shang Jia
Transported between plate and lower decks, improve operational efficiency, while lift span coordinates with lifter plate, does not interfere with the smooth of upper deck
Degree.
Lifter plate both sides inclined-plane is in ramped shaped, and the inside edge of lift span is the inclined-plane being engaged with lifter plate slope, is prevented
Gap is only left between lifter plate and lift span, causes fighter plane to jolt, while after lifter plate drops to lower decks, slope can
To facilitate aircraft to be driven off from lifter plate.
Invisible coating is coated on protection network, can absorbing radar wave, avoid being found, setting signal on protection network lower surface
Lamp, signal lamp are pointed into upper deck, and the fighter plane that can give to land provides guide.
Including run-up motor, run-up machine shaft is connected by infinitely variable transmission and transfer roller, and transfer roller is arranged on lower first
On plate bottom surface, be wound with rope on transfer roller, cable end fixed hook sets mounting hole on lower decks, in mounting hole installation slide
Wheel, pulley upper end are not higher than lower decks upper surface, and rope is hooked in airplane tail group after bypassing pulley by linking up with.
Lower underriding platform includes cell board, and cell board edge sets breach, and the indentation, there of cell board sets pin, adjacent
Cell board head and the tail it is be hinged, including connecting plate, bar hole, pin insertion bar hole are set on connecting plate, connecting plate coordinates in phase
The indentation, there of adjacent cell board, connecting plate do not protrude from the side of cell board, the thickness of connecting plate and the consistency of thickness of cell board, under
The piston rod of lower hydraulic cylinder is hinged on the cell board bottom surface of underriding platform head end, lower hydraulic cylinder is fixed on hull.
Hull afterbody is hinged tripod, tripod end fixed hook, fixes link in the front end of other naval vessels, hook with
Link coordinates, and hook realizes the end to end of hull and other naval vessels after hooking on link.
Lower decks tail end both sides vertical columns, guide rail is fixed on column, rack is set on working face of guide rail, including is extended
Plate, the installation of extension plate end both sides extend gear, extend gear and coordinate in guide rail and engaged with rack, on extension plate bottom surface
It is fixed to extend motor, extend motor and extension plate bottom fixation balloon, air bag tracheae are connected with extending gear drive by belt pulley
Connect air pump.
Brief description of the drawings
Fig. 1 is schematic diagram of the embodiment of the present invention；
Fig. 2 is embodiment illustrated in fig. 1 part A partial enlarged drawing；
Fig. 3 is embodiment illustrated in fig. 1 part B partial enlarged drawing；
Fig. 4 is embodiment illustrated in fig. 1 left view；
Fig. 5 is embodiment illustrated in fig. 4 C portion partial enlarged drawing；
Fig. 6 is embodiment illustrated in fig. 4 D parts partial enlarged drawing；
Fig. 7 is the structural representation of extension plate；
Fig. 8 is the right view of embodiment illustrated in fig. 7 extension plate.
In figure：1st, hydrogen balloon；2nd, protection network；3rd, cable wire；4th, tripod；5th, chain；6th, lifter plate；7th, lower decks；8th, ship
Body；9th, escort vessel；10th, lift span；11st, upper underriding plate；12nd, upper underriding mouth；13rd, matching board；14th, upper deck；15th, connecting rod；
16th, sliding sleeve；17th, upper hydraulic cylinder；18th, link up with；19th, column；20th, pulley；21st, run-up motor 21；22nd, rope；23rd, cell board；
24th, nutation is blurted out；25th, lower hydraulic cylinder；26th, sprocket wheel；27th, pin；28th, infinitely variable transmission；29th, extension plate；30th, gear is extended；
31st, belt pulley；32nd, motor is extended；33rd, air bag；34th, guide rail；35th, rack；36th, connecting plate；37th, lifting motor；38th, transfer roller
38。
Embodiment
Embodiments of the invention are described further below in conjunction with the accompanying drawings：
As Figure 1-Figure 8, multi-functional aircraft carrier of the present invention, including hull 8, set from top to bottom on hull 8
Deck 14 and lower decks 7, upper deck 14 and the both sides of lower decks 7 are fixedly connected by ship wall, and upper deck 14 and the head end of lower decks 7 are equal
It is upturned, flight range is respectively provided with upper deck 14 and lower decks 7 and shuts down region, the flight of upper deck 14 and lower decks 7
Regional location corresponds to up and down, underriding mouth 12 is set on upper deck 14, the upper edge of underriding mouth 12 is hinged over underriding plate 11, upper underriding
Plate 11 and the upper dimensional fits of underriding mouth 12, the upper end secure fit plate 13 of underriding plate 11, matching board 13 is fixed on underriding plate 11
On bottom surface, the one end of 13 both sides bar that is articulated and connected of matching board 15, the other end of connecting rod 15 is hinged on the piston rod of hydraulic cylinder 17
On, the piston rod of upper hydraulic cylinder 17 coordinates in sliding sleeve 16, and sliding sleeve 16 is fixed on the bottom surface of upper deck 14, and upper hydraulic cylinder 17 is solid
It is scheduled on the bottom surface of upper deck 14, sets nutation to blurt out 24 on lower decks 7, nutation is blurted out the be hinged lower underriding platform in 24 edges, under
Underriding platform and nutation are blurted out 24 dimensional fits, and the both sides of hull 8 set escort vessel 9, and the deck of escort vessel 9 is concordant with the deck of hull 8,
Fixed upper fixing tightwire 3, the end of cable wire 3 connect protection network 2, hydrogen balloon 1, hydrogen balloon are fixedly connected with protection network 2 on escort vessel 9
1 by the pull-up of protection network 2, and protection network 2 is located at the top of hull 8.
Operation principle and process：
Including hull 8, upper deck 14 and lower decks 7, upper deck 14 and the both sides of lower decks 7 are set from top to bottom on hull 8
It is fixedly connected by ship wall, upper deck 14 and the head end of lower decks 7 are upturned, and are respectively provided with upper deck 14 and lower decks 7 winged
The flight range position of row region and shutdown region, upper deck 14 and lower decks 7 corresponds to up and down, sets and dives on upper deck 14
Mouth 12, the upper edge of underriding mouth 12 is hinged over underriding plate 11, upper underriding plate 11 and the upper dimensional fits of underriding mouth 12, the upper end of underriding plate 11
Portion's secure fit plate 13, matching board 13 are fixed on the bottom surface of underriding plate 11, the one end of 13 both sides bar that is articulated and connected of matching board 15,
The other end of connecting rod 15 is hinged on the piston rod of hydraulic cylinder 17, and the piston rod of upper hydraulic cylinder 17 coordinates in sliding sleeve 16, sliding
Set 16 is fixed on the bottom surface of upper deck 14, and upper hydraulic cylinder 17 is fixed on the bottom surface of upper deck 14, and nutation is set on lower decks 7
Blurt out 24, nutation 24 edges of blurting out are hinged nutation punching, and nutation punching and nutation are blurted out 24 dimensional fits, and fighter plane is from upper underriding
Plate 11 dives downwards, accelerates in the effect of acceleration of gravity, then falls on nutation punching, then taken off from lower decks 7, improves
The initial velocity that fighter plane takes off, beneficial to taking off, reduces accident.With upper and lower two layers of flight-deck, even if upper strata is flown
Deck is damaged and does not also interfere with the takeoff and landing of aircraft, while bigger space is reserved to upper strata flight-deck, hull 8
Both sides set escort vessel 9, fixed upper fixing tightwire 3 on escort vessel 9, the end of cable wire 3 connection protection network 2, solid on protection network 2
Surely hydrogen balloon 1 is connected, hydrogen balloon 1 is by the pull-up of protection network 2, and protection network 2 is located at the top of hull 8, and protection network 2 can be to a certain extent
The attack of interception guided missile, and be not easy to be found.
Both sides upper and lower ends are respectively mounted sprocket wheel 26 on the inside of ship wall, and the sprocket wheel 26 of homonymy is connected by chain 5, sprocket wheel 26
It is connected with lifting motor 37, lifting motor 37 is fixed on lower decks 7, including lifter plate 6, and the both ends of lifter plate 6 are fixed on
On chain 5, the position that lifter plate 6 is corresponded on upper deck 14 sets lift span 10, and lift span 10 coordinates with lifter plate 6, fighter plane
It can be transported by lifter plate 6 between upper deck 14 and lower decks 7, improve operational efficiency, while lift span 10 and lifting
Plate 6 coordinates, and does not interfere with the flatness of upper deck 14.
The both sides inclined-plane of lifter plate 6 is in ramped shaped, and the inside edge of lift span 10 is oblique to be engaged with the slope of lifter plate 6
Face, prevent from leaving gap between lifter plate 6 and lift span 10, cause fighter plane to jolt, while when lifter plate 6 drops to lower decks
After 7, slope can facilitate aircraft to be driven off from lifter plate 6.
Coat invisible coating on protection network 2, can absorbing radar wave, avoid being found, on the lower surface of protection network 2 set letter
Signal lamp, signal lamp are pointed into upper deck 14, and the fighter plane that can give to land provides guide, will after guided missile contact protection network 2
Blast, protection network 2 can play a part of interception guided missile, prevent that guided missile from directly destroying hull 8, stationary airfoil on protection network 2, such as
Fruit wind-force is excessive, can be sailed with the wind using aerofoil, aerofoil plays a part of sail.
Including run-up motor 21, the rotating shaft of run-up motor 21 is connected by infinitely variable transmission 28 and transfer roller 38, transfer roller 38
On the bottom surface of lower decks 7, rope 22 is wound with transfer roller 38, the end fixed hook 18 of rope 22, peace is set on lower decks 7
Hole is filled, pulley 20 is installed in mounting hole, the upper end of pulley 20 is not higher than the upper surface of lower decks 7, and rope 22 passes through after bypassing pulley 20
Hook 18 is hooked in airplane tail group.
Lower underriding platform includes cell board 23, and the edge of cell board 23 sets breach, and the indentation, there of cell board 23 sets pin
Post 27, adjacent cell board 23 is hinged from beginning to end, including connecting plate 36, and bar hole is set on connecting plate 36, and pin 27 inserts bar shaped
Hole, connecting plate 36 coordinate the indentation, there in adjacent cells plate 23, and connecting plate 36 does not protrude from the side of cell board 23, connecting plate 36
Thickness and cell board 23 consistency of thickness, the work of lower hydraulic cylinder 25 is hinged on the bottom surface of cell board 23 of lower underriding platform head end
Stopper rod, lower hydraulic cylinder 25 are fixed on hull 8.
The afterbody of hull 8 is hinged tripod 4, the end fixed hook 18 of tripod 4, link is fixed in the front end of other naval vessels,
Hook 18 coordinates with link, and hook 18 realizes the end to end of hull 8 and other naval vessels after hooking on link.
The tail end both sides vertical columns 19 of lower decks 7, guide rail 34 is fixed on column 19, rack is set on the working face of guide rail 34
35, including extension plate 29, the end both sides of extension plate 29 installation extension gear 30, extend gear 30 and coordinate and and tooth interior in guide rail 34
Bar 35 engages, fixed on the bottom surface of extension plate 29 to extend motor 32, extends motor 32 and is passed by belt pulley 31 with extending gear 30
The dynamic connection bottom fixation balloon 33 of extension plate 29, the tracheae of air bag 33 connection air pump.
Claims (8)
- A kind of 1. multi-functional aircraft carrier, it is characterised in that：Including hull (8), set from top to bottom on hull (8) upper deck (14) and Lower decks (7), upper deck (14) and lower decks (7) both sides are fixedly connected by ship wall, upper deck (14) and lower decks (7) head end It is upturned, flight range is respectively provided with upper deck (14) and lower decks (7) and shuts down region, upper deck (14) and lower decks (7) flight range position corresponds to up and down, underriding mouth (12) is set on upper deck (14), upper underriding mouth (12) edge is hinged over Underriding plate (11), upper underriding plate (11) and upper underriding mouth (12) dimensional fits, upper underriding plate (11) end secure fit plate (13), Matching board (13) is fixed on underriding plate (11) bottom surface, matching board (13) both sides bar that is articulated and connected (15) one end, connecting rod (15) other end is hinged on the piston rod of hydraulic cylinder (17), and the piston rod of upper hydraulic cylinder (17) coordinates in sliding sleeve (16), Sliding sleeve (16) is fixed on upper deck (14) bottom surface, and upper hydraulic cylinder (17) is fixed on upper deck (14) bottom surface, lower decks (7) nutation is set to blurt out (24) on, nutation is blurted out the be hinged lower underriding platform in (24) edge, and lower underriding platform and nutation are blurted out (24) Dimensional fits, hull (8) both sides set escort vessel (9), and escort vessel (9) deck is concordant with hull (8) deck, on escort vessel (9) Fixing tightwire (3) in fixation, cable wire (3) end connect protection network (2), hydrogen balloon (1), hydrogen are fixedly connected with protection network (2) By protection network (2) pull-up, protection network (2) is located above hull (8) ball (1).
- 2. multi-functional aircraft carrier according to claim 1, it is characterised in that：Both sides upper and lower ends are respectively mounted sprocket wheel on the inside of ship wall (26), the sprocket wheel (26) of homonymy is connected by chain (5), and sprocket wheel (26) is connected with lifting motor, and lifting motor is solid It is scheduled on lower decks (7), including lifter plate (6), lifter plate (6) both ends are fixed on chain (5), it is corresponding on upper deck (14) to rise The position for dropping plate (6) sets lift span (10), and lift span (10) coordinates with lifter plate (6).
- 3. multi-functional aircraft carrier according to claim 2, it is characterised in that：Lifter plate (6) both sides inclined-plane is in ramped shaped, lifting The inside edge in hole (10) is the inclined-plane being engaged with lifter plate (6) slope.
- 4. multi-functional aircraft carrier according to claim 3, it is characterised in that：Protection network coats invisible coating on (2), can inhale Radar wave is received, avoids being found, setting signal lamp on protection network (2) lower surface, signal lamp is pointed into upper deck (14).
- 5. multi-functional aircraft carrier according to claim 4, it is characterised in that：Including run-up motor (21), run-up motor (21) Rotating shaft is connected by infinitely variable transmission (28) and transfer roller (38), and transfer roller (38) is arranged on lower decks (7) bottom surface, transfer roller (38) it is wound with rope (22) on, rope (22) end fixed hook (18) sets mounting hole on lower decks (7), in mounting hole Pulley (20) is installed, pulley (20) upper end is not higher than lower decks (7) upper surface, and rope (22) passes through hook after bypassing pulley (20) (18) hook in airplane tail group.
- 6. multi-functional aircraft carrier according to claim 5, it is characterised in that：Lower underriding platform includes cell board (23), unit Plate (23) edge sets breach, and the indentation, there of cell board (23) sets pin (27), and adjacent cell board (23) head and the tail are be hinged, Including connecting plate (36), bar hole, pin (27) insertion bar hole are set, connecting plate (36) coordinates adjacent on connecting plate (36) The indentation, there of cell board (23), connecting plate (36) do not protrude from the side of cell board (23), the thickness and unit of connecting plate (36) The consistency of thickness of plate (23), the piston rod of lower hydraulic cylinder (25) is hinged on cell board (23) bottom surface of lower underriding platform head end, Lower hydraulic cylinder (25) is fixed on hull (8).
- 7. multi-functional aircraft carrier according to claim 6, it is characterised in that：Hull (8) afterbody is hinged tripod (4), triangle Frame (4) end fixed hook (18), link is fixed in the front end of other naval vessels, and hook (18) coordinates with link.
- 8. multi-functional aircraft carrier according to claim 7, it is characterised in that：Lower decks (7) tail end both sides vertical columns (19), Guide rail (34) is fixed on column (19), rack (35), including extension plate (29), extension plate (29) are set on guide rail (34) working face The installation of end both sides extends gear (30), extends gear (30) and coordinates in guide rail (34) and engaged with rack (35), extension plate (29) it is fixed on bottom surface to extend motor (32), extend motor (32) and be connected by belt pulley (31) with extending gear (30) Extension plate (29) bottom fixation balloon (33), air bag (33) tracheae connection air pump.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710562408.1A CN107685844B (en) | 2017-07-11 | 2017-07-11 | Multi-functional aircraft carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710562408.1A CN107685844B (en) | 2017-07-11 | 2017-07-11 | Multi-functional aircraft carrier |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107685844A true CN107685844A (en) | 2018-02-13 |
| CN107685844B CN107685844B (en) | 2019-03-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710562408.1A Active CN107685844B (en) | 2017-07-11 | 2017-07-11 | Multi-functional aircraft carrier |
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| Country | Link |
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| CN (1) | CN107685844B (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4325317A (en) * | 1979-11-08 | 1982-04-20 | Wilford E Burke | Aircraft carrier |
| NL1032548C2 (en) * | 2006-09-20 | 2008-03-21 | Azure Naval Architects B V | Yacht, includes aircraft hanger inside space defined by hull and superstructure |
| CN201437404U (en) * | 2009-04-08 | 2010-04-14 | 王石诚 | Aircraft carrier with dual-layer flight deck concept |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
| CN103144753A (en) * | 2013-03-28 | 2013-06-12 | 吴德安 | Multilayer lifting deck for aircraft carrier |
| CN203047533U (en) * | 2012-08-31 | 2013-07-10 | 赵天烁 | Slope-gliding launching platform for shipboard aircraft, and application aircraft carrier |
| CN103863537A (en) * | 2012-12-12 | 2014-06-18 | 芦正安 | Aircraft carrier hull with double-deck flight deck |
| CN203975236U (en) * | 2014-07-21 | 2014-12-03 | 韦茂亮 | The runway device that slope underriding Xiang row auxiliary ship carrier aircraft is taken off |
-
2017
- 2017-07-11 CN CN201710562408.1A patent/CN107685844B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4325317A (en) * | 1979-11-08 | 1982-04-20 | Wilford E Burke | Aircraft carrier |
| NL1032548C2 (en) * | 2006-09-20 | 2008-03-21 | Azure Naval Architects B V | Yacht, includes aircraft hanger inside space defined by hull and superstructure |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
| CN201437404U (en) * | 2009-04-08 | 2010-04-14 | 王石诚 | Aircraft carrier with dual-layer flight deck concept |
| CN203047533U (en) * | 2012-08-31 | 2013-07-10 | 赵天烁 | Slope-gliding launching platform for shipboard aircraft, and application aircraft carrier |
| CN103863537A (en) * | 2012-12-12 | 2014-06-18 | 芦正安 | Aircraft carrier hull with double-deck flight deck |
| CN103144753A (en) * | 2013-03-28 | 2013-06-12 | 吴德安 | Multilayer lifting deck for aircraft carrier |
| CN203975236U (en) * | 2014-07-21 | 2014-12-03 | 韦茂亮 | The runway device that slope underriding Xiang row auxiliary ship carrier aircraft is taken off |
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| Publication number | Publication date |
|---|---|
| CN107685844B (en) | 2019-03-19 |
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