CN207141421U - A kind of aircraft carrier main body provided with auxiliary device - Google Patents
A kind of aircraft carrier main body provided with auxiliary device Download PDFInfo
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- CN207141421U CN207141421U CN201720716219.0U CN201720716219U CN207141421U CN 207141421 U CN207141421 U CN 207141421U CN 201720716219 U CN201720716219 U CN 201720716219U CN 207141421 U CN207141421 U CN 207141421U
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- aircraft carrier
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Abstract
A kind of aircraft carrier main body provided with auxiliary device, including:Upper strata flight-deck (1), lower floor's flight-deck (2), cabin storey of hanging oneself (3), lower gondola layer (4), hangar layer (5), communications tower (6), block machine platform (7), it is characterised in that:Lower floor's flight-deck (2) is integrally used as flying-off deck, since stern, is made up of launching platform a, lower slippery runway deck b, horizontal acceleration runway deck c, several sections of the runway deck d that jumps up;Overhead building is provided with lower floor's flight-deck (2), overhead building is topmost upper strata flight-deck (1), and its left front end is provided with and blocks machine platform (7) and its guide rail.The beneficial effects of the utility model are:Substantially improve the landing environment of aircraft carrier, it is possible to achieve the non-ejection of several frame carrier-borne aircrafts is fullyed loaded takeoff simultaneously, greatly improves aircraft carrier fighting capacity;Meanwhile advantage is created with management and control carrier landing risk effectively to reduce, it can double to improve recovery speed of carrier-borne aircraft etc..
Description
Technical field
Aircraft carrier technical field is the utility model is related to, is exactly a kind of aircraft carrier main body provided with auxiliary device.
Background technology
Now, aircraft carrier, which takes off mainly, sliding jump and ejection two ways, before corresponding aircraft carrier flight-deck also has
Kick up and two kinds of design forms of level at end.For the cunning jump formula deck that front end is kicked up, its shortcoming is:In Take-Off Field Length one
Under conditions of fixed, the take-off weight of carrier-borne aircraft is restricted, and can not meet that low thrust-weight ratio carrier-borne aircraft takes off.Though steam ejection takes off
It is so to meet the preferable means that modern carrier-borne aircraft takes off, but its systematic comparison is complicated, technology application requirement is harsher, steam
Amount consumption is larger, and the fltting speed of aircraft carrier can be affected during continuous ejection, and produce steam need the fresh water amount that consumes also compared with
Greatly, this is also undoubtedly a larger burden for sea going aircraft carrier;For electromagnetic launch, the application of technology and grind
Study carefully and be still in the secrecy stage, it is stated that its power consumption is also quite surprising;Either steam ejection or electromagnetic launch, ejection dress
Put in harsh war necessarily one of primary destruction target of enemy, if any one link failure of catapult-launching gear or
It can not just be gone up to the air by carrier-borne aircraft is destroyed, aircraft carrier will be out of action, and be also just far from being denial of the air and control of the sea, aircraft carrier
On will face the danger finished off with one blow except helicopter, other all carrier-borne aircrafts.Equally, if sliding jump formula deck is broken first
Ruin, its carrier-borne aircraft can not go up to the air operation.Either sliding jump or catapult-assisted take-off, it is but only logical for the landing of carrier-borne aircraft
The obstruction system crossed on unique landing runway could realize that the organic efficiency of carrier-borne aircraft, which is far below, lets efficiency fly away.Because landing is run
Road anxiety is busy, and the carrier-borne aircraft to make a return voyage, which often will be lined up to spiral in the air, waits warship, it is therefore desirable to consumes great amount of fuel oil, also aggravates
The fatigue of carrier-borne aircraft pilot.Thus also it is not difficult to find out, of such a size aircraft carrier platform, the Function to supporting carrier-borne aircraft landing
It is extremely limited, cause the waste and devaluation of aircraft carrier precious resources.In a word, prior art aircraft carrier takes off, landed
Auxiliary equipment is relatively simple and fragile, for security and economy, can neither meet high efficiency training and military exercises
Needs, the needs of future war can not be met.From the point of view of real aircraft carrier enters a war history, the person of being bombarded and sink can be found everywhere, and survive
Person is very few.Therefore, future aircraft carrier be except that will possess excellent protective capacities, with greater need for there is seeking survival after being inflicted heavy losses on and again
Secondary counterforce capability, be also required to certainly for carrier-borne aircraft create transmitting-receiving freely, safe and efficient guarantee condition.
The content of the invention
In order to improve the lift-off supportability of aircraft carrier, while improve the recovery ability of carrier-borne aircraft, the utility model
Provide a kind of aircraft carrier main body provided with auxiliary device.
Technical scheme is used by the utility model solves its technical problem:A kind of aircraft carrier provided with auxiliary device
Main body, including:Upper strata flight-deck (1), lower floor's flight-deck (2), cabin storey of hanging oneself (3), lower gondola layer (4), hangar layer (5),
Communications tower (6), block machine platform (7), it is characterised in that:Lower floor's flight-deck (2) is integrally used as flying-off deck, since stern,
It is made up of launching platform a, lower slippery runway deck b, horizontal acceleration runway deck c, several sections of the runway deck d that jumps up, launching platform a
Carrier-borne aircraft takeoff point at and the overhead port of export be additionally provided with water spraying atomization device;Under lower floor's flight-deck (2) is in turn below
Gondola layer (3) and hangar layer (5), overhead building is provided with lower floor's flight-deck (2), and overhead building is topmost upper strata flight
Deck (1), is hang oneself cabin storey (3) and other functional cabins below, overhead each layer rear end open of building, each layer in front end from lower and
Upper successive is forward extended out, and is provided with open type grandstand, and communications tower (6), front end are provided with upper strata flight-deck (1) right side edge
Slightly raise up;Takeoff runway is planned on lower floor's flight-deck (2), upper strata flight-deck (1) is integrally used as alighting deck, plans
Landing runway and arrester wires device;The left and right topside of warship is provided with lift.
Flight-deck (1) left front end in upper strata is prescinded one piece, is provided with blocks machine platform (7) and its guide rail here, block
Machine platform (7) front end and left side, which are respectively equipped with, stops component and machine block network, blocks machine platform (7) and is provided with dead-man's device, is oriented to
The end of track is provided with buffer stop component, and the afterbody for blocking machine platform (7) is additionally provided with pull-type delay loading device.
The region that upper strata flight-deck (1) and lower floor's flight-deck (2) periphery are not subject to heavy duty is equipped with solar-electricity
Pond plate.
Warship bow is provided with bellows t, and bellows t is provided with heater and the ventilation shaft and controlling baffle plate to each layer deck.
Warship bower anchor chain is connected with hydraulic jet propulsion system.
Its advantage is the utility model compared with the prior art:1) carrier-borne aircraft take off, alighting deck layered arrangement, mutually
Do not influence, substantially improve aircraft carrier flight operating environment, reduce aircraft carrier flight operation danger;Meanwhile can exponentially it increase
Add, dropped runway, improved carrier-borne aircraft comprehensively and rise, drop efficiency.2) carrier-borne aircraft rises, drop using straight-through complete deck, adds flight
In the reaction time of member, be advantageous to preferably control the landing of carrier-borne aircraft;Compared with oblique angle alighting deck, due to its runway center line marking with
Aircraft carrier direction of advance is consistent so that carrier-borne aircraft landing difficulty is greatly lowered, and line up becomes to compare when carrier-borne aircraft lands
Easily, course adjustment workload be also greatly reduced, pilot can concentrate one's energy to strive for once warship success;Carrier-borne aircraft is oblique simultaneously
The component velocity also vanishing vertical with aircraft carrier direction of advance existing for the deck-landing of angle, sideslip during carrier landing, turn on one's side because
Element is greatly reduced, thus the precision of carrier landing and security are improved.The little Yang angles of upper strata flight-deck front end
Design so that the success rate that carrier-borne aircraft goes around also is further ensured that, in consideration of it, engine during carrier landing accelerates
Operation just It is not necessary to, due to now carrier-borne aircraft underloading, using its sinking speed raising up plus front end deck, go around into
For power without doubting, the largest benefit so done is can to reduce the overload quantity of carrier landing moment, prevents carrier-borne aircraft
The serious accident such as pintle or arrester wires overload breakage.3) this complete deck, accelerated using Gravitational sliding, the sliding mould that takes off for rising to sky
Formula takes full advantage of the length and height of flying-off deck, maximizes the efficiency of flying-off deck, avoids steam ejection or electromagnetism
The high-grade energy consumption of ejection;Both advantage was created for fullying loaded takeoff for large-scale carrier-borne aircraft, while also reduces aircraft carrier
The technical threshold of carrier-borne aircraft, being advantageous to the more excellent operational aircraft of performance turns into carrier-borne aircraft.4) takeoff point moves to warship stern, is advantageous to
The concentration discharge of hot flame gas and heat energy recycle when carrier-borne aircraft takes off;Blast screen such operation is risen when carrier-borne aircraft takes off
Also without, or even rise braking catch, first allow aircraft engine rated power operate a period of time, be further enlarged to
Peak power, the off program of take-off the brake device is also not necessarily to again after engine working stability, but allows carrier-borne aircraft
It is directly off from small-power, due to there is the boosting of lower slippery runway, it is sufficient that with usual thrust, therefore save raising engine
Time required for power, the high-power run time of aircraft is decreased, so not only enormously simplify operation, and save
Fuel oil, protect carrier-borne aircraft engine (Soviet Union -33 needs the time of nearly 5 seconds from short field take-off from small-power to peak power,
For the full runway of this technology takes off, completely carrier-borne aircraft can be allowed to carry out acceleration of taking off in longer distance, i.e.,
Acceleration time of the carrier-borne aircraft from small-power to peak power is extended, can both protect carrier-borne aircraft engine, warship can also be improved
The effective utilization ratio of carrier aircraft fuel oil);The input of the water spraying atomization device of carrier-borne aircraft takeoff point and the overhead port of export is advantageous to increase
The thrust of carrier-borne aircraft.5) overhead building can increase substantial amounts of cabin, so as to substantially improve aircraft carrier work, living condition;Upper strata
Communication tower height degree on flight-deck, base area greatly reduce, and the influence to carrier landing also minimizes.6) machine is blocked
Platform is the last reliable defence line together of carrier landing, when carrier-borne aircraft needs emergency landing, oblique angle runway can be selected
Slip into and blocked in the machine block network that machine platform has been opened after warship, and promote block machine platform together orbital motion slow down be finally stopped, therefore
Aircraft carrier can effectively be reduced warship and fall into the sea the generation of accident, reduce warship overload to greatest extent, ensure carrier-borne aircraft and
(this blocks machine platform compared with prior art to the safety of aircrew, and the machine block network of prior art is in case of emergency to take resistance
Block what rope position was laid, normal the warship of other carrier-borne aircrafts cannot be carried out by laying machine block network, and it, which is laid and removed, compares
Relatively hastily, secondly, block and overload during machine very big, there is certain damage to carrier-borne aircraft;It is described in the utility model to block machine platform
Be it is standby at any time, on other carrier-borne aircrafts warship influence it is smaller, because its obstruction distance is longer, and by repeatedly increasing resistance
Power and reduce carrier landing overload to greatest extent, the damage to carrier-borne aircraft is smaller).7) week of upper and lower layer flight-deck
Side is equipped with solar panel, and considerable electric power can be provided for aircraft carrier, is created favorable conditions for the electrification of aircraft carrier.8)
The setting of warship bow bellows, the ventilation condition of aircraft carrier can be improved under certain condition, it is energy-saving to be advantageous to aircraft carrier.9) warship bower anchor chain
It is connected with hydraulic jet propulsion system, can have both met the needs that aircraft carrier casts anchor, aircraft carrier motive force can also be increased, improves aircraft carrier navigation
Speed, also significantly reduce the deadweight amount of aircraft carrier.
Brief description of the drawings
Fig. 1 is the utility model schematic front view, and Fig. 2 is the utility model schematic top plan view.
In figure:1- upper stratas flight-deck, 2- lower floors flight-deck, 3- hang oneself cabin storey, gondola layer under 4-, 5- hangar layers, 6-
Communications tower, 7- block machine platform.
Embodiment:
Principle of the present utility model and feature are described below in conjunction with accompanying drawing, illustrated embodiment is served only for explaining
It is bright, be not intended to limit the scope of the utility model.All any modifications made within thought of the present utility model and principle,
Improvement, equivalent substitution etc., should be included within the scope of protection of the utility model.
Referring to Fig. 1, Fig. 2, a kind of aircraft carrier main body provided with auxiliary device, including:Upper strata flight-deck (1), lower floor
Flight-deck (2), cabin storey of hanging oneself (3), lower gondola layer (4), hangar layer (5), communications tower (6), machine platform (7) is blocked, its feature exists
In:Lower floor's flight-deck (2) is integrally used as flying-off deck, since stern, by launching platform a, lower slippery runway deck b, level
Accelerate runway deck c, several sections of compositions of runway deck d of jumping up;Lower floor's flight-deck (2) is lower gondola layer (3) and machine in turn below
Storehouse layer (5), overhead building is provided with lower floor's flight-deck (2), and overhead building is topmost upper strata flight-deck (1) as drop
Fall deck, be hang oneself cabin storey (3) and other functional cabins below, overhead each layer rear end open of building, each layer in front end from lower and
Upper successive forward extends out, and is provided with open type grandstand, and the front end of upper strata flight-deck (1) slightly raises up.
Referring to Fig. 2, takeoff runway p1~p6 is planned on lower floor's flight-deck (2), upper strata flight-deck is advised on (1)
Three regular descent runway p7, p8, p9 and an oblique angle landing runway p10 are drawn, regular descent runway fills provided with arrester wires
Put.
Referring to Fig. 1, at the takeoff point of the carrier-borne aircraft of the launching platform a and the overhead port of export is additionally provided with water spraying atomization device
(not shown).
Referring to Fig. 1, Fig. 2, communications tower (6), communications tower (6) front are provided with upper strata flight-deck (1) right side edge
It is planned to helicopter diamond.
Referring to Fig. 2, upper strata flight-deck (1) left front end is prescinded one piece, here be provided with block machine platform (7) and
Its guide rail (not shown), block machine platform (7) front end and left side is respectively equipped with obstruction component and machine block network (does not show in figure
Go out), block machine platform (7) and be provided with dead-man's device, on oblique angle runway p10 center line, the end of guide rail is set its starting point
Have buffer stop component, block machine platform (7) afterbody be additionally provided with pull-type delay loading device (not shown in figure, towed body can
To be standby redundancy casing on aircraft carrier etc.).
Referring to Fig. 2, warship port side is provided with lift M1, M3, M5, and warship starboard side is provided with lift M2, M4, M6.
Referring to Fig. 2, the upper strata flight-deck (1) and lower floor's flight-deck (2) periphery are not subject to heavily loaded region Jun Pu
Provided with solar panel.
Referring to Fig. 1, warship bow is provided with bellows t, and heater and the ventilation shaft to each layer deck and control are provided with bellows t
Baffle plate (not shown).
Referring to Fig. 1, warship bower anchor chain is connected with hydraulic jet propulsion system (to be not shown, hydraulic jet propulsion system is existing skill in figure
Art).
Claims (7)
1. a kind of aircraft carrier main body provided with auxiliary device, including:Upper strata flight-deck (1), lower floor's flight-deck (2), on
Gondola layer (3), lower gondola layer (4), hangar layer (5), communications tower (6), block machine platform (7), it is characterised in that:Lower floor's flight-deck
(2) it is overall to be used as flying-off deck, since stern, by launching platform a, lower slippery runway deck b, horizontal acceleration runway deck c, jump
Play several sections of compositions of runway deck d;Lower floor's flight-deck (2) is lower gondola layer (4) and hangar layer (5) in turn below, and lower floor flies
Overhead building is provided with deck (2), overhead building is topmost the overall upper strata flight-deck (1) as alighting deck.
A kind of 2. aircraft carrier main body provided with auxiliary device as claimed in claim 1, it is characterised in that:The upper strata flight
Deck (1) edge is provided with communications tower (6), is cabin storey (3) of hanging oneself below, overhead each layer rear end open of building, each layer in front end
Successive forward extends out from bottom to top, and is provided with open type grandstand, and the front end of upper strata flight-deck (1) slightly raises up.
A kind of 3. aircraft carrier main body provided with auxiliary device as claimed in claim 1, it is characterised in that:The launching platform
At the takeoff point of a carrier-borne aircraft and the overhead port of export is additionally provided with water spraying atomization device.
A kind of 4. aircraft carrier main body provided with auxiliary device as claimed in claim 1, it is characterised in that:The upper strata flight
Deck (1) left front end is prescinded one piece, is provided with blocks machine platform (7) and its guide rail here, block machine platform (7) front end and a left side
Side, which is respectively equipped with, stops component and machine block network, blocks machine platform (7) and is provided with dead-man's device, the end of guide rail is provided with buffering
Barrier structure, the afterbody for blocking machine platform (7) are additionally provided with pull-type delay loading device.
A kind of 5. aircraft carrier main body provided with auxiliary device as claimed in claim 1, it is characterised in that:The upper strata flight
The region that deck (1) and lower floor's flight-deck (2) periphery are not subject to heavy duty is equipped with solar panel.
A kind of 6. aircraft carrier main body provided with auxiliary device as claimed in claim 1, it is characterised in that:Aircraft carrier warship bow is provided with
Bellows t, bellows t are provided with heater and the ventilation shaft and controlling baffle plate to each layer deck.
A kind of 7. aircraft carrier main body provided with auxiliary device as claimed in claim 1, it is characterised in that:Aircraft carrier warship bower anchor chain
It is connected with hydraulic jet propulsion system.
Priority Applications (1)
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CN201720716219.0U CN207141421U (en) | 2017-06-09 | 2017-06-09 | A kind of aircraft carrier main body provided with auxiliary device |
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CN201720716219.0U CN207141421U (en) | 2017-06-09 | 2017-06-09 | A kind of aircraft carrier main body provided with auxiliary device |
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CN207141421U true CN207141421U (en) | 2018-03-27 |
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CN201720716219.0U Expired - Fee Related CN207141421U (en) | 2017-06-09 | 2017-06-09 | A kind of aircraft carrier main body provided with auxiliary device |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN107539491A (en) * | 2017-06-09 | 2018-01-05 | 石福军 | A kind of aircraft carrier main body and its auxiliary device |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN107539491A (en) * | 2017-06-09 | 2018-01-05 | 石福军 | A kind of aircraft carrier main body and its auxiliary device |
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Legal Events
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180327 Termination date: 20190609 |
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CF01 | Termination of patent right due to non-payment of annual fee |