CN205525028U - Vertical take -off device of aircraft carrier - Google Patents
Vertical take -off device of aircraft carrier Download PDFInfo
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- CN205525028U CN205525028U CN201620183011.2U CN201620183011U CN205525028U CN 205525028 U CN205525028 U CN 205525028U CN 201620183011 U CN201620183011 U CN 201620183011U CN 205525028 U CN205525028 U CN 205525028U
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Abstract
The utility model discloses a vertical take -off device of aircraft carrier includes at least: the machine of carrying a load on the back, flight -deck and the platform that takes off and land, the machine of carrying a load on the back is flown drive arrangement, fuel cell and automatic control device and is constituteed by all -wing aircraft, year quick -witted plane, cockpit, undercarriage, perpendicular lift arrangement, tie, the platform that takes off and land is that the machine of carrying a load on the back descends and the work platform when taking off, but for lift platform, before the carrier -borne aircraft takes off, at first the adjustment take off and land the quick -witted plane of carrying of platform to the suitable high messenger machine of carrying a load on the back and maintain an equal level with the aircraft carrier deck, then with the carrier -borne aircraft draw to or the carrying on the quick -witted plane and locking the undercarriage with carrier -borne aircraft fixing device to the machine of carrying a load on the back of going by oneself, when the carrier -borne aircraft took off, the perpendicular lift arrangement of the machine of carrying a load on the back at first started, and the machine of carrying a load on the back soars the suspension and leaves the platform that takes off and land, then started the flat drive arrangement that flies and make the machine of carrying a load on the back flat flying with higher speed, and is close or when reaching the take -off speed of carrier -borne aircraft as the level flight speed of the machine of carrying a load on the back, the unblock of carrier -borne aircraft fixing device, and the carrier -borne aircraft goes up to the air smoothly, and the machine of carrying a load on the back returns the aircraft carrier to carry out next time carrying a load on the back of carrier -borne aircraft and takes off.
Description
Technical field
This utility model belongs to aircraft carrier lift-off technology, is specifically related to the device that takes off vertically of a kind of aircraft carrier.
Background technology
Aircraft carrier (Aircraft carrier) is a kind of with large-scale water surface naval vessels that carrier-borne aircraft is main operational weapon.By the configuration of variety classes carrier-borne aircraft, aircraft carrier can complete to include nearly all combat duties such as air-to-ground attack, marine site block, arms deterrence, antisubmarine, anti-ship, and general's strike range expansion is each corner to the world.Carrier-borne aircraft carries fuel, ammunition lift-off is fought supplements fuel with the warship that makes a return voyage, ammunition is most important action during aircraft carrier fleet fights, owing to the deck of aircraft carrier is much smaller relative to airfield, landing airdrome length is the most limited, general at 100-300 rice, carrier-borne aircraft must use some special equipment and means, just can ensure that aircraft normally takes off, lands.Currently, aircraft carrier mode of taking off mainly has two kinds, ski-jump take-off and catapult-assisted take-off, if the carrier-borne aircraft manufactured plus particular design, the most also take off vertically mode.
The sliding formula of jumping is taken off, and to be carrier-borne aircraft take off windward along the cunning of about the 12 ° formula deck that jumps, this mode of taking off be advance speed, the initial velocity provided windward and the deck end obtained to raise up at full speed by aircraft engine extra lift that angle provides completes jointly.Catapult-assisted take-off divides two kinds, and one is steam ejection technology, i.e. promotes the thrust of the additional aircraft engine of huge thrust that piston produces to complete in cylinder by steam on horizontal deck, and another kind is electromagnetic launch, i.e. utilizes electromagnetic energy to launch carrier-borne aircraft.Take off vertically, directly do not go up to the air by aircraft carrier runway, this mode of taking off is confined to custom-designed carrier-borne aircraft, concrete point of three kinds of situations, a kind of be aircraft engine orifice design become can 90 degree turn to such as the Harrier of Britain, Muscovite refined gram of aircraft, the second is that the lift fan that F-35B uses adds nozzle turning function；Three is the V22 osprey aircraft of the U.S., is to install two turbo oar engines at wing tip, makes the aircraft when takeoff and landing have similar gyroplane performance by tilting rotor, and have similar general propeller aircrafts performance when normal flight.
The three of the above mode of taking off is respectively arranged with quality, and the advantage of ski-jump take-off is that technology is relatively easy, and maintaining expense is low, and on warship, staffing is few, fresh-water-saving etc.；Maximum shortcoming is its restriction to carrier-borne aircraft take-off weight, cause carrier-borne aircraft fuel load, bullet-loading capacity on the low side, making the combat radius of carrier-borne aircraft, the to-ground attack capability of carrier-borne aircraft has different weakening, and large-scale operational aircraft such as early warning plane, transporter etc. cannot take off on the sliding deck that jumps；And owing to ski-jump take-off assists without external force, the power of aircraft engine must reach maximum, therefore take-off process not only oil consumption is surprising, also has an impact the life-span of electromotor.Under high sea condition situation, sliding the jolting of formula deck that jump may cause carrier-borne aircraft to be difficult to control to when sliding even go off course, therefore requires higher to the operant skill of pilot.Further, since the landing airdrome length that ski-jump take-off requires is than catapult-assisted take-off bosun, affecting the utilization rate on deck and it is necessary to take off windward, the manipulation to aircraft carrier brings inconvenience, affects fighting efficiency.The advantage of catapult-assisted take-off mode is apparent from, that is, takeoff condition requires low, all can take off against the wind with the wind, will not go off course, and landing airdrome length is short.Maximum advantage is that take-off weight is big, and can take off heavy airplane such as early warning plane, transporter etc., and the fuel load of common opportunity of combat can also be higher with bullet-loading capacity, and fighting efficiency is big.The shortcoming of steam ejection mode is the most prominent: technical sophistication, and maintenance difficulties is big, and maintainer establishment is many, and the especially maintenance of core component open cylinder and the replacing etc. of encapsulant of catapult-launching gear is accomplished by substantial amounts of maintainer.Further, consuming substantial amounts of steam (fresh water is made) when which is taken off, capacity usage ratio is the lowest. it addition, catapult-assisted take-off has had more a huge vapor can (about 200 cubic metres) than ski-jump take-off, take space limited on aircraft carrier.And wartime, once steam ejection device was destroyed, repair difficulty than the sliding deck difficulty that jumps.Although electromagnetic launch capacity usage ratio is high, but equipment is complicated, and parts are various, and reliability needs to be checked under battle conditions.Take off vertically mode, is suitable only for special carrier-borne aircraft, and this aircraft manufacturing is with high costs, technical sophistication, fault rate is high, inconvenient maintenance, and take-off weight is the most little, take oil, to take bullet amount the most limited, and when taking off, oil consumption is surprising, and combat radius is more more than than the routine mode of taking off shortens half.The advantage of the most this mode of taking off is, it is independent of the deck of aircraft carrier, so in the case of in wartime, type aircraft carrier deck is destroyed, carrier-borne aircraft still can take off operation, escort, this to the existence of aircraft carrier fleet sometimes it is critical that, certainly, this kind of carrier-borne aircraft can also use short takeoff mode at ordinary times, thus also can increase voyage, suitably increase and carry bullet.
So far, although the common mode of taking off of carrier-borne aircraft has his own strong points, but all there is its obvious shortcoming.Develop a kind of utilization machine of carrying a load on the back to carry a load on the back the device that carrier-borne aircraft takes off for this, its principle is, first carrier-borne aircraft is carried a load on the back on the machine of carrying a load on the back, then the vertical lift device utilizing machine of carrying a load on the back suspends and leaves deck, carry a load on the back machine flat of recycling flies that driving means is the most flat to fly, when the level speed of the machine of carrying a load on the back reaches the takeoff speed of carrier-borne aircraft, by carrier-borne aircraft release lift-off, machine of carrying a load on the back returns aircraft carrier and carries out the flight of carrying a load on the back of carrier-borne aircraft next time.The machine if an aircraft carrier outfit multi rack is carried a load on the back, is equivalent to add a plurality of fly able aerial runway, can be greatly enhanced fight capability and the survival ability of aircraft carrier undoubtedly.This utility model know-why is simple, and involved device and equipment mostly have the technology of maturation, can put into practice through the test of short-term, form fighting capacity.
Summary of the invention
Technical problem to be solved in the utility model is to provide the device that takes off vertically that a kind of all kinds of carrier-borne aircrafts reliable, efficient, little, applicable to deck dependence take off.
The device that takes off vertically of a kind of aircraft carrier, at least includes: machine of carrying a load on the back, flight-deck and landing platform；Described machine of carrying a load on the back by all-wing aircraft, carrier aircraft plane, driving cabin, undercarriage, vertical lift device, flat fly driving means, fuel tank, carrier-borne aircraft fixing device and self-con-tained unit and form.Described landing platform is carry a load on the back machine landing and work platforms when taking off, for lifting platform；Before carrier-borne aircraft takes off, first adjusting landing platform to proper height makes the carrier aircraft plane of the machine of carrying a load on the back maintain an equal level with flight-deck, and the carrier-borne aircraft being then fully loaded with fuel oil and ammunition travels voluntarily or is towed in the carrier aircraft plane of the machine of carrying a load on the back and locks by fixing device the undercarriage of carrier-borne aircraft；When carrier-borne aircraft takes off, carry a load on the back machine vertical lift device start, machine vertical suspension before this of carrying a load on the back leaves landing platform, the flat driving means that flies of rear startup makes machine of carrying a load on the back accelerate flat flying, when the level speed of the machine of carrying a load on the back is close to or up the takeoff speed of carrier-borne aircraft, carrier-borne aircraft fixing device unlocks, and carrier-borne aircraft goes up to the air smoothly, and machine of carrying a load on the back return aircraft carrier carries out carrying a load on the back of carrier-borne aircraft next time and takes off.
Described machine of carrying a load on the back decision design is without vertical fin, without the aircraft pattern of hydroplane.
The carrier aircraft plane of described machine of carrying a load on the back is provided with carrier-borne aircraft fixing device, fixing device can lock undercarriage before and after carrier-borne aircraft respectively, undercarriage can be prevented in left and right and the movement of fore-and-aft direction, it is possible to moment opens as required, make the undercarriage of carrier-borne aircraft be completely in free state.
The vertical lift device of described machine of carrying a load on the back can be lift engine, it is also possible to be lift fan；Lift engine or lift fan rational deployment are on whole all-wing aircraft and body, even if stopping occur in indivedual lift engine or lift fan does not also interfere with the suspension stability of whole machine of carrying a load on the back.
Further, the lift that the vertical lift device of machine of carrying a load on the back described in produces when the machine of carrying a load on the back takes off is not less than machine and the gross weight of carrier-borne aircraft carried a load on the back thereof of carrying a load on the back.
Further, described in the carry a load on the back all-wing aircraft of machine in flat flying, produce lift, the machine of carrying a load on the back is flat fly during, produced by vertical lift device, lift can gradually reduce.
The flat driving means that flies of described machine of carrying a load on the back can be turbojet, it is also possible to be turbofan；Flat fly driving means and be preferentially installed on the tail of the machine of carrying a load on the back.
Further, the described flat thrust flying driving means generation can ensure that the machine of carrying a load on the back reaches the takeoff speed of carrier-borne aircraft in shorter flying distance；Described takeoff speed is 200-400km/ hour；Described flying distance is 200-2000 rice.
Described landing platform is arranged on the both sides of aircraft carrier flight-deck and the stern of aircraft carrier；Can be fixed pattern lifting platform, it is also possible to be suspension bridge type lifting platform；Suspension bridge type lifting platform is in aircraft carrier training and stretches out from deck and side board wartime, then packs up during daily navigation.
Further, when described landing platform is suspension bridge type lifting platform, it is made up of power source, hydraulic machinery, leading block, pull line, weight cable, hoistable platform and control part etc..Under normal circumstances, machine landing on landing platform of carrying a load on the back, in emergency circumstances can directly land on flight-deck.
The beneficial effects of the utility model are: 1, overcoming ski-jump take-off mode must take off windward, and the shortcoming that can not fully loaded takeoff；2, overcome steam ejection and take off that mode consumes fresh water in a large number, device technique is complicated, keep in repair shortcoming heavy, that staffing is too much；3, eliminate steam storage tank and affiliated facility thereof that steam ejection takes off bulky necessary to mode, significantly expand effective battle space of aircraft carrier；4, to take off mode with the machine of carrying a load on the back carrier-borne aircraft of carrying a load on the back, each model of can taking off calmly is fully loaded with the operational aircraft of fuel oil and ammunition and includes large-scale early warning plane；5, the acceleration that takes off is little, impacts little to the health of pilot, reduces flight error；6, in the case of flight-deck damages, can normally take off various operational aircraft, is greatly enhanced survival ability and the operational efficiency of aircraft carrier；7, the vehicle that machine of carrying a load on the back takes off as carrier-borne aircraft, function singleness, simple in construction, voyage short (the most thousands of rice), speed low (less than 400km/ hour), easily, cost is low in design.In a word, the machine of carrying a load on the back carrier-borne aircraft of carrying a load on the back takes off vertically technology, overcomes carrier-borne aircraft tradition completely and takes off the deficiency of mode, is a kind of subversive Technologies of Shipboard Plane Taking Off, the fight capability of aircraft carrier will be significantly greatly increased.
Accompanying drawing explanation
Fig. 1 is carried a load on the back carrier-borne aircraft flight top view for the machine of carrying a load on the back.
Fig. 2 is machine floor map of carrying a load on the back.
Fig. 3 is the machine of carrying a load on the back on landing platform and carrier-borne aircraft schematic diagram.
Fig. 4 is landing platform distribution schematic diagram on aircraft carrier.
Detailed description of the invention
Below in conjunction with embodiment, the present invention is described in further detail.
As Figure 1-4, the device that takes off vertically of a kind of aircraft carrier described in the utility model, at least include: machine 10 of carrying a load on the back, flight-deck 20 and landing platform 30；Carry a load on the back machine 10 by all-wing aircraft 101, carrier aircraft plane 102, driving cabin 103, undercarriage 104, vertical lift device 105, flat fly driving means 106, fuel tank 107(figure do not show), carrier-borne aircraft fixing device 108(figure does not shows) and self-con-tained unit 109 form.
Landing platform 30 is the machine of carrying a load on the back 10 work platforms when landing and take off, the landing platform 30 used in the present embodiment is lifting platform, and this platform is not shown by power source 301(figure), hydraulic machinery 302(figure does not shows), leading block 303(figure does not shows), pull line 304(figure does not shows), weight cable 305, hoistable platform 306 and controlling organization 307 form.
Before carrier-borne aircraft takes off, first adjusting landing platform 30 to proper height makes the carrier aircraft plane 102 of the machine of carrying a load on the back 10 maintain an equal level with flight-deck 20, is then fully loaded with the carrier-borne aircraft of fuel oil and ammunition and travels voluntarily or be towed in the carrier aircraft plane 102 of the machine of carrying a load on the back 10 and lock undercarriage before and after carrier-borne aircraft by carrier-borne aircraft fixing device 108；When carrier-borne aircraft takes off, the vertical lift device 105 of machine 10 of carrying a load on the back starts, machine 10 vertical suspension before this of carrying a load on the back leaves landing platform 30, the flat driving means 106 that flies of rear startup makes the machine of carrying a load on the back 10 accelerate flat flying, when the level speed of the machine of carrying a load on the back 10 is close to or up the takeoff speed of carrier-borne aircraft, the engine start of carrier-borne aircraft, carrier-borne aircraft fixing device 108 unlocks, carrier-borne aircraft goes up to the air smoothly, and machine 10 of carrying a load on the back returns aircraft carrier to carry out carrying a load on the back of carrier-borne aircraft next time and take off.
Machine of carrying a load on the back 10 described in the present embodiment is designed as without vertical fin, without the generally triangular form aircraft pattern of hydroplane；The vertical lift device 105 of described machine of carrying a load on the back uses lift fan；8 lift fans are symmetrically distributed on the both sides of all-wing aircraft 101 and the body of nearly tail；The total life that when machine 10 of carrying a load on the back takes off, lift fan produces is more than machine 10 and the gross weight of carrier-borne aircraft carried a load on the back thereof of carrying a load on the back；The machine of carrying a load on the back 10 is flat fly during, due to the machine of carrying a load on the back 10 all-wing aircraft 101 and carrier-borne aircraft wing produce lift, the power of lift fan can gradually reduce.
The flat driving means 106 that flies of the machine of carrying a load on the back 10 described in the present embodiment uses turbofan, and 2 fanjets are symmetrically arranged on the tail of the machine of carrying a load on the back 10；The thrust that fanjet produces can ensure that the machine of carrying a load on the back 10 speed in 500-1000 rice flying distance reaches 250-350km/ hour.
Landing platform 30 described in the present embodiment is distributed in the left and right sides of aircraft carrier flight-deck and right stern；Wherein right side sets 3, and left side sets 4, and right stern sets 1；Landing platform 30 all uses suspension bridge pattern and liftable；Suspension bridge type landing platform is in aircraft carrier training and puts down wartime, then packs up during daily navigation.
Under normal circumstances, machine 10 landing on landing platform 30 of carrying a load on the back, in emergency circumstances can directly land on flight-deck 20.
Above example is simply one of the most preferred embodiment; it is to make those skilled in the art be more fully understood that the present invention; it is not to be construed as the restriction to this utility model patent right protection domain; on the contrary; for the common scientific research personnel of this area; the change of all any unsubstantialities utilizing this utility model patent to carry out or adjustment, within all should falling into the protection domain of this patent.
Claims (10)
1. the device that takes off vertically of an aircraft carrier, it is characterised in that: at least include: machine of carrying a load on the back, flight-deck and landing platform；Machine of carrying a load on the back by all-wing aircraft, carrier aircraft plane, driving cabin, undercarriage, vertical lift device, flat fly driving means, fuel tank, carrier-borne aircraft fixing device and self-con-tained unit and form；Landing platform is carry a load on the back machine landing and work platforms when taking off, for lifting platform；Before carrier-borne aircraft takes off, first adjusting landing platform to proper height makes the carrier aircraft plane of the machine of carrying a load on the back maintain an equal level with type aircraft carrier deck, and the carrier-borne aircraft being then fully loaded with fuel oil and ammunition travels voluntarily or is towed in the carrier aircraft plane of the machine of carrying a load on the back and locks by fixing device the undercarriage of carrier-borne aircraft；When carrier-borne aircraft takes off, carry a load on the back machine vertical lift device start, machine vertical suspension before this of carrying a load on the back leaves landing platform, the flat driving means that flies of rear startup makes machine of carrying a load on the back accelerate flat flying, when the level speed of the machine of carrying a load on the back is close to or up the takeoff speed of carrier-borne aircraft, carrier-borne aircraft fixing device unlocks, and carrier-borne aircraft goes up to the air smoothly, and machine of carrying a load on the back return aircraft carrier carries out carrying a load on the back of carrier-borne aircraft next time and takes off.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 1, it is characterised in that: described machine of carrying a load on the back decision design is without vertical fin, without the aircraft pattern of hydroplane.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 1, it is characterized in that: the carrier aircraft plane of described machine of carrying a load on the back is provided with carrier-borne aircraft fixing device, fixing device can lock undercarriage before and after carrier-borne aircraft respectively, undercarriage can be prevented in left and right and the movement of fore-and-aft direction, open also dependent on needs moment, make the undercarriage of carrier-borne aircraft be completely in free state.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 1, it is characterised in that: the vertical lift device of described machine of carrying a load on the back can be lift engine, it is also possible to be lift fan；Lift engine or lift fan rational deployment are on whole all-wing aircraft and body, even if stopping occur in indivedual lift engine or lift fan does not also interfere with the suspension stability of whole machine of carrying a load on the back.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 4, it is characterised in that the lift that the vertical lift device of machine of carrying a load on the back described in: produces when the machine of carrying a load on the back takes off is not less than machine and the gross weight of carrier-borne aircraft carried a load on the back thereof of carrying a load on the back.
The device that takes off vertically of a kind of aircraft carrier the most as claimed in any of claims 1 to 5, it is characterized in that: described in the carry a load on the back all-wing aircraft of machine in flat flying, produce lift, the machine of carrying a load on the back is flat fly during, produced by vertical lift device, lift can gradually reduce.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 1, it is characterised in that: the flat driving means that flies of described machine of carrying a load on the back can be turbojet, it is also possible to be turbofan；Flat fly driving means and be installed on the tail of the machine of carrying a load on the back.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 7, it is characterised in that: the described flat thrust flying driving means generation can ensure that the machine of carrying a load on the back reaches the takeoff speed of carrier-borne aircraft in shorter flying distance；Described takeoff speed is 200-400km/ hour；Described flying distance is 200-2000 rice.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 1, it is characterised in that: described landing platform is arranged on the both sides of aircraft carrier flight-deck and the stern of aircraft carrier；Can be fixed pattern lifting platform, it is also possible to be suspension bridge type lifting platform；Suspension bridge type lifting platform is in aircraft carrier training and stretches out from deck and side board wartime, then packs up during daily navigation.
The device that takes off vertically of a kind of aircraft carrier the most according to claim 9, it is characterized in that: when described landing platform is suspension bridge type lifting platform, be at least made up of power source, hydraulic machinery, leading block, pull line, weight cable, hoistable platform and control part;Under normal circumstances, machine landing on landing platform of carrying a load on the back, in emergency circumstances can directly land on flight-deck.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620183011.2U CN205525028U (en) | 2016-03-10 | 2016-03-10 | Vertical take -off device of aircraft carrier |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620183011.2U CN205525028U (en) | 2016-03-10 | 2016-03-10 | Vertical take -off device of aircraft carrier |
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| CN205525028U true CN205525028U (en) | 2016-08-31 |
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| CN201620183011.2U Active CN205525028U (en) | 2016-03-10 | 2016-03-10 | Vertical take -off device of aircraft carrier |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105584640A (en) * | 2016-03-10 | 2016-05-18 | 上海洲跃生物科技有限公司 | Vertical takeoff device of carrier-based aircraft |
| CN108038258A (en) * | 2017-11-02 | 2018-05-15 | 成都飞机工业（集团）有限责任公司 | A kind of ejection impact dynamic response analysis method based on Coupled Rigid-flexible |
-
2016
- 2016-03-10 CN CN201620183011.2U patent/CN205525028U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105584640A (en) * | 2016-03-10 | 2016-05-18 | 上海洲跃生物科技有限公司 | Vertical takeoff device of carrier-based aircraft |
| CN108038258A (en) * | 2017-11-02 | 2018-05-15 | 成都飞机工业（集团）有限责任公司 | A kind of ejection impact dynamic response analysis method based on Coupled Rigid-flexible |
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