CN102862684A - Novel aircraft carrier flying-off deck - Google Patents
Novel aircraft carrier flying-off deck Download PDFInfo
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- CN102862684A CN102862684A CN2011101925881A CN201110192588A CN102862684A CN 102862684 A CN102862684 A CN 102862684A CN 2011101925881 A CN2011101925881 A CN 2011101925881A CN 201110192588 A CN201110192588 A CN 201110192588A CN 102862684 A CN102862684 A CN 102862684A
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Abstract
The invention discloses a novel aircraft carrier flying-off deck, which comprises an ascending flying-off desk section, wherein a carrier plane flying-off acceleration equipment cabin is arranged below a starting section, a brake is arranged outside two tank wheels which are installed on a support through a wheel shaft inside the cabin, the two tank wheels are connected, a rubber plate is hung on the inner surface of a reinforced crawler belt, and the crawler belt is provided with a special crawler belt plate with a towing hook. Two tank engines with an independent oil box and an independent water box respectively are arranged on an engine support at the side of each tank wheel, the tank engines are connected with the tank wheels through a clutch and a transmission case, and a crawler belt tension wheel installation support is provided with a crawler belt tension wheel with a crawler belt traction motor. The starting section of the ascending flying-off deck is provided with a deck narrow seam, and a telescopic automatic switch, a brake releasing switch and a brake anchoring rod are respectively arranged on the middle-rear section and nearby the end of the deck narrow seam and on flying-off station deck on the rear part. The novel aircraft carrier flying-off deck integrates the advantages of a flat ejection flying-off deck and an ascending flying-off deck, and is also free from the defects of the two flying-off decks.
Description
Technical field:
The present invention relates to aircraft carrier, particularly a kind of have straight catapult-assisted take-off deck and on lift up the advantage of flying-off deck, and do not have the novel aircraft carrier flying-off deck of above-mentioned two kinds of flying-off deck shortcomings simultaneously.
Background technology:
Now the flying-off deck of aircraft carrier mainly contains two kinds, and a kind of is the straight catapult-assisted take-off deck of adopting the catapult-assisted take-off mode, another kind be adopt the sliding mode of flying of jumping up on lift up flying-off deck.Straight catapult-assisted take-off deck can allow carrier-borne aircraft take off with larger take-off weight, can also takeoff data not good second-mission aircraft, because the draw of launching slide rail, can make carrier-borne aircraft automatically enter the correct line that slides, the safety of taking off is larger, do not worry aircraft carrier rolling under bad sea situation, the impact that carrier-borne aircraft is taken off and causes, but the ejector weight and volume that it adopts is all larger, taken the inner space of a large amount of preciousness of aircraft carrier, complex structure is safeguarded comparatively inconvenience, generally is not suitable for the baby carrier below 30,000 tons, empties the difficulty and the cost that have increased aircraft carrier.The ejector of most of kinds all is that active force with aircraft carrier is as dynamic foundation in addition, after many carrier-borne aircrafts that scramble, can make aircraft carrier and reduce the speed of a ship or plane because of the minimizing of active force, thereby affected the maneuverability of aircraft carrier, especially the steam ejector is when taking off carrier-borne aircraft, also can consume a large amount of fresh water and steam, increase the work capacity of fresh water rear supply.Ejector has turn(a)round and overhaul phase, once break down or suffer to hit and just can't use, make the carrier-borne aircraft operation of can't going up to the air, affected the fighting capacity of aircraft carrier, and on lift up flying-off deck because ejector is not installed, just utilize the front portion, deck on the section of lifting up make carrier-borne aircraft lift-off, structure is comparatively simple and weight is also light, do not need to safeguard that tool does not take the inner space of aircraft carrier preciousness, reduce construction difficulty and the cost of aircraft carrier, not only be fit to also suitable baby carrier below 30,000 tons of big-and-middle-sized aircraft carrier.It does not exist turn(a)round and overhaul phase, also can make the carrier-borne aircraft lift-off after just being attacked, can not affect the fighting capacity of aircraft carrier, because it is without any need for power, even if take off again many carrier-borne aircrafts, also can not affect the speed of a ship or plane of aircraft carrier, the maneuverability of aircraft carrier is reduced, more can not increase the logistic work amount of water supply, but because it helps carrier-borne aircraft to take off without any power, just the power with carrier-borne aircraft self accelerates rolling start, the floor space that is limited to aircraft carrier is limited, flying-off deck length generally can be very not long, and this just can not take off with larger take-off weight carrier-borne aircraft, or be to add oil and hang less ammunition, to hang ammunitions and few oiling more, be not combat radius too little be exactly that the attack power is inadequate, also might be that airborne period is too short, carrier-borne aircraft can fight capability be reduced.In addition can only takeoff data airplane carrier fighter preferably, can takeoff and landing performance not good second-mission aircraft, and owing to will make the track line alignment of longitudinal axis and the flying-off deck of carrier-borne aircraft, make carrier-borne aircraft in that to enter the time that when position battle array of taking off need longer, reduced the dynamic frequency that of carrier-borne aircraft, and carrier-borne aircraft is in that to enter the floor space that when position battle array of taking off need larger, limited and waited for the carrier-borne aircraft quantity of taking off behind the blast screen, and then affected the fighting capacity of whole aircraft carrier, since carrier-borne aircraft when taking off without any traction, when aircraft carrier in the situation that produces rolling under the bad sea situation, be not easy when taking off, carrier-borne aircraft to be controlled.More than two kinds of flying-off decks all have such or such deficiency.
Summary of the invention:
The purpose of this invention is to provide a kind of have straight catapult-assisted take-off deck and on lift up the advantage of flying-off deck, and do not have the novel aircraft carrier flying-off deck of above-mentioned two kinds of flying-off deck shortcomings simultaneously.
Technical solution of the present invention is finished as follows.It include lift up flying-off deck on the section of lifting up, flat segments and off section, it is characterized in that: have the off acceleration equipment of carrier-borne aircraft cabin lifting up the off section in deck, one in front and one in back two pairs of tank wheel supports are arranged in the cabin, have above tank wheel is positioned on by the wheel shaft that lengthens at every pair of tank wheel support, reinforced tank track with special manufacturing links up two tank wheel rims, on the special reinforced tank track of making, a special special tank crawler plates of making is arranged, the traction hook that has a traction carrier-borne aircraft to use on it, at the other driving engine mount pad of tank wheel driving engine is installed, couple together by change speed gear box and tank wheel, on the deck of lifting up the off section of flying-off deck in the middle of the special reinforced tank track top of making, have the narrow slit that can allow together the traction hook expose flying-off deck.Carrier-borne aircraft works the sliding running velocity degree when flying away from warship, along with the increase of ground run distance increases, and is low-down in the off stage speed that begins most.This novel aircraft carrier flying-off deck mainly is at the carrier-borne aircraft block clearance time, utilize driving engine and change speed gear box to drive together tank wheel High Rotation Speed, the reinforced tank track that makes simultaneously special manufacturing is high-speed operation forward, and the special caterpillar block of the special manufacturing on it is just linked up with together with traction, drawing the at a high speed forward sliding race of starting of carrier-borne aircraft, and this moment carrier-borne aircraft owing to be subject to self engine thrust and the combined action of traction dbp, just can be fireballing more than simple use self driving engine block clearance time, when increasing it and take off by the runaway speed that increases carrier-borne aircraft from warship speed, and rely on to increase carrier-borne aircraft increase its take-off weight from warship speed, can increase to a certain extent its fighting efficiency.In order further to increase the runaway speed of carrier-borne aircraft, this novel aircraft carrier flying-off deck has adopted main battle tank water-cooled diesel motor, and adopt one in front and one in back two water cooled main battle tank diesel motors and change speed gear box, on the other driving engine mount pad of each tank wheel, a main battle tank water-cooled diesel motor and change speed gear box are arranged, they have separately fuel tank and water tank in order to be independent of each other, fuel tank and water tank are installed in the back side that two main battle tanks are used the water-cooled diesel motor, although this novel aircraft carrier flying-off deck just draws carrier-borne aircraft in the carrier-borne aircraft sliding race starting stage, rather than the such whole process traction in straight catapult-assisted take-off deck, but because it is in the sliding starting stage of running of carrier-borne aircraft, just having given comparatively correct sliding race of carrier-borne aircraft points to and the sliding inertia that runs, when aircraft carrier during rolling, still can have higher steerability and safety when carrier-borne aircraft takes off in bad sea situation.Because this novel aircraft carrier flying-off deck can run the starting stage in that carrier-borne aircraft is sliding, certainly be about to carrier-borne aircraft be drawn to correct cunning and run away on the line, so need not with the carrier-borne aircraft longitudinal axis fully and the sliding line that runs of flying-off deck align, the creep angle of certain angle can be arranged.Although the angle of this creep angle is little, but can obviously strengthen the entrance angle that carrier-borne aircraft enters the battle array position of taking off, can dwindle carrier-borne aircraft and enter the floor space that the battle array position of taking off needs, wait for the carrier-borne aircraft quantity of taking off after increasing blast screen, the departure time of carrier-borne aircraft is shortened, and can improve the dynamic frequency that of carrier-borne aircraft, can increase to a certain extent the fighting capacity of aircraft carrier, or the range of control of increase aircraft carrier, or the attack dynamics of increase carrier-borne aircraft, it also might be the airborne period that increases carrier-borne aircraft, in order to make carrier-borne aircraft can before the sliding race start of a race, reach the maximum thrust of driving engine, and unlike land airplane, in sliding the race, reach the maximum thrust of driving engine, at the place, battle array position of taking off of lifting up the off break deck narrow slit of flying-off deck rear portion, a telescopic braking anchor pole is installed, utilize this telescopic braking anchor pole before the sliding race of carrier-borne aircraft is off, it to be braked, make carrier-borne aircraft after its driving engine reaches maximum thrust, just begin to start to walk to slide and run, can shorten to a certain extent the ground run distance of carrier-borne aircraft.For the traction hook is broken away from and carrier-borne aircraft rear to the carrier-borne aircraft traction, in the posterior segment of lifting up the off break deck narrow slit of flying-off deck, telescopic brake switch is installed, a brake is arranged on every pair of tank wheel support, and a power-transfer clutch is arranged between every main battle tank is with water-cooled diesel motor and its change speed gear box, behind the telescopic brake switch of carrier-borne aircraft nose-gear wheel positive motion, can brake the tank wheel at one time, disconnect main battle tank water-cooled diesel motor and change speed gear box, tank wheel and the special reinforced tank track of making are slowed down, and the special caterpillar block of special manufacturing thereon and traction hook also slow down together, and carrier-borne aircraft does not slow down at this moment, but under the thrust of himself driving engine, accelerate to advancing slip race, can utilize the velocity contrast of carrier-borne aircraft and traction hook, carrier-borne aircraft is separated with the traction hook.Telescopic brake switch can not be located at the end of lifting up the off break deck narrow slit of flying-off deck or near end place, because the traction hook rotates when arriving end place, can not guarantee carrier-borne this moment and traction is linked up with and to be separated fully, if carrier-borne aircraft with the traction hook is rotated, not only can cause carrier-borne aircraft to go up to the air, also might damage carrier-borne aircraft and traction hook, even the reinforced tank track of whole special manufacturing.In order to save diesel oil and protection main battle tank water-cooled diesel motor, telescopic brake switch also reduces main battle tank at one time with the delivery quality of water-cooled diesel motor when the tank wheel is braked, and it is only remained on make a gift of fast operative condition.And in order to protect main battle tank water-cooled diesel motor, begin to enter when taking off battle array position standby for takeoff at carrier-borne aircraft, just must allow first it turn round making a gift of under the fast operative condition.Because the traction hook also will be got back to the place, battle array position of taking off of carrier-borne aircraft, will unclamp immediately the tank wheel after guaranteeing carrier-borne aircraft and the traction hook separates, so near end place the telescopic switch that declutches is installed at the off section of flying-off deck narrow slit.The telescopic switch that declutches is installed in sliding race of flying-off deck to be estimated the nearly head of deck narrow slit and approaches the place two benefits are arranged: the one, and carrier-borne aircraft nose-gear wheel is when positive motion declutches switch, and can guarantee that carrier-borne aircraft and traction are linked up with separates; The 2nd, can be as far as possible early unclamp the tank wheel, make the traction hook rely on inertia to get back to the carrier-borne aircraft place, battle array position of taking off as far as possible.For the reinforced tank track elasticity to special manufacturing is adjusted, can adapt to different sea areas and weather, it is special on carrier-borne aircraft takes off the deck of bottom, acceleration equipment cabin, a track adjusting wheel mounting bracket is installed, a track adjusting wheel is installed on it, by this track adjusting wheel the reinforced tank track of special manufacturing is carried out degree of tightness and regulate.At track adjusting wheel a cranking traction electrical motor is arranged, to guarantee that the traction hook is after effect of inertia stops, also can get back to take off battle array position place of carrier-borne aircraft, can also make simultaneously the traction hook after all carrier-borne aircrafts that need to go up to the air all go up to the air, from carrier-borne aircraft the walk bottom of flying-off deck of battle array position of taking off, guaranteed the smooth of ship aircraft carrier flying-off deck.Take off acceleration equipment at the traction carrier-borne aircraft is sliding when running dry sound for reducing carrier-borne aircraft, mount the rubber plate that the dry sound of reduction is used at the special reinforced tank track inner face of making, but do not mount outside identical rubber plate in order to reduce weight of equipment with manufacturing cost.Acceleration equipment is simple in structure, lightweight, volume is little because the carrier-borne aircraft that this novel aircraft carrier flying-off deck uses takes off, and account for have more than is needed too many aircraft carrier inner space, in addition since its usefulness mainly all be existing equipment, can not give too large difficulty and the cost of manufacturing increase of whole aircraft carrier, make it not only be adapted at using on the big-and-middle-sized aircraft carrier, also be adapted at using on the baby carrier below 30,000 tons.Because it has oneself independently power system, the carrier-borne aircraft of how many sorties that no matter take off can not impact the active force of aircraft carrier, and the speed of a ship or plane of aircraft carrier is descended.Because the main battle tank that it uses not is a lot of with the cold water of employing that the water-cooled diesel motor needs, and therefore can not cause obvious impact to the fresh water rear supply of aircraft carrier.The main battle tank that uses owing to its just draws stage ability full-load operation to carrier-borne aircraft with the water-cooled diesel motor, and turn round under the fast operative condition just making a gift of At All Other Times, so whole system is not very large to the demand of diesel oil, specific efficiency is higher mutually with straight catapult-assisted take-off deck, neither be very outstanding to the rear supply requirement of diesel oil.Because this novel aircraft carrier flying-off deck structure is comparatively simple, safeguards more convenient and the replacing parts also comparatively rapid, generally do not have special turn(a)round and overhaul phase, can not impact taking off of carrier-borne aircraft.Even if genuine in more special situation even so, and fault and the damage situation that can't repair appearred, carrier-borne aircraft also can be as directly the flying-off deck going up to the air with the sliding mode that jumps lifting up, and the situation that can't go up to the air as carrier-borne aircraft straight catapult-assisted take-off deck can not appear, only the take-off weight of carrier-borne aircraft is less.Since this novel aircraft carrier flying-off deck can improve carrier-borne aircraft from warship speed, the second-mission aircraft of below average performance that therefore can take off, but the second-mission aircraft of the performance such as low of taking off surely that differs.This novel aircraft carrier flying-off deck not only can directly be used in the enterprising enforcement of newly-built aircraft carrier, but also can transform lifting up the flying-off deck aircraft carrier on existing, as long as transform accordingly at the off break deck place of lifting up flying-off deck, and under this deck, place, leave the same carrier-borne aircraft acceleration equipment cabin of taking off, in the cabin, install identical parts and get final product.This novel aircraft carrier flying-off deck have have straight catapult-assisted take-off deck and on lift up the advantage of flying-off deck, and do not have the preceence of above-mentioned two kinds of flying-off deck shortcomings simultaneously.Need in addition to illustrate specially 3 points: this novel aircraft carrier flying-off deck can not have fully straight catapult-assisted take-off deck and on lift up the advantage of flying-off deck, some shortcomings that also can have above-mentioned two kinds of first of taking off simultaneously fully, just these two kinds of flying-off deck merits and faultss is a kind of compromise.Two in order to use this novel aircraft carrier flying-off deck, and carrier-borne aircraft must be similar to front-wheel and pull that to launch connection mode such, and sample and its corresponding site are reequiped to front rising and falling.Three traction hooks also should science calculate the hauling distance of carrier-borne aircraft, too short then excessive to the housing construction intensity effect of carrier-borne aircraft, and also possibly can't reach the haulage speed of optimum efficiency, the long DeGrain that then can cause traction, even hook and the synchronous situation of nose-gear also can appear drawing at the traction latter end, should avoid occurring any in top two kinds of situations as far as possible.
Description of drawings:
This accompanying drawing is side direction structural representation of the present invention, and wherein 1 is the aircraft carrier ship side, 2 on lift up the section of lifting up on the flying-off deck, 3 on lift up the flying-off deck flat segments.Telescopic brake switch 5 shown in the accompanying drawing and the telescopic switch 6 that declutches do not need to make so large, and can the carrier-borne aircraft acceleration equipment that takes off being controlled, and don't the ski-running that adds that affects carrier-borne aircraft is run and is advisable.The deck narrow slit of lifting up the off section of flying-off deck place in addition can't show in this accompanying drawing, and the rubber plate that mounts in the tank track and wheel shaft also can't show.
The specific embodiment:
Though this novel novel aircraft carrier flying-off deck is novel, neither innovate fully, but to lifting up a kind of improvement of flying-off deck on existing.Mainly be in the bottom of lifting up the off section 4 of flying-off deck, have the carrier-borne aircraft acceleration equipment cabin 8 of taking off, tank wheel mount pad 15 and 16 two pairs of tank wheels of rear tank wheel mount pad mount pad before under flying-off deck, being equipped with, the wheel shaft that a lengthening is arranged on every pair of tank wheel mount pad, front tank wheel mount pad 15 is equipped with front tank wheel 17 by wheel shaft, rear tank wheel mount pad 16 is equipped with rear tank wheel 18 by wheel shaft, two tank wheels link up with the special reinforced tank track of making 27 circles, at the special reinforced tank track 27 of making a special special caterpillar block 28 of making is arranged, a traction hook 29 that carrier-borne aircraft is drawn is arranged on it.On carrier-borne aircraft takes off the underdeck in acceleration equipment cabin 8, front main battle tank water-cooled diesel motor mount pad 21 is arranged, with rear main battle tank water-cooled diesel motor mount pad 22, two main battle tanks are equipped with front main battle tank water-cooled diesel motor 13 and rear main battle tank water-cooled diesel motor 14 with water-cooled diesel motor mount pad on it.Front main battle tank links together by front gear box 25 and front tank wheel 17 with water-cooled diesel motor 13, and rear main battle tank links together by rear transmission gear box 26 and rear tank wheel 18 with water-cooled diesel motor 14.Front main battle tank is with front clutch 23 between water-cooled diesel motor 13 and the front gear box 25, and rear main battle tank is with power-transfer clutch 24 after having between water-cooled diesel motor 14 and the rear transmission gear box 26.Front fuel tank 9 and front water tank 11 are installed in the back side that front main battle tank is used water-cooled diesel motor 13, and rear fuel tank 10 and rear water box 12 are installed in the back side that rear main battle tank is used water-cooled diesel motor 14.The inside of the reinforced tank track 27 of the special manufacturing in the middle of two tanks wheel has a track adjusting wheel 30 a cranking traction electrical motor 32 to be arranged on it, is installed in carrier-borne aircraft by track adjusting wheel mounting bracket 31 and takes off on the underdeck in acceleration equipment cabin 8.In the middle of the top of the special reinforced tank track 27 of making, on the deck of lifting up the off section 4 of flying-off deck, have one and can allow the traction hook expose the narrow slit on deck.In the deck narrow slit second half section of lifting up the off section 4 of flying-off deck telescopic brake switch 5 is installed, at the place, flying-off deck battle array position at the narrow slit rear portion, deck of lifting up the off section 4 of flying-off deck a telescopic braking anchor pole 7 is housed.
Claims (9)
1. novel aircraft carrier flying-off deck, it include lift up flying-off deck on the section of lifting up, flat segments and off section, it is characterized in that: have the carrier-borne aircraft acceleration equipment cabin of taking off under the off section of flying-off deck lifting up, there are one in front and one in back two pairs of tank wheel supports a tank wheel respectively be arranged on it in the cabin, the tank wheel is installed on the tank wheel support by wheel shaft, two tank wheels link up with the crawler belt circle, at crawler belt a special special caterpillar block of making are arranged, and a traction hook is arranged on it.On the other driving engine mount pad of tank wheel, there is driving engine to link together by change speed gear box and tank wheel.On the deck of lifting up the off section of flying-off deck place in the middle of crawler belt top, leave the narrow slit that can allow together the traction hook expose flying-off deck.
2. a kind of novel aircraft carrier flying-off deck as claimed in claim 1, it is characterized in that: its driving engine that adopts is two main battle tank water-cooled diesel motors one in front and one in back, link together by former and later two change speed gear boxs and two tank wheels respectively, it has separately fuel tank and water tank.
3. a kind of novel aircraft carrier flying-off deck as claimed in claim 1, it is characterized in that: its crawler belt that adopts is the special reinforced tank track of making.
4. a kind of novel aircraft carrier flying-off deck as claimed in claim 1 is characterized in that: on the track adjusting wheel mounting bracket on carrier-borne aircraft takes off the equipment compartment underdeck, a track adjusting wheel is installed has the cranking traction electrical motor on it.
5. a kind of novel aircraft carrier flying-off deck as claimed in claim 1, it is characterized in that: the inner face at tank track has mounted rubber plate.
6. a kind of novel aircraft carrier flying-off deck as claimed in claim 1 is characterized in that: between driving engine and change speed gear box power-transfer clutch is installed.
7. a kind of novel aircraft carrier flying-off deck as claimed in claim 1, it is characterized in that: the wheel shaft between tank wheel support and change speed gear box is equipped with brake.
8. a kind of novel aircraft carrier flying-off deck as claimed in claim 1, it is characterized in that: in the second half section of lifting up the off break deck narrow slit of flying-off deck place telescopic brake switch is installed, and near end place the telescopic switch that declutches is installed at this narrow slit.
9. a kind of novel aircraft carrier flying-off deck as claimed in claim 1, it is characterized in that: the place, battle array position of taking off after lifting up the off break deck narrow slit of flying-off deck is equipped with a telescopic braking anchor pole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101925881A CN102862684A (en) | 2011-07-05 | 2011-07-05 | Novel aircraft carrier flying-off deck |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101925881A CN102862684A (en) | 2011-07-05 | 2011-07-05 | Novel aircraft carrier flying-off deck |
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| Publication Number | Publication Date |
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| CN102862684A true CN102862684A (en) | 2013-01-09 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011101925881A Pending CN102862684A (en) | 2011-07-05 | 2011-07-05 | Novel aircraft carrier flying-off deck |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104108473A (en) * | 2013-04-22 | 2014-10-22 | 陈俞任 | Runway-free multi-aircraft simultaneous take-off high-speed aircraft carrier with submarines |
| CN105015790A (en) * | 2015-08-17 | 2015-11-04 | 陈穗 | Airplane takeoff assisting system of marine worm and wormwheel device |
| CN105667822A (en) * | 2016-03-30 | 2016-06-15 | 代翔 | Aircraft cyclic transfer traction system |
| CN105775153A (en) * | 2016-03-23 | 2016-07-20 | 马同金 | Dragging device for aircraft carrier catapult |
| CN105882974A (en) * | 2016-05-13 | 2016-08-24 | 中国航空工业集团公司西安飞机设计研究所 | Air cargo position adjusting device |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2926872A (en) * | 1957-03-15 | 1960-03-01 | Thiokol Chemical Corp | Aircraft launching apparatus |
| US2969942A (en) * | 1959-07-28 | 1961-01-31 | Charles M Scheuerman | Catapult return system |
| CN1419508A (en) * | 2000-02-24 | 2003-05-21 | 弗雷德里克·让-皮埃尔·德莫勒 | An acceleration system |
| CN101300173A (en) * | 2005-10-12 | 2008-11-05 | 东海旅客铁道株式会社 | Acceleration device |
| CN201385785Y (en) * | 2009-03-31 | 2010-01-20 | 王力丰 | Aircraft carrier launching device |
| CN101758930A (en) * | 2009-12-28 | 2010-06-30 | 刘国忠 | Dynamic acceleration runway for take-off of carrier aircraft |
| CN201784808U (en) * | 2010-06-22 | 2011-04-06 | 吕铁燕 | Launching catapult for carrier-based aircraft |
| CN102107737A (en) * | 2010-09-19 | 2011-06-29 | 朱惠芬 | Front-pull rear-push aircraft carrier ejector and ejection method |
-
2011
- 2011-07-05 CN CN2011101925881A patent/CN102862684A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2926872A (en) * | 1957-03-15 | 1960-03-01 | Thiokol Chemical Corp | Aircraft launching apparatus |
| US2969942A (en) * | 1959-07-28 | 1961-01-31 | Charles M Scheuerman | Catapult return system |
| CN1419508A (en) * | 2000-02-24 | 2003-05-21 | 弗雷德里克·让-皮埃尔·德莫勒 | An acceleration system |
| CN101300173A (en) * | 2005-10-12 | 2008-11-05 | 东海旅客铁道株式会社 | Acceleration device |
| CN201385785Y (en) * | 2009-03-31 | 2010-01-20 | 王力丰 | Aircraft carrier launching device |
| CN101758930A (en) * | 2009-12-28 | 2010-06-30 | 刘国忠 | Dynamic acceleration runway for take-off of carrier aircraft |
| CN201784808U (en) * | 2010-06-22 | 2011-04-06 | 吕铁燕 | Launching catapult for carrier-based aircraft |
| CN102107737A (en) * | 2010-09-19 | 2011-06-29 | 朱惠芬 | Front-pull rear-push aircraft carrier ejector and ejection method |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104108473A (en) * | 2013-04-22 | 2014-10-22 | 陈俞任 | Runway-free multi-aircraft simultaneous take-off high-speed aircraft carrier with submarines |
| CN104108473B (en) * | 2013-04-22 | 2016-07-27 | 陈俞任 | Exempt from runway multimachine with flying band submarine high speed aircraft carrier |
| CN105015790A (en) * | 2015-08-17 | 2015-11-04 | 陈穗 | Airplane takeoff assisting system of marine worm and wormwheel device |
| CN105775153A (en) * | 2016-03-23 | 2016-07-20 | 马同金 | Dragging device for aircraft carrier catapult |
| CN105775153B (en) * | 2016-03-23 | 2018-11-02 | 马同金 | A kind of towing device of aircraft carrier ejector |
| CN105667822A (en) * | 2016-03-30 | 2016-06-15 | 代翔 | Aircraft cyclic transfer traction system |
| CN105667822B (en) * | 2016-03-30 | 2018-07-27 | 成都天空营地科技有限公司 | A kind of aircraft cyclic transfer trailer system |
| CN105882974A (en) * | 2016-05-13 | 2016-08-24 | 中国航空工业集团公司西安飞机设计研究所 | Air cargo position adjusting device |
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Application publication date: 20130109 |