CN201737161U - Aircraft carrier aircraft taking-off run-up device - Google Patents
Aircraft carrier aircraft taking-off run-up device Download PDFInfo
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- CN201737161U CN201737161U CN2010202898134U CN201020289813U CN201737161U CN 201737161 U CN201737161 U CN 201737161U CN 2010202898134 U CN2010202898134 U CN 2010202898134U CN 201020289813 U CN201020289813 U CN 201020289813U CN 201737161 U CN201737161 U CN 201737161U
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- 229910000831 Steel Inorganic materials 0.000 claims abstract description 24
- 239000010959 steel Substances 0.000 claims abstract description 24
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 15
- 229910052742 iron Inorganic materials 0.000 claims description 7
- 238000012423 maintenance Methods 0.000 abstract description 5
- 230000003028 elevating effect Effects 0.000 abstract 4
- 238000010276 construction Methods 0.000 abstract 1
- 238000005265 energy consumption Methods 0.000 abstract 1
- 230000001133 acceleration Effects 0.000 description 4
- 230000006837 decompression Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 241000209202 Bromus secalinus Species 0.000 description 2
- 230000002950 deficient Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241000196324 Embryophyta Species 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011033 desalting Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000021715 photosynthesis, light harvesting Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
An aircraft carrier aircraft taking-off run-up device belongs to deck facilities on an aircraft carrier, and particularly relates to an accelerator used when a carrier aircraft takes off. The device is arranged on a deck of an aircraft, and is characterized in that an embedded type elevating platform pit is arranged on the deck at the taking-off end of the aircraft, and a hydraulic elevating platform is fixedly mounted in the elevating platform pit; a run-up vehicle is equipped with a traction steel cable and a reset steel cable connected with a drive device; and the run-up vehicle is located on the hydraulic elevating platform, and the aircraft is located on the run-up vehicle. The utility model has the advantages of novel conception, simple and reasonable structure, and easy implementation, the aircraft can be accelerated to take off under the double action of the run-up vehicle and the aircraft, the aircraft can take off rapidly with a short take-off distance, and the length of the aircraft carrier can be shortened; the equipment has light weight, the occupied space is small, and the cost of construction is low; the maintenance is convenient, the maintenance personnel is greatly reduced, and the running and maintenance costs are low; the energy utilization rate is improved, and the energy consumption is reduced; and the use range is wide, various aircrafts can use the device to take off, and the fighting capacity is improved.
Description
Technical field
The utility model belongs to the aircraft-carrier-deck facility, relates in particular to the acceleration device of ship-board aircraft when taking off.
Background technology
The aircraft carrier ship-board aircraft berths above deck, landing.Current, ship-board aircraft adopts sliding taking off more and catapult-assisted take-off usually.
Described cunning is taken off more, and the takeoff and landing deck end of aircraft carrier is arranged to upwarp the slope, takes off the back and forms inclined throw movements along upwarping the slope, goes out the deck, flies to blue sky.Sliding lift-off technology content is low more, and device is simple.The defective that exists is the bosun, and it is slow to take off; The maximum take-off weight of taking off is restricted, and early warning plane can not take off; Fighting capacity is low.
Described catapult-assisted take-off is provided with ejector, is with the slide block on the high pressure steam promotion piston drive ejection orbit, and ship-board aircraft is launched away.It has taken off than much progress more than sliding, but has obvious defects: bulky, for producing and delivering vapor, to possess sea water desalting plant, large-sized boiler and numerous and diverse pipeline on the aircraft carrier; Maintenance workload is big, and service personnel is many; Water consumption is big, and energy resource consumption is many, and boiler wants continuous running to produce steam, will consume a large amount of steam during work, takes off and once consumes water vapour more than 1 ton, and energy-output ratio is too big; Steam utilization has only about 6%, and energy dissipation is serious; This device is too big because launch power, still can't launch robot airplane.
Summary of the invention
In order to overcome the defective that prior art exists, the purpose of this invention is to provide a kind of carrier ship-board aircraft run-up device that takes off, improve and take off performance, shorten coasting distance,, simplify the structure of launching apparatus so that shorten the warship body length, alleviate weight of equipment, energy savings is improved its combat capabilities.
The carrier ship-board aircraft run-up device that takes off is located on the deck of aircraft carrier, be characterized in establishing on the described deck of taking off end flush type bay-lift hole, hydaulic lift platform is packed in the bay-lift hole, hydraulic gear drives hydaulic lift platform and rises, descends, and its stroke is equivalent to the height of run-up car; The run-up car is established traction steel rope of cable, the steel cable that resets is connected with actuating device; The run-up car is seated on the hydaulic lift platform, and aircraft is seated on the run-up car.
Establish automobile-used groove shape track of run-up and opening steel cable guide groove on the described deck, its A/F is 2-3cm.
Establish launching platform on the described run-up car, its length is suitable with airframe length, and width slightly is wider than the airplane rising and landing wheel width; The landing of establishing wheel pressure sensor and aircraft on the launching platform is taken turns corresponding, the sound and light signal when the accurate position that testing airplane takes off, transmission over radio pressure-bearing and decompression; Shifting board is established in the launching platform rear end, the steel cable adaptor union is connected with traction steel rope of cable, the steel cable that resets; Launching platform divide into wheel to and buting iron, wheel is to rolling on the hydaulic lift platform rail level, separates with the run-up car when buting iron prevents that aircraft from starting.
Described hydaulic lift platform is divided into hydraulic gear, and hydraulic gear is packed in bottom, bay-lift hole, and hydraulic gear drives the lifting of bay-lift, establish two groove shape tracks on the hydaulic lift platform table top, with the wheel of run-up car to matching, with deck groove shape track gauge from equating, and overlap; Also establishing electromagnetic lock on the hydaulic lift platform is connected with the buting iron that the run-up car is established.
When aircraft does not take off, hydaulic lift platform is in extreme lower position, run-up car launching platform table top is consistent with the aircraft carrier deck level, aircraft reaches run-up car launching platform as usual, the landing wheel of aircraft drops on the wheel pressure sensor of run-up car exactly, the instruction hydaulic lift platform rises after obtaining sound and light signal, holds up run-up car and aircraft, and is concordant with deck level until the hydaulic lift platform rail level.Chaufeur slams brake, and open the throttle wide is to maximum rating, and the run-up car starts and quickens rapidly, and its acceleration/accel is far longer than the acceleration/accel that aircraft self takes off; When aircraft under self thrust and the effect of run-up car tractive force, obtain to quicken the higher acceleration/accel that slides than the independent power of aircraft; When aircraft nose wheel will leave the run-up car, the wheel pressure sensor decompression of front-wheel was also sent sound and light signal, and chaufeur is the pull-up jociey stick immediately, and aircraft continues lift-off from car.The run-up car certain distance that then advances under effect of inertia stops, and returns the lifting hole then, and hydaulic lift platform descends, and the launching platform of run-up car is concordant with the deck again, uses when taking off once more.
Compared with prior art, the utility model has the advantages that:
1, novel, structural reduction, reasonable is implemented easily, and aircraft quickens to take off under the dual dynamic effect of run-up car and aircraft, takes off rapidly, and the time is short, and the take off distance weak point can shorten the warship body length.
2, weight of equipment is light, takes up room to significantly reduce, and cost is low; Be convenient to safeguard that service personnel is few, operation and maintenance cost is low.
3, improve capacity usage ratio, the departure time only continues 3-4 time second, and energy resource consumption reduces greatly.
4, range of use is wide, and all kinds of can taking off aircraft is improved its combat capabilities.
Description of drawings
The carrier-borne run-up apparatus structure scheme drawing that flies up of Fig. 1 aircraft carrier.
Fig. 2 is the birds-eye view of Fig. 1.
Fig. 3 is that the A of Fig. 2 is to view.
Fig. 4 is the A-A cross sectional drawing of Fig. 2.
The specific embodiment
By Fig. 1, Fig. 2, Fig. 3, Fig. 4 as can be seen, the carrier ship-board aircraft run-up device that takes off is located on the deck 13.Establish twice groove shape track 14 on the deck 13, the run-up wheel rolls in track to 6 and moves ahead.If opening steel cable guide groove 15, traction steel rope of cable 8 place opening steel cable guide groove 15.The end that takes off on deck 13 is established flush type bay-lift hole 12, hydaulic lift platform 9 is divided into hydraulic gear 11 and is packed in bay-lift and cheats 12 bottoms, drive hydaulic lift platform 9 liftings by hydraulic gear 11, concordant during hydaulic lift platform 9 most significant bits with 13 planes, deck, during hydaulic lift platform 9 lowest orders, run-up car 1 table top is concordant with 13 planes, deck.
Establish launching platform 2 on the run-up car 1, launching platform 2 is cheated 12 length with bay-lift, width is corresponding, and its length is suitable with aircraft 16 fuselage length, width than aircraft after two landings wheel width slightly wide.Hydaulic lift platform 9 is reduced to low level during standby, and launching platform 2 covers bay-lift hole 12.It is corresponding with aircraft 16 front and back landing wheels to establish three sensors 3 on the launching platform 2, and the landing wheel is pressed on the sensor 3 before taking off, and testing airplane 16 accurate takeoff settings just can be instructed when the front-wheel decompression in the accelerator and be taken off.Shifting board 4, steel cable adaptor union 5 and traction steel rope of cable 8, the steel cable 8 that resets ' be connected are established in launching platform 2 rear ends.When run-up car one starting shifting board 4 promptly rises, prevent that aircraft 16 from separating with run-up car 1.Shifting board 4 fell when run-up car 1 resetted.The launching platform 2 of run-up car 1 is divided into wheel to 6, matches with the groove shape track that hydaulic lift platform 9 is established, and is seated on the hydaulic lift platform 9 groove shape tracks.Launching platform 2 is divided into buting iron 7, is connected with the electromagnetic lock 10 that hydaulic lift platform 9 is established.Traction steel rope of cable 8 and the steel cable 8 that resets ' be connected with actuating device (among the figure mark).When taking off, actuating device traction run-up car 1 starts rapidly, quickens, and drives aircraft 16 and moves ahead, and when run-up car 1 resets, is resetted by the steel cable 8 that resets ' pulling.
Establish two groove shape tracks on the platform of hydaulic lift platform 9, its gauge equates 6 gauge, groove shape track 14 gauges on deck 13 with the run-up wheel, and is connected mutually with deck 13 groove shape tracks 14.During starting, run-up car starting rapidly moves ahead along the groove shape track 14 on bay-lift track and the deck, makes aircraft 16 reach takeoff speed rapidly.Establish electromagnetic lock 10 on the hydaulic lift platform 9 and be connected mutually with the buting iron 7 that run-up car 1 is established, electromagnetic lock 10 is just opened when the actuating device of traction steel rope of cable 8 is started by electricity, and run-up car 1 is freely moved ahead.Electromagnetic lock 10 closures during dead electricity are pinned the run-up car 1 after returning automatically.Hydaulic lift platform 9 is divided into hydraulic gear 11, and hydraulic gear 11 is packed in bay-lift and cheats 12 bottoms, and hydraulic gear 11 bears the total weight of bay-lift 9, run-up car 1 and aircraft 16.
During standby, aircraft 16 reaches the run-up car, and run-up car 1 is seated on the hydaulic lift platform 9, and hydraulic gear 11 jack-up bay-lifts 9 are concordant with 13 planes, deck.When taking off, run-up car 1 rolls rapidly along the groove shape track 14 on bay-lift and deck and moves ahead, and reaches takeoff speed until aircraft, and aircraft 16 quickens to take off again on the launching platform 2 of run-up car 1.
Claims (4)
1. the carrier ship-board aircraft run-up device that takes off is located on the deck (13) of aircraft carrier, it is characterized in that the end of taking off on described deck (13) is established flush type bay-lift hole (12), and hydaulic lift platform (9) is packed in the bay-lift hole (12); Run-up car (1) is established traction steel rope of cable (8), the steel cable that resets (8 ') is connected with actuating device, and the aircraft that takes off (16) is seated on the run-up car (1), and run-up car (1) is seated on the hydaulic lift platform (9).
2. the carrier ship-board aircraft according to claim 1 run-up device that takes off is characterized in that establishing on the described deck (13) the groove shape track (14) and the opening steel cable guide groove (15) of run-up car (1) usefulness, and its A/F is 2-3cm.
3. the carrier ship-board aircraft according to claim 1 run-up device that takes off is characterized in that establishing launching platform (2) on the described run-up car (1), and length is suitable with airframe length, and width slightly is wider than aircraft (16) landing wheel width; It is corresponding with the landing wheel of aircraft (16) to establish wheel pressure sensor (3) on the launching platform (2), and the landing wheel is pressed on the sensor (3); Shifting board (4) is established in launching platform (2) rear end, steel cable adaptor union (5) is connected with traction steel rope of cable (8), the steel cable that resets (8 '); Launching platform (2) is divided into wheel to (6) and buting iron (7).
4. the carrier ship-board aircraft according to claim 1 run-up device that takes off, it is characterized in that described hydaulic lift platform (9) divides into hydraulic gear (11), hydraulic gear (11) is packed in bottom, bay-lift hole (12), establishing two groove shape tracks on hydaulic lift platform (9) table top matches to (6) with the wheel of run-up car (1), equate with deck (13) fovea superior channel suspending rail (14) gauge, and overlap; Also establishing electromagnetic lock (10) on the hydaulic lift platform (9) is connected mutually with buting iron (7) on the run-up car (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202898134U CN201737161U (en) | 2010-08-05 | 2010-08-05 | Aircraft carrier aircraft taking-off run-up device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202898134U CN201737161U (en) | 2010-08-05 | 2010-08-05 | Aircraft carrier aircraft taking-off run-up device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201737161U true CN201737161U (en) | 2011-02-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010202898134U Expired - Fee Related CN201737161U (en) | 2010-08-05 | 2010-08-05 | Aircraft carrier aircraft taking-off run-up device |
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| Country | Link |
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| CN (1) | CN201737161U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105151312A (en) * | 2015-09-30 | 2015-12-16 | 罗元建 | Buried type automatic aircraft traction system and traction method |
| CN106697319A (en) * | 2017-01-17 | 2017-05-24 | 张其予 | Aircraft takeoff traction apparatus |
| CN107539495A (en) * | 2017-07-24 | 2018-01-05 | 陆永俊 | One kind takes off accelerator |
| CN106275391B (en) * | 2016-08-19 | 2018-10-26 | 姚立波 | The disengaged land undercarriage of aircraft |
| RU2739477C1 (en) * | 2020-01-20 | 2020-12-24 | Федеральное государственное бюджетное образовательное учреждение высшего образования Балтийский государственный технический университет "ВОЕНМЕХ" им. Д.Ф. Устинова (БГТУ "ВОЕНМЕХ") | Mobile launcher unit |
-
2010
- 2010-08-05 CN CN2010202898134U patent/CN201737161U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105151312A (en) * | 2015-09-30 | 2015-12-16 | 罗元建 | Buried type automatic aircraft traction system and traction method |
| CN105151312B (en) * | 2015-09-30 | 2018-01-16 | 罗元建 | Embedded autoplane trailer system and traction method |
| CN106275391B (en) * | 2016-08-19 | 2018-10-26 | 姚立波 | The disengaged land undercarriage of aircraft |
| CN106697319A (en) * | 2017-01-17 | 2017-05-24 | 张其予 | Aircraft takeoff traction apparatus |
| CN106697319B (en) * | 2017-01-17 | 2023-04-11 | 张其予 | Traction device for take-off of airplane |
| CN107539495A (en) * | 2017-07-24 | 2018-01-05 | 陆永俊 | One kind takes off accelerator |
| RU2739477C1 (en) * | 2020-01-20 | 2020-12-24 | Федеральное государственное бюджетное образовательное учреждение высшего образования Балтийский государственный технический университет "ВОЕНМЕХ" им. Д.Ф. Устинова (БГТУ "ВОЕНМЕХ") | Mobile launcher unit |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110209 Termination date: 20110805 |