CN106347698B - Aircraft carrier launching apparatus - Google Patents
Aircraft carrier launching apparatus Download PDFInfo
- Publication number
- CN106347698B CN106347698B CN201610876039.9A CN201610876039A CN106347698B CN 106347698 B CN106347698 B CN 106347698B CN 201610876039 A CN201610876039 A CN 201610876039A CN 106347698 B CN106347698 B CN 106347698B
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- air
- air outlet
- platform
- aircraft
- setting
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- 230000001174 ascending effect Effects 0.000 claims abstract description 23
- 230000008859 change Effects 0.000 claims abstract description 5
- 230000036651 mood Effects 0.000 claims description 4
- 238000002955 isolation Methods 0.000 claims description 3
- 230000009467 reduction Effects 0.000 claims description 3
- 230000008901 benefit Effects 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000035899 viability Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
Abstract
Aircraft carrier launching apparatus, main body includes sliding platform (11), air outlet (10), flow generator (7), it is characterized by: the end place of upwarping setting air outlet (10) for sliding platform (11), air outlet (10) at least one set be horizontally installed on slide platform (11) upwarp end, the opening upwards of air outlet (10) tilt upward, it is formed ascending air (8), ascending air (8) and the end that upwarps for sliding platform (11) form angle with platform (11) front is slided, ascending air (8) blows to aircraft (1) bottom slided on platform (11), it forms lifting force or is lifted the direction that air-flow face change of flight device (1) moves horizontally, aircraft (1) is tilted upward be sent from slide platform (11) upwarp end.
Description
Technical field
The present invention relates to launching apparatus, in particular to aircraft carrier launching apparatus.
Background technique
Chinese patent literature CN102120497A disclosed enclosed cylinder aircraft carrier steam on 07 13rd, 2011
Ejector provides enclosed cylinder carrier aircraft steam catapult, can be up to the purpose of ejection aircraft takeoff.It is of the present invention
Enclosed cylinder carrier aircraft steam catapult passes through the enclosed cylinder slide opening through good lubrication and sealing, both ends using leash
Connect respectively with piston and tractor, and through commutation into rotation to, formed the specific shuttling movement mechanism of ejector.Piston benefit
It is moved with leash driving tractor, and then airplane catapult is driven to take off.Leash is made of highly elastic material, and section is flat
It is flat-shaped, there is lesser bending radius in flat direction.When by commutation tensioning wheel, leash bending becomes in perfect elasticity
Shape state will not be damaged because of flexural fatigue.Device of the present invention have go slick, reliable performance, high-efficient, volume
It small, water-saving, the advantages that structure is simple, easily fabricated, infrared signature is small, is installed and used suitable for aircraft carrier, to accelerating China's aircraft carrier
Speed is developed, improves aircraft carrier fighting capacity, viability is of great significance.
Since structure is complicated, bulky for steam catapult, therefore, it is necessary to be further improved.
Summary of the invention
The purpose of the present invention is intended to provide a kind of simple and reasonable, easy to operate, durable, reliable performance, this boat
Female launching apparatus structure is simple, at low cost, to overcome shortcoming in the prior art.
By the aircraft carrier launching apparatus that this purpose designs, main body includes sliding platform, air outlet, flow generator, feature
Be: the end place of the upwarping setting air outlet for sliding platform, air outlet at least one set, which is horizontally installed on, slides the upper of platform
Stick up end, the opening upwards of air outlet or tilt upward, form ascending air, ascending air and slide platform upwarp end and
It slides platform front and forms angle, ascending air blows to the aircraft bottom slided on platform, forms lifting force or lifting air-flow
The direction that face change of flight device moves horizontally, aircraft is tilted upward be sent from slide platform upwarp end.
The air outlet intersects setting with the end that upwarps for sliding platform；
The air outlet orientation outlet air setting or adjustable deflecting outlet air setting, adjustable deflecting outlet air are rotated real by wind deflector
It is existing；
The air-out direction of the air outlet is upward or tilts upward；The air outlet is gradually risen by front end to end, shape
At an inclined outlet air discharge surface；
The wind deflector of the air outlet is erect to the wind deflector of inclination ordered arrangement or the air outlet and is erect by tilting to
Along aircraft advance moving direction ordered arrangement；The end that upwarps for sliding platform is arranged in the air inlet of the flow generator
Side or bottom, air inlet and air outlet form angle, eliminate swirling eddy caused by air inlet or outlet；
Wind deflector on the outside of the air outlet tilts wind to outside, and external ambient windstream is stopped outward, formed every
From air-flow wall, reduce aircraft takeoff influenced by ambient windstream.
One group of the wind-guiding front edge of board is obliquely installed, and is guided out general mood stream into line tilt, by aircraft bottom forward,
It blows upwards and holds up aircraft at least part weight, front air deflector a line to end wind deflector a line, every row arranges gradually
It erects, generates the three-dimensional ascending air for tilting to setting.
The air outlet and flow generator perforation connect, and flow generator, which is arranged in, slides the upwarping in end of platform
Portion, flow generator air inlet, which is arranged in, slides upwarping end one or both sides or bottom or sliding on platform front end for platform
Portion.
The flow generator is turbofan or paddle fan or axial-flow fan, is evenly spaced in the lower part of air outlet or goes out
Inlet front end.
The wind deflector is rotatablely connected electrically-controlled component, and motor, gear, connecting rod, wind deflector and connecting rod is arranged on electrically-controlled component
It is flexibly connected, connecting rod drives wind deflector to swing back and forth.
The air outlet setting is in strip netted platform, and wind deflector is set to one of the netted platform of air outlet bar shaped
Part.
The present invention is interacted between end and ascending air by sliding upwarping for platform, by the horizontal power of aircraft
A is converted into rising thrust by the area blocking of ascending air and aircraft bottom gradually to be lifted submitting for aircraft and slides platform
The effect of upwarping end, reach 4 two groups of a thousand pieces of gold, thus help aircraft saving fuel oil increase aircraft flight voyage, economy
Efficiently.
So that above-mentioned operation is recycled progress, greatly improves work efficiency.It is with simple and reasonable, operation side
Just, the characteristics of durable, reliable performance.
Detailed description of the invention
Fig. 1 is the schematic diagram that first embodiment of the invention slides platform.
Fig. 2 is the schematic top plan view that first embodiment of the invention slides platform.
Fig. 3 is the schematic elevation view that first embodiment of the invention slides platform.
Fig. 4 is the partial enlargement diagram that first embodiment of the invention slides platform.
Specific embodiment
The invention will be further described with reference to the accompanying drawings and embodiments.
Referring to embodiment (referring to figures 1-4)
Aircraft carrier launching apparatus, main body include sliding platform 11, air outlet 10, flow generator 7, it is characterised in that: described
The end place of the upwarping setting air outlet 10 of platform 11 is slided, 10 at least one set of air outlet, which is horizontally installed on, slides upwarping for platform 11
End, the opening upwards of air outlet 10 or tilts upward, and forms ascending air 8, ascending air 8 and that slides platform 11 upwarp end
It holds and slides 11 front of platform and form angle, ascending air 8 blows to 1 bottom of aircraft slided on platform 11, forms lifting force
Or the direction that moves horizontally of lifting air-flow face change of flight device 1, aircraft 1 is tilted upward be sent from slide platform 11 upwarp end
End.
The air outlet 10 intersects setting with the end that upwarps for sliding platform 11；
The air outlet 10 orients outlet air setting or adjustable deflecting outlet air setting, adjustable deflecting outlet air are rotated by wind deflector 2
It realizes.
The air-out direction of the air outlet 10 is upward or tilts upward；The air outlet 10 is gradually risen by front end to end
Height forms an inclined outlet air discharge surface；
The wind deflector 2 of the air outlet 10 is erect to the wind deflector 2 of inclination ordered arrangement or the air outlet 10 by tilting
To setting along 1 advance moving direction ordered arrangement of aircraft.
One group of 2 front end of wind deflector is obliquely installed, and is guided out general mood stream into line tilt, by 1 bottom of aircraft towards
Before, upwards blow hold up 1 at least part weight of aircraft, 2 a line of front air deflector is to 2 a line of end wind deflector, and every row is gradually
Gradually arrangement is erect, and generates the three-dimensional ascending air 8 for tilting to setting.
The air outlet 10 is connected with the perforation of flow generator 7, flow generator 7 be arranged in slide platform 11 upwarp end
End is internal, and 7 air inlet 9 of flow generator, which is arranged in, slides upwarping end one or both sides or bottom or sliding platform for platform 11
11 upper front ends.
The flow generator 7 is turbofan or paddle fan or axial-flow fan 3, is evenly spaced in the lower part of air outlet 10
Or 10 front end of air outlet；
The side or bottom for upwarping end for sliding platform 11, air inlet is arranged in the air inlet 9 of the flow generator 7
9 form angle with air outlet 10, eliminate swirling eddy caused by air inlet or outlet；
The wind deflector in 10 outside of air outlet tilts wind 14 to outside, and external ambient windstream 13 is stopped outward,
The air-flow wall of isolation is formed, reduction aircraft 1 takes off and influenced by ambient windstream 13.
The wind deflector 2 is rotatablely connected electrically-controlled component 4, is arranged motor, gear, connecting rod 6 on electrically-controlled component 4, wind deflector 2 with
Connecting rod 6 is flexibly connected, and connecting rod drives wind deflector 2 to swing back and forth.
The setting of air outlet 10 is in strip netted platform, and wind deflector 2 is set to the netted platform of 10 bar shaped of air outlet
It is a part of.
Aircraft 1 is moved on sliding platform 11 by horizontal power A promotion, slides the gas of platform 11 upwarped on end
Flow-generator 7 generates air-flow by the outflow conversion ascending air of air outlet 10, ascending air and 1 horizontal power of aircraft join by
The moving direction of aircraft 1 changes to deviate and rise；
The body of aircraft 1 and wing bottom stop the ascending air inertia force that generation lift touches aircraft 1 relatively will
The inclination of aircraft 1 send out slide platform 11 upwarp end；
One group of 2 front end of wind deflector is obliquely installed, and is guided out general mood stream into line tilt, by 1 bottom of aircraft forward, to
On blow hold up 1 at least part weight of aircraft, 2 a line of front air deflector to 2 a line of end wind deflector, the gradually high arrangement of every row
It erects, the inertia force that the three-dimensional ascending air that generation tilts to setting touches aircraft 1, which sends out the inclination of aircraft 1, slides platform
11 upwarp end；
The wind deflector in 10 outside of air outlet tilts wind 14 to outside, and external ambient windstream 13 is stopped outward, is formed
The air-flow wall of isolation, reduction aircraft 1 take off and are influenced by ambient windstream 13, guarantee ascending air and 1 horizontal power of aircraft
It joins to change the moving direction of aircraft 1 to deviate and rise；Every row gradually erect by high arrangement, generates and tilts to the front end of setting to rear
The inertia force that blowing force three-dimensional ascending air in the same size in end touches aircraft 1, which sends out the inclination of aircraft 1, slides the upper of platform 11
Stick up end.
The aircraft 1 that the air-out direction that air outlet is adjusted in wind deflector 2 adapts to different weight takes off.
Above-mentioned is preferred embodiment of the invention, and basic principles and main features and the present invention of the invention have been shown and described
The advantages of.Those skilled in the art should be recognized that the present invention is not limited to the above embodiments, above embodiments and description
Described in merely illustrate the principles of the invention, without departing from the spirit and scope of the present invention, the present invention also has respectively
Kind changes and improvements, these changes and improvements all fall within the protetion scope of the claimed invention.The claimed scope of the invention by
Appended claims and its equivalent define.
Claims (1)
1. aircraft carrier launching apparatus, main body includes sliding platform (11), air outlet (10), flow generator (7), it is characterised in that:
It is described slide platform (11) the end place of upwarping setting air outlet (10), air outlet (10) at least one set be horizontally installed on slide it is flat
Platform (11) upwarps end, the opening upwards of air outlet (10) or tilts upward, and is formed ascending air (8), ascending air (8) and
The end that upwarps for sliding platform (11) forms angle with platform (11) front is slided, and ascending air (8), which blows to, slides platform (11)
On aircraft (1) bottom, form lifting force or be lifted air-flow face change of flight device (1) direction for moving horizontally, by aircraft
(1) tilt upward be sent from slide platform (11) upwarp end；The air outlet (10) upwarps end with slide platform (11)
Intersection setting；Air outlet (10) the orientation outlet air setting or adjustable deflecting outlet air setting, adjustable deflecting outlet air is by wind deflector (2)
Rotation is realized；
The air-out direction of the air outlet (10) is upward or tilts upward；The air outlet (10) is gradually risen by front end to end
Height forms an inclined outlet air discharge surface；
The wind deflector (2) of the air outlet (10) erect to the wind deflector (2) of inclination ordered arrangement or the air outlet (10) by
Setting is tilted to along aircraft (1) advance moving direction ordered arrangement；
One group of wind deflector (2) front end is obliquely installed, and is guided out general mood stream into line tilt, by aircraft (1) bottom towards
Before, upwards blow hold up aircraft (1) at least part weight, front air deflector (2) a line to end wind deflector (2) a line,
Every row arranges setting gradually, generates the three-dimensional ascending air (8) for tilting to setting；
The air outlet (10) and flow generator (7) perforation connect, and the upper of platform (11) is being slided in flow generator (7) setting
Stick up terminus inner, flow generator (7) air inlet (9) setting upwarps end one or both sides or bottom slide platform (11)
Or slide platform (11) upper front end；
The flow generator (7) is turbofan or paddle fan or axial-flow fan (3), is evenly spaced under air outlet (10)
Portion or air outlet (10) front end；
The wind deflector (2) is rotatablely connected electrically-controlled component (4), and motor, gear, connecting rod (6), wind-guiding are arranged on electrically-controlled component (4)
Plate (2) is flexibly connected with connecting rod (6), and connecting rod drives wind deflector (2) to swing back and forth；
Air outlet (10) setting is in strip netted platform, and wind deflector (2) is set to the netted platform of air outlet (10) bar shaped
Some；
Air inlet (9) setting of the flow generator (7) is in the side or bottom for upwarping end for sliding platform (11), air inlet
Mouth (9) and air outlet (10) form angle, eliminate swirling eddy caused by air inlet or outlet；
Wind deflector on the outside of the air outlet (10) tilts wind (14) to outside, by external ambient windstream (13) to extrernal resistance
It blocks, forms the air-flow wall of isolation, reduction aircraft (1) is taken off and influenced by ambient windstream (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610876039.9A CN106347698B (en) | 2016-10-08 | 2016-10-08 | Aircraft carrier launching apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610876039.9A CN106347698B (en) | 2016-10-08 | 2016-10-08 | Aircraft carrier launching apparatus |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106347698A CN106347698A (en) | 2017-01-25 |
| CN106347698B true CN106347698B (en) | 2019-08-23 |
Family
ID=57866154
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610876039.9A Active CN106347698B (en) | 2016-10-08 | 2016-10-08 | Aircraft carrier launching apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106347698B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101244764A (en) * | 2008-03-07 | 2008-08-20 | 王刚 | Cascade connection type hybrid power ejection propulsion vehicle for takeoff of airplane |
| CN102745333A (en) * | 2012-07-31 | 2012-10-24 | 李文铎 | Internal combustion steam boosting take-off unit of airplane |
| CN104670447A (en) * | 2015-01-29 | 2015-06-03 | 赵凤银 | Aircraft carrier, ship and land-water jet runway system with efficient short-range slide or vertical take-off and landing aircraft units |
| CN105035343A (en) * | 2015-08-13 | 2015-11-11 | 济南环太机电技术有限公司 | Vapor emission type shipboard aircraft carrier catapult |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3038922B1 (en) * | 2013-08-27 | 2019-09-25 | Engineered Arresting Systems Corporation | Electric unmanned aerial vehicle launcher |
-
2016
- 2016-10-08 CN CN201610876039.9A patent/CN106347698B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101244764A (en) * | 2008-03-07 | 2008-08-20 | 王刚 | Cascade connection type hybrid power ejection propulsion vehicle for takeoff of airplane |
| CN102745333A (en) * | 2012-07-31 | 2012-10-24 | 李文铎 | Internal combustion steam boosting take-off unit of airplane |
| CN104670447A (en) * | 2015-01-29 | 2015-06-03 | 赵凤银 | Aircraft carrier, ship and land-water jet runway system with efficient short-range slide or vertical take-off and landing aircraft units |
| CN105035343A (en) * | 2015-08-13 | 2015-11-11 | 济南环太机电技术有限公司 | Vapor emission type shipboard aircraft carrier catapult |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106347698A (en) | 2017-01-25 |
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