CN106364691A - Catapult gliding shuttle runway of shipboard aircraft on carrier - Google Patents
Catapult gliding shuttle runway of shipboard aircraft on carrier Download PDFInfo
- Publication number
- CN106364691A CN106364691A CN201610706009.3A CN201610706009A CN106364691A CN 106364691 A CN106364691 A CN 106364691A CN 201610706009 A CN201610706009 A CN 201610706009A CN 106364691 A CN106364691 A CN 106364691A
- Authority
- CN
- China
- Prior art keywords
- runway
- shuttle
- carrier
- traction medium
- traction
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000003754 machining Methods 0.000 claims description 11
- 238000005336 cracking Methods 0.000 claims description 4
- 239000004677 Nylon Substances 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 241000656145 Thyrsites atun Species 0.000 claims description 3
- 239000002131 composite material Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 3
- 229920001778 nylon Polymers 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 abstract 1
- 230000007613 environmental effect Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
- 238000005096 rolling process Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 241001093152 Mangifera Species 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 239000013028 medium composition Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification 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
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Bridges Or Land Bridges (AREA)
Abstract
The present invention provides a catapult gliding shuttle runway of a shipboard aircraft on a carrier. The catapult gliding shuttle runway of the shipboard aircraft on the carrier is structurally composed of a runway ditch, a set of carrier rollers, runway ditch cover plates, a traction medium connecting plate, an I-shaped slider, a traction rod hooking piece and traction medium. The two ends of the set of carrier rollers are arranged in the runway ditch through bearings, carrier rollers of the set of carrier rollers are in rolling connection with the traction medium, the middle of the traction medium is fixed to the traction medium connecting plate through bolts, the traction medium connecting plate is connected with the I-shaped slider at the bottom of a gliding shuttle, the bottoms of the two sets of runway ditch cover plates are connected with an upper opening of the runway ditch, the edges of the middles of the two sets of runway ditch cover plates are in sliding connection with grooves in the two sides of the I-shaped slider, and the top of the I-shaped slider is provided with the shipboard aircraft traction rod hooking piece. The catapult gliding shuttle runway has the beneficial effects that the structure is simple, processing and installation are easy, the use is convenient, the gliding shuttle is lightweight, the friction resistance is small, the power consumption is small, and the good environmental protection and energy saving effects are achieved.
Description
Technical field
The present invention relates to carrier-based aircraft ejector processing technique field, specifically aircraft carrier ejection shuttle runway.
Background technology
The nuclear aircraft carrier in known west uses steam catapult and increases in the Electromagnetical ejector developed, steam ejection
The whole piece runway of device is exactly two open cylinders, and the runway of Electromagnetical ejector is exactly whole piece linear electric motors, and two kinds of ejectors are suitable
Complexity, prices are rather stiff, all in more than hundred million dollars of 1-10, thus only employs steam on the nuclear aircraft carrier of Fructus Mangifera Indicae at present
Ejector and Electromagnetical ejector.
Content of the invention
It is an object of the invention to provide a kind of simple in structure and low in cost, can be in nuclear aircraft carrier or aircraft carrier powered by conventional energy
The aircraft carrier ejection shuttle runway of the towed ejector of synchronous bidirectional of upper use.
The purpose of the present invention is realized in the following manner, and aircraft carrier launches shuttle runway, and its structure is by runway
Ditch, idler machining, runway trench cover, traction medium connecting plate, I shape slide block, traction pike pole connect part and traction medium composition, support
The two ends of roller group are arranged among runway ditch by bearing, and the carrying roller of idler machining is connected with being rolled with traction medium, draws medium
Centre is fixed with traction medium connecting plate by bolt, and traction medium connecting plate is connected with the I shape slide block of shuttle bottom, and two
The bottom of group runway trench cover and the connection suitable for reading of runway ditch, the middle edge of two groups of runway trench covers and I shape slide block both sides
Groove is slidably connected, and the top of I shape slide block arranges carrier-borne motor drawbar hook and connects part；
Described aircraft carrier ejection shuttle runway, the edge suitable for reading of runway ditch is provided with flange, the bottom of runway trench cover
Together with being bolted on flange, two sides of runway trench cover and type aircraft carrier deck are fixed together and form ejection runway.
Traction medium is one of industrial sheet base band, nylon tape or steel wire rope or two or more composite band.
The invention has the beneficial effects as follows: structure is simple, takes up room little, and convenient processing is installed, and can substantially reduce carrier-borne aircraft
The cost of ejector, is slidably connected with runway trench cover using I shape slide block, can effectively reduce shuttle weight, reduces resistance
Power, reduces brake inertia, effectively improves service life, and conventional vapor ejector becomes station a whole set of with the ejection runway of Electromagnetical ejector
The 80% of ejector cost, and the runway cost of belt carrier-based aircraft ejector accounts for the 10% of a whole set of ejector cost, 90% cost is
Power-equipment, power-equipment is common apparatus again, is thus advantageous to popularizing of synchronous mode carrier-based aircraft ejector, is in future
The essential equipment of state's ejector of aircraft carrier shipboard aircraft.
Brief description
Fig. 1 is the section structure schematic diagram that aircraft carrier launches shuttle runway.
Description of reference numerals: runway ditch 1, idler machining 2, runway trench cover 3, traction medium 4, traction medium connecting plate 5,
I shape slide block 6, carrier-borne motor drawbar hook connect part 7.
Specific embodiment
With reference to Figure of description, aircraft carrier of the present invention ejection shuttle runway is described in detail below.
The aircraft carrier ejection shuttle runway of the present invention, is situated between including runway ditch 1, idler machining 2, runway trench cover 3, traction
Matter connecting plate 4, I shape slide block 6, traction pike pole connect part 8 and traction medium, and the two ends of idler machining 2 are arranged on runway by bearing
Among ditch 1, the carrying roller of idler machining 2 is connected with being rolled with traction medium 4, in the middle of traction medium 4 by bolt with traction medium even
Fishplate bar 5 is fixing, and traction medium connecting plate 5 is connected with the I shape slide block of shuttle bottom, the bottom of two groups of runway trench covers 3 and race
Road ditch 1 connection suitable for reading, the middle edge of two groups of runway trench covers 3 is slidably connected with the groove of I shape slide block 6 both sides, I shape
The top of slide block 6 arranges carrier-borne motor drawbar hook and connects part 7；
Described aircraft carrier ejection shuttle runway, the edge suitable for reading of runway ditch 1 is provided with flange, the bottom of runway trench cover 3
Together with portion is bolted on flange, two sides of runway trench cover 3 and type aircraft carrier deck are fixed together and form ejection race
Road.
Traction medium is one of industrial sheet base band, nylon tape or steel wire rope or two or more composite band.
Embodiment
Using method is as follows:
Make guide slit with middle the cracking of runway cover plate, I shape slide block is embedded in cracking, I shape slider bottom passes through to slide
Shuttle connecting plate with traction medium is connected, traction medium two ends respectively at ejection module and playback module connect, ejection module with
Playback module takes off for carrier-borne aircraft and provides hauling speed and power to respectively shuttle forward direction hauling speed and pull strength, and carrier-borne aircraft rises
After flying, playback module provides reversely traction to make shuttle return to carrier-borne aircraft takeoff setting for shuttle again, and the idler machining in runway ditch is
Traction medium provides to lift and slides to reduce the frictional resistance of traction medium and runway ditch.
The foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, although with reference to aforementioned reality
Apply example the present invention has been described in detail, for a person skilled in the art, it still can be to aforementioned each enforcement
Technical scheme described in example is modified, or carries out equivalent to wherein some technical characteristics.All essences in the present invention
Any modification, equivalent or improvement made within god and principle etc., should be included within the scope of the present invention.
It is the known technology of those skilled in the art in addition to technical characteristic disclosed in the description of the present invention.
Claims (3)
1. aircraft carrier ejection shuttle runway is it is characterised in that include runway ditch, idler machining, runway trench cover, traction medium
Connecting plate, I shape slide block, traction pike pole connect part and traction medium, the two ends of idler machining by bearing be arranged on runway ditch it
In, the carrying roller of idler machining is connected with being rolled with traction medium, is fixed with traction medium connecting plate by bolt in the middle of traction medium,
Traction medium connecting plate is connected with the I shape slide block of shuttle bottom, the bottom of two groups of runway trench covers and runway ditch company suitable for reading
Connect, the middle edge of two groups of runway trench covers is slidably connected with the groove of I shape slide block both sides, the top of I shape slide block sets
Put carrier-borne motor drawbar hook and connect part；
Using method is as follows:
Make guide slit with middle the cracking of runway cover plate, I shape slide block is embedded in cracking, I shape slider bottom passes through to slide
Shuttle connecting plate with traction medium is connected, traction medium two ends respectively at ejection module and playback module connect, ejection module with
Playback module takes off for carrier-borne aircraft and provides hauling speed and power to respectively shuttle forward direction hauling speed and pull strength, and carrier-borne aircraft rises
After flying, playback module provides reversely traction to make shuttle return to carrier-borne aircraft takeoff setting for shuttle again, and the idler machining in runway ditch is
Traction medium provides to lift and slides to reduce the frictional resistance of traction medium and runway ditch.
2. aircraft carrier ejection shuttle runway according to claim 1 is it is characterised in that the edge suitable for reading of runway ditch sets
It is equipped with flange, together with the bottom of runway trench cover is bolted on flange, two sides of runway trench cover and aircraft carrier first
Plate is fixed together and forms ejection runway.
3. aircraft carrier ejection shuttle runway according to claim 1 is it is characterised in that traction medium is industrial chip base
One of band, nylon tape or steel wire rope or two or more composite band.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706009.3A CN106364691A (en) | 2016-08-23 | 2016-08-23 | Catapult gliding shuttle runway of shipboard aircraft on carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706009.3A CN106364691A (en) | 2016-08-23 | 2016-08-23 | Catapult gliding shuttle runway of shipboard aircraft on carrier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106364691A true CN106364691A (en) | 2017-02-01 |
Family
ID=57878502
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610706009.3A Pending CN106364691A (en) | 2016-08-23 | 2016-08-23 | Catapult gliding shuttle runway of shipboard aircraft on carrier |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106364691A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109178335A (en) * | 2018-08-16 | 2019-01-11 | 刘贵文 | A kind of fan gas operated boosting aircraft catapult |
| CN109353492A (en) * | 2018-09-28 | 2019-02-19 | 李模萍 | A kind of method of rising and falling of vehicle orientation rate controlling V-arrangement sliding slot |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2062132A1 (en) * | 1970-12-17 | 1972-07-13 | Beck, Dieter, 7470 Ebingen | Speed control for gliders |
| CN102910295A (en) * | 2012-07-17 | 2013-02-06 | 朱惠芬 | Two-way driving winding speedup type ship-borne aircraft catapult |
| CN105584638A (en) * | 2016-03-14 | 2016-05-18 | 济南环太机电技术有限公司 | Integrated disc-type carrier aircraft landing arresting device and arresting method thereof |
| CN205952336U (en) * | 2016-08-23 | 2017-02-15 | 杨祥红 | Aircraft carrier launches shuttle runway |
-
2016
- 2016-08-23 CN CN201610706009.3A patent/CN106364691A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2062132A1 (en) * | 1970-12-17 | 1972-07-13 | Beck, Dieter, 7470 Ebingen | Speed control for gliders |
| CN102910295A (en) * | 2012-07-17 | 2013-02-06 | 朱惠芬 | Two-way driving winding speedup type ship-borne aircraft catapult |
| CN105584638A (en) * | 2016-03-14 | 2016-05-18 | 济南环太机电技术有限公司 | Integrated disc-type carrier aircraft landing arresting device and arresting method thereof |
| CN205952336U (en) * | 2016-08-23 | 2017-02-15 | 杨祥红 | Aircraft carrier launches shuttle runway |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109178335A (en) * | 2018-08-16 | 2019-01-11 | 刘贵文 | A kind of fan gas operated boosting aircraft catapult |
| CN109353492A (en) * | 2018-09-28 | 2019-02-19 | 李模萍 | A kind of method of rising and falling of vehicle orientation rate controlling V-arrangement sliding slot |
| CN109353492B (en) * | 2018-09-28 | 2022-02-08 | 李模萍 | Landing and landing method for directional speed control V-shaped sliding groove of aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206231638U (en) | A kind of permanent-magnetism linear motor type electromagnetic launch technology of unmanned aerial vehicle device | |
| CN106364691A (en) | Catapult gliding shuttle runway of shipboard aircraft on carrier | |
| CN109502505A (en) | Car lift structure and move electric system certainly | |
| CN207608269U (en) | Car lift structure and move electric system certainly | |
| CN103935266A (en) | Traveling vehicle power supply device | |
| CN108372864B (en) | Vacuum pipeline train magnetic suspension EMS/EDS hybrid bearing structure | |
| CN104691776B (en) | Permanent-magnet linear catapult-launching gear | |
| CN103359295A (en) | Energy-efficient carrier-based aircraft interceptor | |
| CN205952336U (en) | Aircraft carrier launches shuttle runway | |
| CN106477063B (en) | Multipurpose dynamic energy storage type carrier-based aircraft ejector system and its application method | |
| CN201712793U (en) | Novel aircraft catapult | |
| CN209776183U (en) | Magnetic suspension logistics vehicle applied to underground pipe gallery logistics system | |
| RU2012153450A (en) | METHOD FOR CARRIAGE OF PASSENGERS AND CARGOES BY AIR AND SYSTEM FOR TRANSPORTATION OF PASSENGERS AND CARGOES BY AIR | |
| CN106169264A (en) | Aircraft carrier launches and blocks simulated training system | |
| CN206218248U (en) | Electromechanical integration dynamic energy storage type carrier-based aircraft ejector system | |
| CN105501458B (en) | Rail sliding car chain carrier-based aircraft ejector | |
| CN204507292U (en) | A kind of Electromagnetical ejector | |
| CN202669848U (en) | Power generating and braking device utilizing translational kinetic energy of train | |
| CN106314816B (en) | The design application method of electromechanical integration dynamic energy storage type carrier-based aircraft ejector system | |
| US20230339520A1 (en) | An aerial electromagnetic flying vehicle | |
| CN206068190U (en) | Multipurpose dynamic energy storage type carrier-based aircraft ejector system | |
| CN211169678U (en) | Quick lifting mechanical device of lifting goods elevator | |
| CN204642101U (en) | A kind of track moves ship dolly | |
| CN103935368A (en) | Railroad platform specially used for conveying cars quickly | |
| CN109774483A (en) | Pantograph synchronous rolling contact device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170201 |