CN205952336U - Aircraft carrier launches shuttle runway - Google Patents
Aircraft carrier launches shuttle runway Download PDFInfo
- Publication number
- CN205952336U CN205952336U CN201620921928.8U CN201620921928U CN205952336U CN 205952336 U CN205952336 U CN 205952336U CN 201620921928 U CN201620921928 U CN 201620921928U CN 205952336 U CN205952336 U CN 205952336U
- Authority
- CN
- China
- Prior art keywords
- runway
- shuttle
- carrier
- ditch
- 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.)
- Expired - Fee Related
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Abstract
The utility model provides an aircraft carrier launches shuttle runway, its structure is by the runway ditch, bearing roller group, the runway cover plate, pull the medium connecting plate, the I shape slider, it links the piece and draws medium composition to draw the pike pole, the bearing setting is passed through among the runway ditch in the both ends of bearing roller group, the bearing roller of bearing roller group with pull medium roll connection, pull in the middle of the medium through the bolt with to pull the medium connecting plate fixed, it is connected to pull the I shape slider of medium connecting plate bottom the shuttle, the bottom of two sets of runway cover plates is connected with the runway ditch is suitable for reading, the recess sliding connection of edge and I shape slider both sides in the middle of two sets of runway cover plates, the top of I shape slider sets up the carrier -borne aircraft and draws even piece of pike pole, should launch the shuttle runway and have simple structure, easily processing, easily installation facilitate the use, shuttle light in weight, and frictional resistance is little, and power consumption is little, has fine environmental protection and energy saving effect.
Description
Technical field
The utility model is related to carrier-based aircraft ejector processing technique field, and specifically a kind of aircraft carrier ejection is slided
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 the U.S. at present
Ejector and Electromagnetical ejector.
Content of the invention
The purpose of this utility model is to provide a kind of simple in structure and low in cost, can be in nuclear aircraft carrier or powered by conventional energy
The aircraft carrier ejection shuttle runway of the towed ejector of synchronous bidirectional using on aircraft carrier.
The purpose of this utility model is realized in the following manner, aircraft carrier launch shuttle runway, its structure be by
Runway ditch, idler machining, runway trench cover, traction medium connecting plate, I shape slide block, traction pike pole connect part and traction medium group
Become, the two ends of idler machining are arranged among runway ditch by bearing, the carrying roller of idler machining is rolled with traction medium and is connected, and traction is situated between
Fixed with traction medium connecting plate by bolt in the middle of matter, 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 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 be slidably connected, 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, runway trench cover
Together with bottom is bolted on flange, two sides of runway trench cover 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.
The beneficial effects of the utility model are：Structure is simple, takes up room little, and convenient processing is installed, and can substantially reduce warship
The cost of carrier aircraft ejector, is slidably connected with runway trench cover using I shape slide block, can effectively reduce shuttle weight, subtract
Few resistance, reduces brake inertia, effectively improves service life, and conventional vapor ejector becomes station with the ejection runway of Electromagnetical ejector
The 80% of a whole set 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% make
Valency is power-equipment, and power-equipment is common apparatus again, is thus advantageous to popularizing of synchronous mode carrier-based aircraft ejector, is not
Carry out the essential equipment of Chinese 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.
Aircraft carrier of the present utility model launches shuttle runway, including runway ditch 1, idler machining 2, runway trench cover 3, leads
Introducing 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 by bearing
Among runway ditch 1, the carrying roller of idler machining 2 is rolled with traction medium 4 and is connected, by bolt and traction medium in the middle of traction medium 4
Connecting plate 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
Runway 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-shaped
The top of type 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, runway trench cover 3
Bottom be bolted on flange together with, two sides of runway trench cover 3 and type aircraft carrier deck are fixed together composition bullet
Penetrate runway.
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 leads to
Cross shuttle connecting plate to be connected with traction medium, the two ends of traction medium connect respectively at ejection module and playback module, launch mould
Block and playback module take off for carrier-borne aircraft and provide hauling speed and power to respectively the positive hauling speed of shuttle and tractive force, carrier-borne
After machine takes off, playback module provides reversely traction to make shuttle return to carrier-borne aircraft takeoff setting, the carrying roller in runway ditch for shuttle again
Group provides to lift for traction medium and slides to reduce the frictional resistance of traction medium and runway ditch.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, although ginseng
According to previous embodiment, the utility model is described in detail, for a person skilled in the art, it is still permissible
Technical scheme described in foregoing embodiments is modified, or equivalent is carried out to wherein some technical characteristics.All
Any modification, equivalent or improvement made within spirit of the present utility model and principle etc., should be included in this practicality
Within new protection domain.
It is the known technology of those skilled in the art in addition to technical characteristic disclosed in specification of the present utility model.
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 rolled with traction medium and is connected, and is fixed with traction medium connecting plate by bolt, lead in the middle of traction medium
Introducing matter connecting plate is connected with the I shape slide block of shuttle bottom, the bottom of two groups of runway trench covers and the connection suitable for reading of runway ditch,
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 setting warship of I shape slide block
Carrier aircraft traction pike pole connects 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 tractive force, 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 |
|---|---|---|---|
| CN201620921928.8U CN205952336U (en) | 2016-08-23 | 2016-08-23 | Aircraft carrier launches shuttle runway |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620921928.8U CN205952336U (en) | 2016-08-23 | 2016-08-23 | Aircraft carrier launches shuttle runway |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205952336U true CN205952336U (en) | 2017-02-15 |
Family
ID=57976806
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620921928.8U Expired - Fee Related CN205952336U (en) | 2016-08-23 | 2016-08-23 | Aircraft carrier launches shuttle runway |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205952336U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106364691A (en) * | 2016-08-23 | 2017-02-01 | 济南环太机电技术有限公司 | Catapult gliding shuttle runway of shipboard aircraft on carrier |
-
2016
- 2016-08-23 CN CN201620921928.8U patent/CN205952336U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106364691A (en) * | 2016-08-23 | 2017-02-01 | 济南环太机电技术有限公司 | Catapult gliding shuttle runway of shipboard aircraft on carrier |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170215 Termination date: 20170823 |