CN204606231U - A kind of aircraft carrier hydrodynamic force catapult-launching gear - Google Patents
A kind of aircraft carrier hydrodynamic force catapult-launching gear Download PDFInfo
- Publication number
- CN204606231U CN204606231U CN201520196811.3U CN201520196811U CN204606231U CN 204606231 U CN204606231 U CN 204606231U CN 201520196811 U CN201520196811 U CN 201520196811U CN 204606231 U CN204606231 U CN 204606231U
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- water tank
- pressure water
- pressure
- cylinder
- draw bar
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Abstract
The utility model relates to a kind of aircraft carrier hydrodynamic force catapult-launching gear, comprise high-pressure water tank, supercharger, heating wire, wire, power supply, source switch, high-pressure conduit, valve, shower nozzle, inlet point, slag-drip opening, cylinder, piston, draw bar, seal ring, it is characterized in that: the top of high-pressure water tank is provided with inlet point, water in high-pressure water tank is added by inlet point, the bottom of high-pressure water tank is provided with slag-drip opening, water unnecessary in high-pressure water tank is released by slag-drip opening, shower nozzle is connected with one end of cylinder, piston is provided with in cylinder, piston is connected with one end of draw bar, the surrounding of draw bar is provided with seal ring, draw bar from cylinder motion after, seal ring resets.The utility model volume is little, structure simple, and reliability is high, is conducive to the comprehensive fight capability improving aircraft carrier.
Description
Technical field
The utility model relates to a kind of ejector, and specifically a kind of aircraft carrier hydrodynamic force catapult-launching gear, belongs to aircraft carrier catapult-launching gear technical field.
Background technology
Aircraft carrier; be called for short " aircraft carrier "; the large-scale water surface naval vessels of to be a kind of with carrier-borne aircraft be main operational weapon; warship body usually has huge deck and is seated the warship island on right side; aircraft carrier is the core naval vessel of an aircraft carrier group; other ship in fleet provides its protection and supply, and aircraft carrier then provides air umbrella and long-range strike ability.Be developed so far, aircraft carrier has been the indispensable weapon of Modern Navy, also be one of most important naval vessels in sea warfare, rely on aircraft carrier, a country can in the place away from its territory, and not rely on local airport situation apply military pressure and fight, even to this day, aircraft carrier has been the indispensable sharp weapon of Modern Navy, becomes the symbol of a national overall national strength.
As everyone knows, the mode of taking off of the carrier-borne aircraft on aircraft carrier has three kinds: take off vertically, ski-jump take-off and catapult-assisted take-off, catapult-assisted take-off is a kind of mode of taking off that can improve carrier-borne aircraft fight capability, some developed country adopts the aircraft carrier of catapult-assisted take-off mode mostly to adopt steam catapult in the world at present, and Electromagnetical ejector is not full-fledged yet, in order to break the technical monopoly of western developed country, strengthen the military capability of the country of China, therefore, in the urgent need to inventing a kind of novel aircraft carrier ejector.
Summary of the invention
The technical problems to be solved in the utility model is: provide that a kind of volume is little, structure is simple, and the aircraft carrier hydrodynamic force catapult-launching gear that reliability is high.
In order to solve the problems of the technologies described above, the technical solution adopted in the utility model is: a kind of aircraft carrier hydrodynamic force catapult-launching gear, comprises high-pressure water tank, supercharger, heating wire, wire, power supply, source switch, high-pressure conduit, valve, shower nozzle, inlet point, slag-drip opening, cylinder, piston, draw bar, seal ring, it is characterized in that: described high-pressure water tank is built with water, high-pressure water tank is connected with supercharger, heating wire is provided with in high-pressure water tank, heating wire is connected with wire, wire is connected with power supply, wire is provided with source switch, and high-pressure water tank is connected with valve by high-pressure conduit, and valve is connected with shower nozzle by high-pressure conduit, the top of high-pressure water tank is provided with inlet point, water in high-pressure water tank is added by inlet point, and the bottom of high-pressure water tank is provided with slag-drip opening, and water unnecessary in high-pressure water tank is released by slag-drip opening, shower nozzle is connected with one end of cylinder, be provided with piston in cylinder, piston is connected with one end of draw bar, and the surrounding of draw bar is provided with seal ring, draw bar from cylinder motion after, seal ring reset.
The length of described cylinder is greater than the length of described piston.
Described seal ring adopts marmem manufacture, and draw bar is after washing seal ring open, and seal ring automatically resets, and prevents pressure from leaking.
Described draw bar is connected with undercarriage, and piston driving draw bar moves, thus drives carrier-borne aircraft to take off.
The diameter of described slag-drip opening is greater than the diameter of described inlet point.
Described valve is check valve, and object prevents aqueous reflux.
Described source switch is that switch put by hilted broadsword pair, and when supercharger is started working, heating wire quits work, and when supercharger quits work, heating wire is started working.
Described high-pressure water tank adopts insulated heat and high pressure resistant material is made, and object keeps the temperature of high-pressure water tank inside and prevents electric leakage.
Described supercharger provides pressure to high-pressure water tank, when supercharger no longer increases to the pressure that high-pressure water tank provides, heating wire is started working, and heating wire produces amount of heat makes the temperature of water raise, pressure increases, thus reaches the effect of the pressure increased in high-pressure water tank.
Compared with prior art, the utility model has following beneficial effect: volume is little, structure is simple, and reliability is high, is conducive to the comprehensive fight capability improving aircraft carrier.
Accompanying drawing explanation
Accompanying drawing is structural representation of the present utility model.
In figure: 1-high-pressure water tank, 2-supercharger, 3-heating wire, 4-wire, 5-power supply, 6-source switch, 7-high-pressure conduit, 8-valve, 9-shower nozzle, 10-inlet point, 11-slag-drip opening, 12-cylinder, 13-piston, 14-draw bar, 15-seal ring.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
As shown in drawings, a kind of aircraft carrier hydrodynamic force catapult-launching gear, comprises high-pressure water tank 1, supercharger 2, heating wire 3, wire 4, power supply 5, source switch 6, high-pressure conduit 7, valve 8, shower nozzle 9, inlet point 10, slag-drip opening 11, cylinder 12, piston 13, draw bar 14, seal ring 15, it is characterized in that: described high-pressure water tank 1 is built with water, high-pressure water tank 1 is connected with supercharger 2, heating wire 3 is provided with in high-pressure water tank 1, heating wire 3 is connected with wire 4, wire 4 is connected with power supply 5, wire 4 is provided with source switch 6, and high-pressure water tank 1 is connected with valve 8 by high-pressure conduit 7, and valve 8 is connected with shower nozzle 9 by high-pressure conduit 7, the top of high-pressure water tank 1 is provided with inlet point 10, water in high-pressure water tank 1 is added by inlet point 10, and the bottom of high-pressure water tank 1 is provided with slag-drip opening 11, and water unnecessary in high-pressure water tank 1 is released by slag-drip opening 11, shower nozzle 9 is connected with one end of cylinder 12, be provided with piston 13 in cylinder 12, piston 13 is connected with one end of draw bar 14, and the surrounding of draw bar 14 is provided with seal ring 15, draw bar 14 from cylinder 12 move after, seal ring 15 resets.
The length of described cylinder 12 is greater than the length of described piston 13.
Described seal ring 15 adopts marmem manufacture, and draw bar 14 is after washing seal ring 15 open, and seal ring 15 automatically resets, and prevents pressure from leaking.
Described draw bar 14 is connected with undercarriage, and piston 13 drives draw bar 14 to move, thus drives carrier-borne aircraft to take off.
The diameter of described slag-drip opening 11 is greater than the diameter of described inlet point 10.
Described valve 8 is check valve, and object prevents aqueous reflux.
Described source switch 6 puts switch for hilted broadsword is two, and when supercharger 2 is started working, heating wire 3 quits work, and when supercharger 2 quits work, heating wire 3 is started working.
Described high-pressure water tank 1 adopts insulated heat and high pressure resistant material is made, and object keeps the temperature of high-pressure water tank 1 inside and prevents electric leakage.
Described supercharger 2 provides pressure to high-pressure water tank 1, when the pressure that supercharger 2 provides to high-pressure water tank 1 no longer increases, heating wire 3 is started working, and heating wire 3 produces amount of heat makes the temperature of water raise, pressure increases, thus reaches the effect of the pressure increased in high-pressure water tank 1.
When equipment works, supercharger 2 provides pressure to high-pressure water tank 1, now heating wire 3 does not work, when the pressure that supercharger 2 provides to high-pressure water tank 1 no longer increases, heating wire 3 is started working, heating wire 3 produces amount of heat makes the temperature of water raise, and pressure increases, thus reaches the effect of the pressure increased in high-pressure water tank 1.
When needs launch carrier-borne aircraft, High-Pressure Water is discharged in cylinder 12 by high-pressure water tank 1, and High-Pressure Water promotes piston 13 and draw bar 14 moves, thus drives carrier-borne aircraft to take off.
The above is preferred implementation of the present utility model; it should be pointed out that for those skilled in the art, under the prerequisite not departing from the utility model principle; can also make some improvements and modifications, these improvements and modifications are also considered as protection domain of the present utility model.
Claims (2)
1. an aircraft carrier hydrodynamic force catapult-launching gear, comprise high-pressure water tank (1), supercharger (2), heating wire (3), wire (4), power supply (5), source switch (6), high-pressure conduit (7), valve (8), shower nozzle (9), inlet point (10), slag-drip opening (11), cylinder (12), piston (13), draw bar (14), seal ring (15), it is characterized in that: described high-pressure water tank (1) is built with water, high-pressure water tank (1) is connected with supercharger (2), heating wire (3) is provided with in high-pressure water tank (1), heating wire (3) is connected with wire (4), wire (4) is connected with power supply (5), wire (4) is provided with source switch (6), high-pressure water tank (1) is connected with valve (8) by high-pressure conduit (7), valve (8) is connected with shower nozzle (9) by high-pressure conduit (7), the top of high-pressure water tank (1) is provided with inlet point (10), water in high-pressure water tank (1) is added by inlet point (10), the bottom of high-pressure water tank (1) is provided with slag-drip opening (11), water unnecessary in high-pressure water tank (1) is released by slag-drip opening (11), shower nozzle (9) is connected with one end of cylinder (12), piston (13) is provided with in cylinder (12), piston (13) is connected with one end of draw bar (14), the surrounding of draw bar (14) is provided with seal ring (15), draw bar (14) from cylinder (12) motion after, seal ring (15) resets.
2. a kind of aircraft carrier hydrodynamic force catapult-launching gear according to claim 1, is characterized in that: the length of described cylinder (12) is greater than the length of described piston (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520196811.3U CN204606231U (en) | 2015-03-25 | 2015-03-25 | A kind of aircraft carrier hydrodynamic force catapult-launching gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520196811.3U CN204606231U (en) | 2015-03-25 | 2015-03-25 | A kind of aircraft carrier hydrodynamic force catapult-launching gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204606231U true CN204606231U (en) | 2015-09-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520196811.3U Expired - Fee Related CN204606231U (en) | 2015-03-25 | 2015-03-25 | A kind of aircraft carrier hydrodynamic force catapult-launching gear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204606231U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108128478A (en) * | 2017-11-27 | 2018-06-08 | 北京特种机械研究所 | A kind of accumulator tank for hydrodynamic force ejection |
| CN108657459A (en) * | 2018-05-07 | 2018-10-16 | 北京特种机械研究所 | A kind of hydrodynamic force catapult-launching gear of ship-board aircraft |
-
2015
- 2015-03-25 CN CN201520196811.3U patent/CN204606231U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108128478A (en) * | 2017-11-27 | 2018-06-08 | 北京特种机械研究所 | A kind of accumulator tank for hydrodynamic force ejection |
| CN108657459A (en) * | 2018-05-07 | 2018-10-16 | 北京特种机械研究所 | A kind of hydrodynamic force catapult-launching gear of ship-board aircraft |
| CN108657459B (en) * | 2018-05-07 | 2019-09-10 | 北京特种机械研究所 | A kind of hydrodynamic force catapult-launching gear of ship-board aircraft |
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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: 20150902 Termination date: 20160325 |