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Rotary cylinder type fuel gas ejector

A technology of rotating cylinders and catapults, applied in the direction of launch/drag transmission devices, etc., can solve the problems of large space occupation, impracticality, large power consumption, etc., and achieve the effects of long service life, simple structure, and small space occupation.

Inactive Publication Date: 2016-07-06
银世德
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Some of the authorized gas catapults and explosive catapults are semi-open, and some are equipped with push rods and traction ropes, which take up a lot of space, are not well sealed, and are very impractical. Now a few countries are researching and testing electromagnetic catapults. The catapult uses a lot of power and is very technical
Therefore, it is inconvenient to use in our country

Method used

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  • Rotary cylinder type fuel gas ejector
  • Rotary cylinder type fuel gas ejector
  • Rotary cylinder type fuel gas ejector

Examples

Experimental program
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Effect test

Embodiment Construction

[0027] According to attached figure 1 As shown, first open an opening with a width of about 30 mm from one end of the tubular outer cylinder (10) to the other end. When the piston is about to reach the top dead center, the corresponding tubular outer cylinder (10) at the position of the rear end of the piston On one side, open a front exhaust port (11), then fix the tubular outer cylinder (10) below the flight deck (14), the tubular outer cylinder opening (1) is aligned with the traction groove of the flight deck (14), The front exhaust port (11) is connected to the outside of the ship with a pipeline. On the tubular inner cylinder (12), open one with the tubular outer cylinder opening (1), the oblique opening (3) of the tubular inner cylinder equal in length and width. On both sides of the inclined opening (3) of the tubular inner cylinder, a rectangular groove (15) identical with the length and width of the inclined opening is respectively set, (referring to figure 2 ). ...

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Abstract

The invention provides a rotary cylinder type gas catapult, which is characterized in that: a tubular inner cylinder with an oblique opening is placed in a fully open tubular outer cylinder, and a tractor is installed on the upper part of the piston. The tractor moves the cylinder with oblique opening to rotate less than 350°, and closes the opening of the tubular outer cylinder. The advantages of the present invention are: simple structure, no preparatory work for use, long service life, less space occupation, and can also be used For steam ejection, the present invention includes: tubular outer cylinder opening part (1), return spring (2), tubular inner cylinder chute (3), tractor (4), aircraft (5), piston (6) , combustion chamber (7), inlet (8), rear exhaust port (9), tubular outer cylinder (10), front exhaust port (11), tubular inner cylinder (12), buffer spring (13), Flight deck (14), rectangular groove (15), wave type leaf spring (16), rectangular aluminum alloy sealing strip (17), roller (18), oblique opening plug of tubular inner cylinder (19), piston ring (20).

Description

technical field [0001] The invention provides an aircraft carrier catapult, in particular a rotary cylinder type gas catapult, which is a booster device for an aircraft carrier-borne aircraft to take off, and belongs to the field of weapons and equipment. Background technique [0002] At present, most countries with aircraft carriers in the world generally use steam catapults. The cylinders of these catapults are all open, and sealing strips are used to seal the openings of the cylinders. This technology is complicated to use and the parts are easily damaged. Its largest The disadvantage is that there is always sufficient steam, which is very inconvenient to use and delays the ejection time of the aircraft, and the current modern wars are generally local wars under high-tech conditions. The restrictions of time and space "forbidden areas" have been greatly reduced, and combat operations have become more sudden. Some of the authorized gas catapults and explosive catapults ar...

Claims

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Application Information

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IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 银世德
Owner 银世德
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