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Gas turbine engine

A gas turbine and engine technology, which is applied to gas turbine devices, engine components, machines/engines, etc., can solve the problems of difficult starting, slow starting speed, and low energy utilization rate, and achieves convenient operation, saving installation space, and simple structure. Effect

Inactive Publication Date: 2018-12-07
浦江县速达进出口有限公司
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Problems solved by technology

[0002] With the development of science and the progress of society, the country has been promoting the development of science and technology. The demand for automobiles in today's life has increased sharply, and the technical requirements for engines have also increased greatly. Among them, gas turbine engines are the most demanded engines today. One, the general gas turbine engine has disadvantages such as mismatched air-fuel ratio, limited power, low energy utilization rate, and difficulty in starting, which lead to difficulty in starting in winter, high fuel consumption, and slow start-up speed. The device of this invention solves this problem

Method used

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Embodiment Construction

[0015] Such as figure 1 and figure 2As shown, a gas turbine engine of the present invention includes a fuselage 100 and a gas chamber 154 arranged in the fuselage 100, the left end of the gas chamber 154 is provided with a discharge chamber 126, and the right end of the gas chamber 126 is provided with The first cavity 119, the right end of the first cavity 119 communicates with the second cavity 113, and the left end of the first cavity 119 is sequentially provided with a third cavity at the bottom of the gas cavity 154 from right to left 106 and the fourth cavity 104, the gas chamber 154 and the discharge chamber 126 are provided with a vertically symmetrical elastic steel ball intake mechanism, and the inner wall of the left end of the gas chamber 154 is provided with an elastic steel ball intake mechanism The compression tube 133 at the right end and communicated with it, the intake compression tube 136 is connected with sliding fit in the compression tube 133, the top p...

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Abstract

The invention discloses a gas turbine engine. The gas turbine engine comprises an engine body and a gas cavity which is formed in the engine body; a discharge cavity is formed in the left end of the gas cavity; a first cavity is formed in the right end of the gas cavity; a second cavity is formed in the right end of the first cavity in a communicating manner; a third cavity and a fourth cavity which are positioned in the bottom of the gas cavity are formed in the left end of the first cavity from right to left in sequence; elastic steel ball gas inlet mechanisms which are in longitudinal symmetry are arranged between the gas cavity and the discharge cavity; and a compressing pipe which is positioned at the right end of each elastic steel ball gas inlet mechanism and communicates with the elastic steel ball gas inlet mechanism is arranged on the inner wall of the left end of the gas cavity. The gas turbine engine is simple in structure, low in gas loss, high in energy utilization rate,convenient to start, and full of power.

Description

technical field [0001] The invention relates to the technical field of engines, in particular to a gas turbine engine. Background technique [0002] With the development of science and the progress of society, the country has been promoting the development of science and technology. The demand for automobiles in today's life has increased sharply, and the technical requirements for engines have also increased greatly. Among them, gas turbine engines are the most demanded engines today. One, the general gas turbine engine has disadvantages such as mismatched air-fuel ratio, limited power, low energy utilization rate, and difficulty in starting, which lead to difficulty in starting in winter, high fuel consumption, and slow start-up speed. The device of this invention solves this problem . Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a gas turbine engine, which can solve the above-mentioned problems in the prio...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C3/14F02C3/22F02C7/04F02C7/22F02C7/232F02C7/275
CPCF02C3/14F02C3/22F02C7/04F02C7/22F02C7/232F02C7/275
Inventor 俞李娜
Owner 浦江县速达进出口有限公司
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