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Automatic 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 slow startup speed, difficult startup, low energy utilization rate, etc., and achieves saving installation space, convenient operation and simple structure. Effect

Inactive Publication Date: 2018-11-30
浦江县速达进出口有限公司
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

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

[0016] Such as figure 1 and figure 2As shown, an automatic 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 There is a 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 chamber 154 from right to left. cavity 106 and the fourth cavity 104, the gas cavity 154 and the discharge cavity 126 are provided with a vertically symmetrical elastic steel ball intake mechanism, and the inner wall of the left end of the gas cavity 154 is provided with the elastic steel ball intake mechanism. The compression tube 133 at the right end of the mechanism and connected thereto. The compression tube 133 is slidingly fitted with an intake ...

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Abstract

The invention discloses an automatic gas turbine engine. The automatic gas turbine engine comprises an engine body and a gas chamber disposed in the engine body. The left end of the gas chamber is provided with a burning chamber. The right end of the gas chamber is provided with a first cavity. The right end of the first cavity is communicated with a second cavity. The left end of the first cavityis orderly provided with a third cavity and a forth cavity at the bottom of the gas chamber from left to right. Elastic steel ball air intake mechanisms symmetrical vertically are arranged between the gas chamber and the burning chamber. The inner wall of the left end of the gas chamber is provided with compression tubes located at the right ends of the elastic steel ball air intake mechanisms and communicated with the elastic steel ball air intake mechanisms. The automatic gas turbine engine has a simple structure, has a low gas loss and a high energy use rate, is easy to start and has enough powder.

Description

technical field [0001] The invention relates to the technical field of engines, in particular to an automatic 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 an automatic gas turbine engine, which can solve the above-mentione...

Claims

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Application Information

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IPC IPC(8): F02C3/14F02C7/22F02C7/057F02C7/275
CPCF02C3/14F02C7/057F02C7/22F02C7/275
Inventor 俞李娜
Owner 浦江县速达进出口有限公司
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