Intelligent gas turbine engine
A gas turbine and engine technology, which is applied in the direction of engine components, turbine/propulsion fuel delivery system, fuel control of turbine/propulsion device, etc., can solve the problems of difficult start, slow start speed, low energy utilization rate, etc., and achieve easy operation , Save installation space and simple structure
Inactive Publication Date: 2018-11-30
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
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[0016] Such as figure 1 and figure 2As shown, an intelligent 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 intak...
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The invention discloses an intelligent gas turbine engine. The intelligent gas turbine engine comprises an engine body and a gas chamber disposed in the engine body. The left end of the gas chamber isprovided 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 cavity is 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 intelligent gas turbine engine has a simple structure, has a low gas loss and a high energy use rate, is easy to start and hasenough powder.
Description
technical field [0001] The invention relates to the technical field of engines, in particular to an intelligent 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 intelligent gas turbine engine, which can solve the above-ment...
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IPC IPC(8): F02C7/22F02C9/48
CPCF02C7/22F02C9/48
Inventor 俞李娜
Owner 浦江县速达进出口有限公司