Manteiga J.A., Nussbaum J.H., Noon J.L. Gas turbine or jet engine stator vane frame. Patent US No. 6343912 B1. General Electric Company, 2002.US6343912 1999年12月7日 2002年2月5日 General Electric Company Gas turbine or jet engine stator vane frame...
FIELD: engine technology. ;SUBSTANCE: invention relates to turbine construction. A rotary gas turbine engine contains a body with annular shells. There are... RU KOMINOV 被引量: 0发表: 2022年 STARTING EQUIPMENT OF GAS TURBINE ENGINE shaft side or of a starting device and by judging ignition...
4) turbojet engine 涡轮喷气发动机 1. The improved and modification designs were conducted for a turbojet engine. 对某型涡轮喷气发动机进行了改进、改型设计。 更多例句>> 5) gas turbine engine 燃气涡轮发动机 1. The development history of aviation engine oil is briefly described , and the ...
Some is fed to the engine (3), which drives a second compressor (4), before exiting through the rear nozzle (5). The rear compressor's exhaust drives the compressor at the front (6). Artwork: Gas turbine engine designed by Frank Whittle in 1937 and formally patented two years later. ...
摘要: PURPOSE: To improve an engine speed more speedy than that of a prior art by reducing centrifugal force which is acted on a gas flow part.收藏 引用 批量引用 报错 分享 文库来源 求助全文 JET PROPULSION ENGINE OR OUTPUT PART STRUCTURE FOR 优质文献 ...
ainterest him 感兴趣他 [translate] avalue respectively is 价值分别为 [translate] ain our hybrid,we use flywheel and a gas-turbine engine that is akin to a miniature jet engine 在我们的杂种,我们使用飞轮和是如同到微型喷气机引擎的一个燃气轮机引擎 [translate] ...
In a gas turbine jet propulsion plant containing a compressor, combustion apparatus and a turbine, having a main conduit, a by-pass duct branching from the main conduit on the upstream side of the combustion chambers so as to by-pass the combustion chamber and the turbine, the by-pass duct...
百度试题 题目which type of gas turbine engine provides very limited of jet thrust ?相关知识点: 试题来源: 解析 turboprop engine 反馈 收藏
(VBV). * High pressure turbine active clearance control (HPTACC). * Low pressure turbine active clearance control (LPTACC). Major components covered. * Electronic engine control, N1 speed sensor, N2 speed sensor, exhaust gas temperature (EGT) sensors, engine temperature probes and pressure ports....
Turbofan engines, commonly used to power aircraft, are a type of air-breathing jet engine that includes a fan and a core (turbine) engine that both ... TB Company 被引量: 0发表: 2017年 Reinforcement of the turbine case in a gas turbine jet engine In one embodiment, 302 are formed not...