Helicopter turbine engine protection system
作者： Leonard M. Greene
DOI:
关键词: Start up 、 Marine engineering 、 Engine coolant temperature sensor 、 Protection system 、 Automotive engineering 、 Turbine 、 Engineering
摘要: A helicopter having a turbine engine disposed therein includes an over-stress protection system. The system computer for storing data and input such as keyboard inputting safe temperature profile starting the engine. sensor is provided measuring actual outlet during start up of then compared with water and/or alcohol injected into when exceeds temperature. use ground based tank airborne in flight are also disclosed.
lens.org 参考文章(13)
M. Samuel Moore, Helicopter engine warning or control system ,(1985)
Hajime Toriya, Isao Takehara, Haruo Urushidani, Tetsuo Sasada, Method of starting gas turbine ,(1989)
F. Jay Eichelberger, Robert E. Miller, Low profile cart for the insitu collection filteration and recycle of fluids from machinery ,(1990)
Jon A. Jensen, Coolant recycling system ,(2001)
Yoshinori Hirano, Takao Kubozuka, Yoshimasa Hayashi, Cooling system for automotive engine ,(1985)
John Matthews, Frederick Boyle, John Martin, Albert Ruff, Gary Gerber, L. Silzle, System for periodic fluid maintenance of apparatus ,(2001)
Raymond C. LeBlanc, J. Allen Oliver, David W. Smith, Aircraft flight line servicing system ,(1976)
Frank C Mock, Water injection system for gas turbine engines ,(1957)