Abstract:
A gas turbine engine (20, 80) has a compressor section (24) including a lower pressure compressor (44, 94) and a higher pressure compressor (52, 100), and a turbine section (28). A core engine housing (90) surrounds the compressor section (24) and the turbine section (28). An outer intermediate housing wall defines an internal chamber (88) between the core housing (90) and the outer intermediate housing (86). A fan rotor (42, 84) and a fan casing (82) surround the fan rotor (42, 84) to define a bypass duct (B) between the fan case (82) and the outer intermediate housing (86). A heat exchanger (108) is mounted in the internal chamber (88) and receives high pressure air for cooling the high pressure air and delivering the high pressure air into the core engine housing (90) to be utilized as cooling air for a component. Air from the lower pressure compressor (44, 94) is utilized to cool the higher pressure air in the heat exchanger (108).
Abstract:
본 발명은 Co 약 10 내지 약 15중량%, Cr 약 18 내지 약 22중량%, Al 약 0.5 내지 약 1.3중량%, Ta 약 3.5 내지 약 4.5중량%, Mo 약 1 내지 약 2중량%, W 약 13.5 내지 약 17.0중량%, C 약 0.08중량% 이하, Zr 약 0.06중량% 이하, B 약 0.015중량% 이하, Mn 약 0.4 내지 약 1.2중량%, Si 약 0.1 내지 약 0.3중량% 및 잔여량의 Ni를 포함하는 고용체 강화 초합금 용접 조성물에 관한 것이다.
Abstract:
A fluid impeller for us in applications requiring superior cavitation erosion resistance. The impeller has a body fabricated from a castable metastable austenitic steel alloy which has a preferred chemical composition in the range of 17.5-18.5% chromium, 0.5-0.75% nickel, 0.45-55% silicon, 0.2-0.25% nitrogen, 15.5-16.0% manganese and 0.1%-0.12% carbon. Quantitative testing has shown cavitation resistance of four to six times that of standard boiler feed pump materials. A method for making cavitation resistant fluid impellers is also disclosed.
Abstract:
A dry vacuum pump comprises a stator component and at least one rotor component. To improve the tolerance of the pump to corrosive gases passing through the pump, the stator component and/or said at least one rotor component are formed from silicon-molybdenum (SiMo) ductile iron.
Abstract:
At least one of a cylinder (6), a rotor (8), a front plate (14), and a rear plate (16), all of which form compression chambers (18), is made of a metal, and a surface treatment is conducted on a portion of such at least one of those members.