公开(公告)号：US09932124B2

公开(公告)日：2018-04-03

申请号：US14654925

申请日：2013-11-26

Applicant: General Electric Company

Inventor： Deepak Manohar Kamath ,  Todd James Buchholz ,  Mehdi Milani Baladi ,  Michael Jay Epstein

IPC: B64D37/30 ,  F02C7/236 ,  F02C3/22 ,  F02C6/08 ,  F02C7/224 ,  F02C9/40

CPC classification number: B64D37/30 ,  F02C3/22 ,  F02C6/08 ,  F02C7/224 ,  F02C7/236 ,  F02C9/40 ,  Y02T50/672

Abstract: A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fuel at high pressure through the supply line where the pump is operably coupled to the compressor such that operation of the turbine engine drives the pump and a method for delivering fuel in a fuel system to a turbine engine.

公开(公告)号：US20160333794A1

公开(公告)日：2016-11-17

申请号：US14709343

申请日：2015-05-11

Applicant: General Electric Company

Inventor： Mehdi Milani Baladi ,  Edward Michael Yanosik, JR. ,  Richard Bradford Hook, JR. ,  Scott Edward Farley ,  Gordon Jeffery Follin

IPC: F02C9/18 ,  F02C3/04

CPC classification number: F02C9/18 ,  F01D5/145 ,  F01D5/148 ,  F01D17/14 ,  F02C3/04 ,  F02C9/20 ,  F02K1/30 ,  F05D2220/32 ,  F05D2260/16 ,  F05D2260/202 ,  F15D1/008 ,  F15D1/025 ,  Y02T50/673 ,  Y02T50/675

Abstract: One embodiment of the present discloses includes a system. The system includes a turbine and a fluid supply system. The turbine includes a main flow path, a plurality of turbine blades disposed along the main flow path, at least one flow control area disposed along the main flow path, and at least one fluid injection port fluidly coupled to the main flow path. The fluid supply system is fluidly coupled to the at least one fluid injection port, wherein the fluid supply system is configured to supply a fluid to the at least one fluid injection port to adjust an effective area of the at least one flow control area.

Abstract translation: 本公开的一个实施例包括一个系统。 该系统包括涡轮机和流体供应系统。 涡轮机包括主流路，沿着主流路设置的多个涡轮机叶片，沿着主流路设置的至少一个流动控制区域以及流体连接到主流路的至少一个流体注入口。 流体供应系统流体地联接到至少一个流体注入端口，其中流体供应系统被配置为将流体供应到至少一个流体注入端口以调节至少一个流动控制区域的有效面积。