发明名称 Geared architecture for high speed and small volume fan drive turbine
摘要 A gas turbine engine includes a flex mount for a fan drive gear system. A very high speed fan drive turbine drives the fan drive gear system.
申请公布号 US8899915(B2) 申请公布日期 2014.12.02
申请号 US201414260557 申请日期 2014.04.24
申请人 United Technologies Corporation 发明人 McCune Michael E.;Husband Jason;Schwarz Frederick M.;Kupratis Daniel Bernard;Suciu Gabriel L.;Ackermann William K.
分类号 F01D15/12;F02C7/36;F02C7/20;F02K3/06;F02C3/107 主分类号 F01D15/12
代理机构 Carlson, Gaskey & Olds, PC 代理人 Carlson, Gaskey & Olds, PC
主权项 1. A gas turbine engine comprising: a fan shaft driving a fan; a frame which supports said fan shaft; a plurality of gears to drive said fan shaft; a flexible support which at least partially supports said plurality of gears, said flexible support having a different stiffness than said frame; a first turbine section providing a drive input into said plurality of gears; and a second turbine section, wherein said first turbine section has a first exit area at a first exit point and rotates at a first speed, wherein said second turbine section has a second exit area at a second exit point and rotates at a second speed, which is faster than the first speed, wherein a first performance quantity is defined as the product of the first speed squared and the first area, wherein a second performance quantity is defined as the product of the second speed squared and the second area, and wherein a ratio of the first performance quantity to the second performance quantity is between about 0.5 and about 1.5.
地址 Hartford CT US