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 |