发明名称 COMBUSTOR SEAL MISTAKE-PROOFING FOR A GAS TURBINE ENGINE
摘要 A combustor seal for use between a downstream end of a combustor and a turbine vane includes a seal body and a plurality of seal alignment features. The plurality of seal alignment features projects from the seal body. The seal alignment features are arranged such that there is only one alignment of the combustor seal with the turbine vane.
申请公布号 US2015240724(A1) 申请公布日期 2015.08.27
申请号 US201314432339 申请日期 2013.10.01
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Low Kevin Joseph;Wong Joey
分类号 F02C7/28;F01D11/00;F02C3/04 主分类号 F02C7/28
代理机构 代理人
主权项 1. A combustor seal for use between a downstream end of a combustor and a turbine vane, the combustor seal comprising: a seal body; and a plurality of seal alignment features projecting from the seal body, wherein the seal alignment features are arranged such that there is only one alignment of the combustor seal with the turbine vane.
地址 Hartford CT US