Invention Application
- Patent Title: SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR
- Patent Title (中): 燃气轮机发动机喷油器接口
-
Application No.: PCT/US2014038214Application Date: 2014-05-15
-
Publication No.: WO2015053818A3Publication Date: 2015-06-18
- Inventor: DRAKE CHRISTOPHER , MAX SETH A , HARRIS MEGGAN
- Applicant: UNITED TECHNOLOGIES CORP
- Assignee: UNITED TECHNOLOGIES CORP
- Current Assignee: UNITED TECHNOLOGIES CORP
- Priority: US201361846110 2013-07-15
- Main IPC: F23R3/14
- IPC: F23R3/14
Abstract:
A swirler for a combustor of a gas turbine engine includes a swirler outer body with a swirler threaded section defined around a swirler central longitudinal axis. A bulkhead support shell for a combustor of a gas turbine engine includes a swirler boss with a boss threaded section defined around a swirler central longitudinal axis. A combustor of a gas turbine engine includes a bulkhead support shell with a swirler boss. The combustor also includes a swirler mountable to the swirler boss at a threaded interface defined around a swirler central longitudinal axis.
Information query