Invention Grant
- Patent Title: Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle
-
Application No.: US14822973Application Date: 2015-08-11
-
Publication No.: US10012104B2Publication Date: 2018-07-03
- Inventor: Donald W Peters
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Bachman & LaPointe, P.C.
- Main IPC: F02K1/00
- IPC: F02K1/00 ; F01D17/16 ; F01D9/02 ; F02K1/12 ; F02K3/10
Abstract:
A nozzle system includes a static structure including a multiple of convergent flap rails and a synchronization ring including an inner ring radially spaced from an outer ring via a multiple of struts. The multiple of convergent flap rails extend at least partially between the inner ring and the outer ring.
Public/Granted literature
- US20160102574A1 Gas Turbine Engine Convergent/Divergent Nozzle With Unitary Synchronization Ring For Roller Track Nozzle Public/Granted day:2016-04-14
Information query
