Invention Grant
- Patent Title: Engine exhaust system with directional nozzle
- Patent Title (中): 发动机排气系统带定向喷嘴
-
Application No.: US12303970Application Date: 2007-06-11
-
Publication No.: US08132755B2Publication Date: 2012-03-13
- Inventor: Charles Hollimon , John Barber , John Herman Sherrer , Robert Laramee
- Applicant: Charles Hollimon , John Barber , John Herman Sherrer , Robert Laramee
- Applicant Address: US TX Fort Worth
- Assignee: Bell Helicopter Textron Inc.
- Current Assignee: Bell Helicopter Textron Inc.
- Current Assignee Address: US TX Fort Worth
- Agent James E. Walton; Richard G. Eldredge
- International Application: PCT/US2007/013675 WO 20070611
- International Announcement: WO2008/127260 WO 20081023
- Main IPC: B64C15/12
- IPC: B64C15/12

Abstract:
An exhaust system for an aircraft has a primary exhaust duct for communicating exhaust gas from an engine exhaust exit and is configured for movement with the engine. A secondary exhaust duct is in fluid communication with the primary exhaust duct and is movably mounted to the airframe. The secondary duct has a portion selectively rotatable relative to the remainder of the secondary duct for directing the exhaust gas vector. The system has means for maintaining a generally consistent relative alignment between the primary duct and the secondary duct.
Public/Granted literature
- US20110131948A1 Engine Exhaust System with Directional Nozzle Public/Granted day:2011-06-09
Information query