Patent · US Active

Engine exhaust system

US8123159B2 · kind B2 · utility

2Cited by
8References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 11, 2007
Grant dateFeb 28, 2012
Priority date
Expiry dateDec 18, 2028

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

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 system has means for maintaining a generally consistent relative alignment between the primary duct and the secondary duct.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.