Turbojet engine exhaust casing with integral suspension lugs
US5190245A · kind A · utility
15Cited by
2References
3Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jun 17, 1992 |
| Grant date | Mar 2, 1993 |
| Priority date | — |
| Expiry date | Jun 17, 2012 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2230/642
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The exhaust casing of a turbojet engine has a cross-sectional shape in the form of a regular polygon and carries at least three external hanging lugs provided with holes for receiving fixing axles of a rear suspension structure for the engine. The lugs are carried by non-consecutive sides of the casing in ), manner that the geometrical axis of the hole of each lug is situated at the intersection of the median planes of the two sides of the casing adjacent the side carrying the lug.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.