Aircraft with reciprocating engines partially embedded in the fuselage
US8573532B2 · kind B2 · utility
0Cited by
3References
9Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Oct 20, 2009 |
| Grant date | Nov 5, 2013 |
| Priority date | — |
| Expiry date | Nov 17, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D29/04
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft provided with turbojet engines of which the nacelles are partially embedded in the fuselage of the aircraft is disclosed. The aircraft includes an internal space at engine nacelles. The internal space includes a platform capable of supporting personnel and maintenance equipment, with the portions of the nacelles located inside the aircraft comprising trapdoors or devices for accessing inside the engines from the platform.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.