Lateral turbojet improved in order to limit the deformation thereof
US9366186B2 · kind B2 · utility
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10References
13Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jul 15, 2011 |
| Grant date | Jun 14, 2016 |
| Priority date | — |
| Expiry date | Jan 29, 2033 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/941
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbojet includes an intermediate casing outer shroud connected to a front suspension and a primary structure connected to a rear suspension; the shroud and the primary structure are held in a coaxial relationship by arms with at least some of the arms being shaped and/or arranged to deform in response to thrust from the turbojet by creating a deforming torque between the shroud and the primary structure in opposition to opposing stress generated by the thrust.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.