Bypass turbojet-engine cowling comprising an electrically grounded displaceable component
US6237325A · kind A · utility
17Cited by
3References
19Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Sep 1, 1999 |
| Grant date | May 29, 2001 |
| Priority date | — |
| Expiry date | Sep 1, 2019 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbojet-engine cowling combined with a thrust reverser comprising a large-displacement displaceable component (7) includes an electrically grounding mechanism for the displaceable component (7) when in its forward-thrust position. The grounding mechanism comprises an elastic device (20) dedicated to shunt the electric current away from any mechanical member used in the displacement without any displaceable connecting element.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.