Method to reduce carbon brake wear through residual brake force
US7735938B2 · kind B2 · utility
8Cited by
30References
23Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Oct 17, 2007 |
| Grant date | Jun 15, 2010 |
| Priority date | — |
| Expiry date | Jun 5, 2028 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C25/44
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The method for reducing aircraft carbon brake wear involves monitoring the commanded initiation of braking, and setting a residual brake clamping force to a predetermined minimum residual brake clamping force, which is maintained following the commanded initiation of braking to prevent release of braking during taxiing of the aircraft. The minimum residual brake clamping force is applied despite a commanded release of braking until at least one predetermined control logic condition occurs.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.