Method to reduce carbon brake wear through residual brake force
US7441844B2 · kind B2 · utility
15Cited by
28References
18Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Feb 18, 2005 |
| Grant date | Oct 28, 2008 |
| Priority date | — |
| Expiry date | Nov 10, 2025 |
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.