Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Aircraft brake wear limit indicator having integral configuration control and method

Aircraft brake wear limit indicator having integral configuration control and method

US Patent 5228541 · Granted Jul 20, 1993

Estimated economic value: $30,822,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Shape memory alloy locking apparatuses2022
Methods and apparatus for controlling landing gear retract braking2022
Methods and apparatus for controlling landing gear retract braking2021
Hydraulic systems for shrinking landing gear2020
Hydraulic systems for shrinking landing gear2020
Methods and apparatus for controlling landing gear shrink2019
Aircraft door dampening system2016
Electrical interlock and indication system for aircraft2009
Actuation system for tail section of aircraft2008
Cargo door electrical control and warning indication system and method of use2003
Hydraulic actuation system for cargo doors with cam-type latches2002
Aircraft door latch lock mechanism1994