MESSIER-BUGATTI-DOWTY
200Patents
200Active
200Granted
59Portfolio score
Filing activity: Mar 2, 2004 → Jun 24, 2019 · 55 expiring within 5 years
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9758678B2 | Protecting parts made of carbon-containing composite material from oxidation | Mechanical Engineering; Lighting; Heating | 25 | Active |
| US8602352B2 | Method for operating a landing gear assembly with a breaker strut | Performing Operations; Transporting | 23 | Active |
| US9969233B2 | Mechanical actuator with a hydraulic damper device | Emerging Cross-Sectional Technologies | 16 | Active |
| US9056431B2 | Apparatus comprising an end fitting connected to a body | Emerging Cross-Sectional Technologies | 12 | Active |
| US8403259B2 | Method of taxiing an aircraft | Emerging Cross-Sectional Technologies | 12 | Active |
| US8998348B2 | Hydraulic brake architectures for aircrafts for braking at least one wheel of the aircraft | Performing Operations; Transporting | 11 | Active |
| US8491740B2 | Method of connecting a composite material structural element to a tube | Emerging Cross-Sectional Technologies | 10 | Active |
| US8220598B2 | Friction device for controlling force, and a friction damper comprising such a device | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US9145204B2 | Device for unlocking an undercarriage in a deployed position, and an undercarriage fitted with such a device | Performing Operations; Transporting | 9 | Active |
| US9517837B2 | Method for reducing the apparent manoeuvring time for landing gear of an aircraft | Performing Operations; Transporting | 9 | Active |
| US8294408B2 | Power supply with two series inverters for a polyphase electromechanical actuator | Electricity | 9 | Active |
| US9650131B2 | Method for rotationally driving an aircraft wheel | Emerging Cross-Sectional Technologies | 8 | Active |
| US8393565B2 | Method of feeding energy to actuators associated with an aircraft undercarriage | Performing Operations; Transporting | 8 | Active |
| US9855792B2 | Aircraft wheel comprising a duct establishing a leakage path in the wheel | Performing Operations; Transporting | 8 | Active |
| US8604733B2 | Electric actuator including two current-controlled voltage inverters powering an electrical machine, and reconfigurable in the presence of a defect | Electricity | 7 | Active |
| US9540097B2 | Multifunction device for an undercarriage | Emerging Cross-Sectional Technologies | 7 | Active |
| US9197088B2 | Module for converting voltage between a high-voltage electrical network of an aircraft and an energy storage element | Electricity | 6 | Active |
| US10053210B2 | Aircraft undercarriage including a telescopic linear rod | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8430457B2 | Wheel bar and a wheel specially adapted therefor | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8152247B2 | Method of managing the power supply to a non-reversible actuator for a vehicle wheel brake | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8948994B2 | Electromechanical braking system for an aircraft | Performing Operations; Transporting | 6 | Active |
| US8268393B2 | Method of fabricating a friction part out of carbon/carbon composite material | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US9399806B2 | Titanium alloy composition for the production of high-performance parts, in particular for the aeronautical industry | Chemistry; Metallurgy | 5 | Active |
| US8311685B2 | Method of distributing braking within at least one group of brakes of an aircraft | Performing Operations; Transporting | 5 | Active |
| US8444086B2 | Aircraft wheel-and-brake set fitted with a rotary drive device | Emerging Cross-Sectional Technologies | 5 | Active |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.