Matches 1 - 21 out of 21


Match Document Document Title
US20110132704 BRAKE ACTUATOR ASSEMBLY WITH LINE REPLACEABLE MOTOR FEATURES  
An aircraft brake system electromechanical actuator is provided. The actuator is configured with features that allow the electric motor to be a line replaceable unit. One such feature is a...
US20090065640 BRAKING-ENERGY EQUALIZATION SYSTEM  
A braking-energy equalization system applied to an aircraft undercarriage, which undercarriage includes at least two sets of landing gear, with each set of landing gear including at least two...
US20080135680 Methods and brake disc assemblies to increase the use of friction material  
Methods and brake disc assemblies are disclosed to increase the use of friction material. A disclosed example carbon composite brake disc includes a generally annular body having an opening, an...
US20100090058 BRAKE SHUTOFF VALVE TEST  
A system, apparatus and method of verifying operation of a vehicle fluid brake system shutoff valve is provided, wherein the shutoff valve is adapted to enable or inhibit the transmission of fluid...
US20060243857 Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system  
This invention relates to method and apparatus of the calculation of aircraft braking friction and other relating landing parameters including but not limited to aircraft braking action, aircraft...
US20080272235 Load-distributing rotor insert for aircraft brakes  
An aircraft brake rotor includes a circular rotor disk (10) having first and second walls (12) and a peripheral wall (14) connecting the first and second walls (12), the peripheral wall (14)...
US20090065635 Pitch-oscillation limitation system applied to an aircraft  
A pitch-oscillation limitation system, applied to an aircraft having main landing gear located toward the center of the aircraft and forward landing gear located under the nose of the aircraft,...
US20110253833 BRAKE SYSTEM FOR AIRCRAFT UNDERCARRIAGE  
A braking system for an aircraft provided with undercarriage, wherein an axial-flux reversible electrical machine is associated to at least one wheel of the undercarriage and is set in rotation by...
US20100090059 BRAKING  
A brake apparatus (1) and method of operating the apparatus are disclosed. The apparatus (1) has a plurality of brake elements (2, 3, 4, 5, 6) with a combined thickness of Y. At least one of the...
US20110062280 ELECTROMAGNETIC LANDING GEAR BRAKES  
An electromagnetic control for the landing gear of an aircraft includes a hub to be fixed to a frame of an aircraft landing gear. A rotor rotates with a tire on the aircraft landing gear....
US20090069958 SYSTEME DE FREINAGE DIFFERENTIEL  
A braking system for the landing gear of an aircraft, which landing gear includes a bogey containing at least four wheels, each equipped with a brake, with the bogey having at least two axles that...
US20100078519 METHOD TO DEGRADE BRAKING MODES  
A system, apparatus and method of controlling a braking system of a vehicle having a plurality of rotating wheels and a plurality of brakes, each brake corresponding to one of the plurality of...
US20110220763 TAPERED BRAKE DISK  
A brake stack comprises a stator having an annular, inner periphery section disposed substantially along a first radial plane extending normal to an axis of a wheel, and a stator side wall having...
US20100276988 DIFFERENTIAL EMERGENCY/PARK ELECTRIC BRAKE SYSTEM  
A system, apparatus and method provide emergency differential braking for effecting braked steering of an aircraft. A brake input device is provided that not only allows for emergency and parking...
US20140209739 METHOD AND DEVICE FOR LATERAL CONTROL OF A TAXIING AIRCRAFT  
The device includes, but is not limited to a calculating unite for automatically applying, if conditions for turning of the aircraft are met, a symmetrical braking value at a brake assembly, then...
US20100104465 COMBUSTION SYNTHESIS TO BOND METAL INSERTS TO C-C COMPOSITE SURFACES  
Method of joining a carbon-carbon composite piece 30 together with a metal insert 20, e.g. in the manufacture of aircraft brake discs 10. The method includes the steps of: providing a...
US20050194495 Aircraft landing gear  
The present invention relates to aircraft landing gear having a landing gear brake to brake at least one landing gear wheel and a hydraulic supply for the actuation of the landing gear brake. The...
US20100116604 SECURITY BRAKING DEVICE MOUNTED BETWEEN A HYDRAULIC FUEL TANK AND ACTUATION MEMBERS CAPABLE OF ACTING ON BRAKING MEMBERS  
The device includes a loading and non-compression locking mechanism for a master cylinder hydraulically connected to a hydraulic fuel tank and to braking members. The mechanism is dependent upon a...
US20100274458 ELECTRIC BRAKE ARCHITECTURE WITH DISSIMILAR EMERGENCY BRAKING PATH  
A system, apparatus and method provide a means for controlling an electric brake actuator. An electromechanical actuator controller (EMAC) is configured to receive first data indicative of a...
US20150291280 AIRCRAFT ELECTRIC BRAKING SYSTEM  
An electrically actuated braking system for an aircraft, comprising: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an...
US20150266567 ELECTRIC HYDRAULIC MOTOR SYSTEM FOR AIRCRAFT  
An electric hydraulic motor system for aircraft having a taxing and takeoff mode and a braking mode. While in the taxiing and takeoff mode, a battery and optionally other sources of energy stored...

Matches 1 - 21 out of 21