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JP5705108B2 |
An aircraft landing gear arrangement comprises a nose landing gear assembly and at least one main landing gear assembly. The nose landing gear assembly has a nose landing gear wheel with a high energy brake apparatus therein. The main la...
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JP5701574B2 |
A landing gear (1, 1") for an aircraft (2), having mounting means (5, 57) fitted to the fuselage (3) of the aircraft (2); at least one wheel (6); and at least one supporting arm (7, 7") having a first end portion (8, 8") connected to the...
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JP2015067273A |
To provide a system, method and apparatus for brake load alleviation among at least one first brake and at least one second brake.The method involves: sensing an amount of brake pedal application in response to application of at least br...
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JP5699021B2 |
The present disclosure provides a highly reliable landing gear assembly of an aircraft with a simple configuration. In place of conventional landing gear assemblies of aircrafts, the landing gear assembly includes a control system config...
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JP5683590B2 |
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JP5669028B2 |
An apparatus includes a fitting connected to a body. The fitting has an engagement portion including a channel formed into a peripheral surface of it and an axis. The body includes an axial layer provided around at least some of the peri...
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JP2015016847A |
To realize operation stability, stability of the attitude of an airframe on landing, an economic effect of reducing exhaustion of consumable members and prevention of damage to airframe members by debris produced on rupture breaking by a...
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JP5659370B1 |
To provide an apparatus capable of operating in a higher wave state by suppressing fluctuation of a pitch angle generated in a hydroplane body. A float 3 is divided in the length direction thereof to form a base member 3a connected to a ...
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JP5658862B2 |
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JP5656203B2 |
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JP5654563B2 |
The invention relates to a device for selectively transmitting force, the device comprising a first element and a second element that is movably mounted on the first element, a friction member being arranged between the first element and...
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JP5649711B2 |
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JP5610598B2 |
A bearing assembly (2′) comprising a housing (3′) supporting first and second bearing ring portions (4, 4′) with bearing surfaces to engage an inner tubular member (1′) at axially spaced regions, characterized in that either: the...
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JP5608918B2 |
To provide an aircraft steering angle control system that minimizes the amount of skidding of an airframe that is turning on a low-µ taxiway surface such as an icy taxiway surface and allows for directional control of the airframe by a ...
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JP5600157B2 |
The method involves correcting an instruction of braking according to a pitching angle (theta) of an aircraft (1) during braking. The correction process is carried out by subtracting the instruction of braking from a breaking setpoint co...
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JP5600155B2 |
The method involves installing a bypass (500) on brake systems of an aircraft, where the bypass is associated with insulation valves (400, 501) maintained in a normal mode in an insulation state. Each insulation valve is controllable to ...
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JP5599602B2 |
A pneumatic tire, particularly a radial aircraft tire is described. The tire (100) comprises a radial ply carcass, a tread (18), a crown reinforcement (50) comprising one or more belt layers (53) or strips reinforced by cords (51) orient...
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JP5596218B2 |
A method of positioning landing gear of an airplane is provided that includes providing the landing gear including a shock strut, a truck beam operatively pivotally connected to the shock strut, first and second interconnected links oper...
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JP5592672B2 |
A skid rail for aircrafts comprising (i) a base member comprising a long board fixed to a bottom surface of an aircraft fuselage, and bosses integrally projecting from an outer surface of the long board with longitudinal intervals, (ii) ...
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JP5584856B2 |
An actuator system (100) is provided. The actuator system (100) includes a housing (130) including a cavity (150) defined by the housing and an opening defined in a wall of the housing, the housing encasing an actuator within the cavity,...
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JP5579552B2 |
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JP5575242B2 |
A passive RFID transponder sensor system includes a sensor assembly having a focused field transponder antenna with a highly magnetically permeable transponder antenna stem, and a reader antenna with an electrical reader coil generating ...
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JP5577383B2 |
A brake monitoring system is described for use on aircraft having carbon brakes. The system displays the number of times the brakes have been applied in a preselected counting interval such as during each takeoff and landing cycle. By ra...
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JP5560189B2 |
The process for manufacturing a mechanical component (10), comprises fabricating a draft of insert by winding a beam or a sheet linked with coated wire (32) around a rotating polygonal component, inserting the draft in a first container,...
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JP5547822B2 |
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JP5547819B2 |
The invention relates to a method for making an arm for a hinged structure such as an aircraft landing gear structure, this arm comprising a main body (30; 130; 230) extending in a longitudinal direction (AP; BP; CP), and including an in...
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JPWO2012105037A1 |
Made of a material such as rubber, the fins 22 are placed on the outer surface of the ring-shaped substrate 21, and the fins on the lower part of the tire are located on the lower side of the tire than the rotational torque in the direct...
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JP5530298B2 |
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JP5531006B2 |
The invention relates to a device including elements for automatically controlling an aircraft on the ground along the lateral axis, by a dissymmetrical use of the engines and/or brakes of the aircraft.
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JP5519076B2 |
A drive unit (16) for an aircraft running gear (2) having at least a first wheel (4) and a second wheel (6) on a common wheel axis (A) is characterized in that the drive unit (16) is drivingly coupleable to the first and second wheels (4...
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JP5508455B2 |
The architecture has a normal braking hydraulic circuit (C1) including a pressure control servo valve (BCV) that has a supply port (P) connected to a pressure source (Alim), return port (R) and an utilization port (U) connected to a brak...
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JP5502496B2 |
An aircraft shock strut (12) includes a cylinder (32) and a piston (30) movable within the cylinder. A lower bearing (40) and an upper bearing (46) provide sliding engagement between the cylinder and the piston. The upper bearing is fixe...
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JP5495281B2 |
An aircraft landing gear assembly includes a bogie beam, a landing gear strut and a stop. The landing gear strut has a first end arranged to be pivotally coupled to an aircraft and a second end pivotally coupled to the bogie beam. The st...
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JP5497965B2 |
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JP5497784B2 |
The invention relates to a method of fabricating a structural part comprising a tubular portion from which there projects a structural element made of composite material, the method comprising the steps of: shaping a plane preform compri...
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JP5491164B2 |
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JP2014076797A |
To provide a braking architecture that ensures satisfactorily high reliability of both a braking system and anti-skid protection feature without an increase in the number of components included in the braking system.Each brake includes p...
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JP5480361B2 |
An anchoring harpoon intended in particular for an aircraft, capable of cooperating with an anchoring grate of a platform, includes jack elements including a cylinder element containing mobile piston elements provided with a rod that ext...
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JP5475652B2 |
The invention relates to a shock-absorber for aircraft landing gear, the shock-absorber having two elements mounted to slide telescopically one in the other and defining an internal volume that is filled with hydraulic fluid and with gas...
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JP5469374B2 |
A lock configured to lock retractable devices such as retractable landing gear for aircraft in a retracted position. The lock comprises a pivotally mounted hook member with a hook portion arranged to maintain a capture pin attached for e...
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JP5465796B2 |
A system and methods for an electric autobrake function suitable for use with an aircraft is disclosed. The system includes a single master autobrake channel configured to generate a master autobrake command and a plurality of slave auto...
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JP5457551B2 |
A method of operating an aircraft landing gear between a deployed position and a retracted position. The landing gear comprises a leg hinged to the aircraft, the leg being stabilized in the deployed position by a folding strut comprising...
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JP5443652B2 |
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JP5442857B2 |
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JP5421216B2 |
The network (10) has a three-phase power bus (11) conveying three-phase alternating current (AC) power generated by one direct current (DC)/AC converter (12) that is powered by a DC source of an aircraft. The DC/AC converter is fitted wi...
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JP5416988B2 |
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JP5409822B2 |
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JP5405290B2 |
The architecture has power distribution members (150, 250) for distributing power to respective electromechanical actuators (105, 106, 108, 205, 206, 208) connected to the architecture, where the architecture receives power from power su...
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JP5405691B2 |
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JP5379105B2 |
The architecture has electro mechanical actuator controllers (EMAC1-EMAC8) providing power signals to electro mechanical brake actuators (1-4) in response to a braking order. Wheels (L1, L2, R1, R2) on each of landing gears are regrouped...
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