Ratier-Figeac Sas

Hamilton Sundstrand Corporation

Ratier Figeac

Christian Fages

Bruno Seminel

Floyd Kent Matlack

A bellows comprises a unitary bellows body extending from a first end to a second end in an axial direction. The stiffness of the bellows body varies in at least an axial direction.

Bellows

A tank that may be used in combination with an actuating means such as a pneumatic door actuator includes a first, inner, enclosure positioned and enclosed within a second, outer, enclosure, to provide an enclosed chamber between the inner enclosure and outer enclosure. The pressure in the chamber may be measured with a gauge that does not extend into the inner enclosure. The measured pressure may then be monitored and compared in order to detect a change in pressure and thereby also detect a leak through a wall from the inner enclosure. The tank may also be used to inflate and/or deploy an emergency evacuation slide in an aircraft.

Fail-safe tank with integrated sensor and methods for detecting a leak in a wall of the tank

An ice breaking seal for a ball screw comprises a first, ice breaking section and a second, sealing section formed integrally with the ice breaking section. The ice breaking section is formed of a polymeric material and has a first hardness. The sealing section is formed of a polymeric material and has a second hardness, which is lower than the first hardness.

Ice breaking seal

A method of mounting a metal blade root to a composite propeller blade body includes inserting a connection portion of the blade body into a bore formed in the blade root, wherein the connection portion comprises at least one depression formed in an outer surface thereof, and applying pressure to the outer surface of the blade root to cause it to deform and engage with the depressions, thereby mechanically coupling the blade root to the propeller blade body.

Propeller blade root coupling

A counterweight for use in a variable-pitch propeller system (includes a weighted element having walls forming a sealed chamber). The sealed chamber contains a weighting material, and an arm. The counterweight is configured to be coupled to a propeller blade the walls of the weighted element and the arm comprise a single piece, and are an additively manufactured single piece. The weighting material may comprise a powder element. The sealed chamber may have been sealed during the additive manufacturing process, or after the additive manufacturing process has been completed.

Propeller counterweight

A propeller blade retention element comprises a body portion formed of a corrosion resistant metal, and at least one bearing race portion attached to the body portion, the race portion being formed of an induction hardenable, corrosion resistant metal.

Propeller blades

A transmission or gearbox assembly with fail-safe means for providing redundancy where failure can lead to loss of torque transmission between component parts of the assembly, the assembly comprising a plurality of first components in torque transmitting engagement and at least one second component associated with at least one of the first components, the second component being joined to the respective first component by a discontinuous joint. Preferably, each first component of the system has a corresponding second component joined thereto by a discontinuous joint.

Gearbox assembly

A valve comprises a valve seat and a rotary valve element. The valve seat comprises a valve opening having a sealing surface. The valve element is mounted with respect to said valve seat for rotation about an axis of rotation between a closed position in which the valve element substantially closes the valve opening and an open position in which the valve element permits flow through the valve opening. The valve opening is elliptical in shape, having spaced apart upper and lower edges the upper and lower edges being generated as respective ellipses formed by parallel sections through a conical surface. The valve seat sealing surface is defined between said upper and lower edges.

Fluid flow control valves

A weldless assembly comprises a plurality of tubes, wherein the plurality of tubes includes an inner tube, an intermediate tube, and an outer tube; a first closure end configured to cap a first side of the plurality of tubes; and a second closure end configured to cap a second side of the plurality of tubes.

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Figeac, France

Christian Fages