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Mra Systems Inc patents


Recent patent applications related to Mra Systems Inc. Mra Systems Inc is listed as an Agent/Assignee. Note: Mra Systems Inc may have other listings under different names/spellings. We're not affiliated with Mra Systems Inc, we're just tracking patents.

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Turbine engines with variable area nozzle

A turbine engine having an engine core, an inner cowl radially surrounding the engine core, an outer cowl radially surrounding the inner cowl and spaced from the inner cowl to form an annular passage between the inner and outer cowls that defines a nozzle, at least one control surface provided on the inner cowl and movable between a retracted position, where the nozzle has a first cross-sectional area, and an extended position where the nozzle has a second cross-sectional area that is less than the first cross-sectional area and an actuator operably coupled to the control surface and configured to move the control surface to control the cross-sectional area of the nozzle.. . ... Mra Systems Inc

Thermal insulation blanket and thermal insulation blanket assembly

A thermal insulation blanket assembly having a thermal insulation blanket including an aerogel insulation material having a first surface and a second surface that is oppositely-disposed from the first surface, a backing covering the second surface of the aerogel insulation material, and a skin layer covering the first surface of the aerogel insulation material.. . ... Mra Systems Inc

Integrated thrust reverser actuation system

A turbofan engine assembly having a turbine engine and a nacelle that surrounds at least a portion of the turbine engine to define an annular bypass duct that defines a forward-to-aft bypass air flow path. The turbofan engine assembly further comprises a fixed portion and a movable portion which is movable in a direction along the bypass air flow path to an opened position that defines a thrust reversing outlet through which at least a portion of the bypass air flow may be directed. ... Mra Systems Inc

Thrust reverser assembly

A thrust reverser assembly for a gas turbine engine including a core engine, a nacelle surrounding at least a portion of the core engine to define a bypass duct between the nacelle and the core engine, including a translating cowl moveable between a first position and a second position, a blocker door movable between a stowed position and a deployed position. The thrust reverser assembly includes multiple actuator assemblies to both translate the cowl and deploy the blocker door.. ... Mra Systems Inc

Gas turbine engine with thrust reverser assembly and method of operating

A gas turbine engine and thrust reverse assembly having a set of outer doors movable between a stowed position and an deployed position, where the set of outer doors extends outwards from the nacelle and a set of blocker doors movable between a stowed position and an deployed position, where the set of blocker door extends into an air flow conduit defined by the bypass duct to deflect air outwards.. . ... Mra Systems Inc

Thrust reverser assembly

A thrust reverser assembly for a gas turbine engine including a core engine, a nacelle surrounding at least a portion of the core engine defining a bypass duct between the nacelle and the core engine where an outer door movable between a stowed position and a deployed position extends outwards from the nacelle and a blocker door movable between a stowed position and an deployed position extends into an airflow conduit defined by the bypass duct to deflect air outwards.. . ... Mra Systems Inc

Aircraft and empennage section of an aircraft

An aircraft having a fuselage terminating in an empennage with a tail extending upwardly from the empennage. An engine strut extends from the empennage with an engine mounted to the engine strut and a moveable control surface provided on the engine strut.. ... Mra Systems Inc

Acoustic liner for gas turbine engine components

A single degree of freedom (sdof) acoustic liner includes a porous face sheet, a substantially imperforate back sheet generally parallel to and opposing said porous face sheet and defining a thickness therebetween, and an acoustic core layer of contiguous adjacent resonant cavities disposed between the porous face sheet and the imperforate back sheet. The acoustic core layer includes a first resonant cell having a first internal volume therein and a second resonant cell having a second internal volume therein different than the first internal volume. ... Mra Systems Inc








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