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US 2026/0092580 A1Published application
Ram air turbine fixed within aircraft
AssigneeHamilton Sundstrand Corporation
InventorsViktor Kilchyk, Debabrata Pal
Life of this patent
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Abstract
An aircraft system, having: a section of a fuselage surrounding an interior portion of an aircraft; an aperture defined along the section of the fuselage; an inlet scoop at the aperture; an inlet channel extending away from the inlet scoop to the interior portion of the aircraft; and a Ram Air Turbine (RAT) connected to the inlet channel, wherein the RAT is fixed within the interior portion of the aircraft.
Claims18
An aircraft system, comprising:
- a section of a fuselage surrounding an interior portion of an aircraft;
- an aperture defined along the section of the fuselage;
- an inlet scoop at the aperture;
- an inlet channel extending away from the inlet scoop to the interior portion of the aircraft;
- and
- a Ram Air Turbine (RAT) connected to the inlet channel, wherein the RAT is fixed within the interior portion of the aircraft.
3 more elements
An aircraft system, comprising:
- a fuselage surrounding an interior portion of an aircraft;
- wherein the fuselage defines a forward portion and an aft portion, wherein the fuselage defines stagnation zones including a first stagnation zone in the forward portion and a second stagnation zone in the aft portion;
- a first aperture defined at the first stagnation zone and a second aperture defined at the second stagnation zone;
- an inlet scoop at the first aperture;
- an exhaust vent at the second aperture;
- an inlet channel extending away from the inlet scoop to the interior portion of the aircraft;
- a Ram Air Turbine (RAT) connected to the inlet channel, wherein the RAT is fixed within the interior portion of the aircraft;
- and
- an outlet channel extending from the RAT to the exhaust vent.
6 more elements
Dependencies are inferred from the claim text.