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US 2026/0126007 A1Published application
Gas turbine engine for an aircraft
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorsGideon Daniel VENTER, Michael SCHACHT
Life of this patent
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Abstract
Proposed is a gas turbine engine for an aircraft, having an oil system that includes an oil tank and at least one shaft that is mounted rotatably on a casing by means of bearing units. At least one of the bearing units and the oil tank are arranged in a bearing chamber.
Claims15
A gas turbine engine for an aircraft, having an oil system that comprises an oil tank, and having at least one shaft that is mounted rotatably on a casing by means of bearing units, at least one of the bearing units and the oil tank being arranged in a bearing chamber,
- wherein
- an interior space of a casing of the oil tank is connected via a venting line to a breather, in the region of which the amount of oil in the air can be reduced.
Dependencies are inferred from the claim text.