Tank suitable for holding liquids
AssigneeROLLS-ROYCE plc
InventorsGeorge H. Bennett, Alfred W. Osborn, Clive N. Bunyan, Ronald A. Midgley
Life of this patent
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Abstract
An oil tank suitable for an aircraft mounted gas turbine engine is divided into three series connected chambers. Aerated oil after engine use is fed into the first chamber and de-aerated oil withdrawn from the third chamber for engine use. The chambers are interconnected in such a manner that when the tank is inverted, a reservoir of oil is retained within the third chamber to provide a continued supply of oil to the oil outlet for a finite time period and insufficient oil flows into the first chamber from the second to obstruct an air vent provided in the first chamber.
Claims8
A tank suitable for holding a liquid comprising first and second baffles adapted to divide the interior of said tank into first, second and third series interconnected chambers, each adapted to contain said liquid, and inlet adapted to supply a mixture of a gas and said liquid to said first chamber, an outlet adapted to withdraw said liquid from said third chamber and venting means having an outlet through which said gas present in said first chamber is vented, said baffles being so adapted and arranged that when said tank is in its normal spacial disposition, liquid supplied in operation to said first chamber flows into said third chamber via said second chamber, and if said tank subsequently adopts a spacial position other than said normal spacial disposition, the flow of liquid from said third chamber to said second chamber is prevented or is of a sufficiently low level that an adequate quantity of liquid is retained within said third chamber to provide a continuity of liquid flow through said outlet for a finite time period and unsufficient liquid flows from said second chamber into said first chamber to obstruct said venting means.
Dependencies are inferred from the claim text.