The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 21, 2020

Filed:

Feb. 19, 2016
Applicant:

Orbital Australia Pty Ltd, Balcatta, Western Australia, AU;

Inventors:

Geoffrey Paul Cathcart, Mount Lawley, AU;

Stephen John Karay, Scarborough, AU;

Nicholas Coplin, Merriwa, AU;

John Howard Tubb, Befordale, AU;

Callan Murray Bleechmore, Beaconsfield, AU;

Donald Andrew Railton, Duncraig, AU;

Mario Charles Muscat, Ballajura, AU;

Assignee:

ORBITAL AUSTRALIA PTY LTD, Balcatta, Western Australia, AU;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01M 1/02 (2006.01); F02M 37/00 (2006.01); B64D 37/08 (2006.01); F01M 5/00 (2006.01); B64D 37/02 (2006.01); B60K 15/03 (2006.01); B64C 39/02 (2006.01); F02M 37/02 (2006.01); F04B 17/04 (2006.01);
U.S. Cl.
CPC ...
B64D 37/08 (2013.01); B60K 15/03 (2013.01); B64C 39/024 (2013.01); B64D 37/02 (2013.01); F01M 1/02 (2013.01); F01M 5/001 (2013.01); F02M 37/0088 (2013.01); F02M 37/025 (2013.01); F04B 17/04 (2013.01); B60K 2015/0325 (2013.01); B60K 2015/03105 (2013.01); B60K 2015/03111 (2013.01); B60K 2015/03217 (2013.01); B60K 2015/03236 (2013.01); B60K 2015/03243 (2013.01); B60Y 2200/51 (2013.01); B64C 2201/044 (2013.01); F01M 2001/0223 (2013.01);
Abstract

An unmanned aerial vehicle has an internal combustion engine, and a fuel and lubrication system comprising a fuelling system for fuelling the engine and a lubrication system for delivering lubricating oil to the engine. The fuelling system comprises a fuel reservoir from which fuel can be delivered to the engine. The fuel reservoir comprises a main tank and a header tank. The lubrication system comprises an oil tank. The oil tank is accommodated internally within the main tank to provide an integrated assembly. The arrangement provides for warming of lubrication oil for the UAV engine using several available heat sources. Further, the arrangement facilitates a configuration and layout intended to minimise or negate any undesirable moments of inertia for the UAV during flight as fuel and oil is consumed.


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