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:
May. 21, 2019

Filed:

Jun. 12, 2015
Applicant:

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

Inventors:

Goeffrey Paul Cathcart, Mount Lawley, AU;

Nicolass Harry Buters, Maylands, AU;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02P 15/02 (2006.01); F02P 3/04 (2006.01); F02P 3/08 (2006.01); F02P 5/15 (2006.01); F02P 9/00 (2006.01); F02P 17/00 (2006.01); F02P 15/08 (2006.01); F02C 7/266 (2006.01); F02D 41/22 (2006.01);
U.S. Cl.
CPC ...
F02P 15/02 (2013.01); F02C 7/266 (2013.01); F02P 3/0407 (2013.01); F02P 3/0807 (2013.01); F02P 5/1502 (2013.01); F02P 9/007 (2013.01); F02P 15/08 (2013.01); F02P 17/00 (2013.01); F02D 2041/227 (2013.01); F02D 2400/08 (2013.01); Y02T 10/46 (2013.01);
Abstract

The ignition system () of an engine (particularly for a UAV) has a primary (), and a secondary () ignition system to provide redundancy for 'get you home' capability should the primary ignition system fail. The secondary ignition provides a lower energy or shorter duration spark than the higher energy or longer duration sparking of the primary ignition system, and is retarded relative to primary sparking. Timing of the secondary sparking can be advanced in the event of primary sparking failure. Fuelling strategy can be shifted from a leaner stratified charge to a richer homogenous charge when relying just on the secondary ignition system for ignition. The secondary ignition system can be of a lower spark energy and/or duration than the primary ignition system, avoiding the cost, complexity and weight of replicating the primary ignition system, and to improve packaging within the engine housing, particularly within the limited payload and space limits of a UAV.


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