A gas turbine engine is supported on an aircraft fuselage by a pylon which carries a mounting ring. The mounting ring is releasably coupled to an engine ring on the casing of the engine, centered on the engine axis. A further member extends from the pylon and is secured to a location on the engine which is axially spaced from the mounting ring. The arrangement enables the engine to be on the pylon in different orientations, to suit different mounting configurations on the aircraft.
This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.
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