An engine cowl door assembly is provided for fuselage mounted turbine engines to minimize manufacturing costs and part counts. In one embodiment, the engine cowl door assembly includes at least one non-handed engine cowl door, a pylon apron coupled to the fuselage of an aircraft and providing an attachment point for a first portion of the engine cowl door and a fairing coupled to the turbine engine and providing a latching point for a second portion of the engine cowl door to the turbine engine. The pylon apron, positioned on an inboard side of the turbine engine, and the fairing, positioned on an outboard side of the turbine engine, are identically shaped to provide interchangeability of the engine cowl door from a turbine engine mounted on a first side of an aircraft fuselage to a turbine engine mounted on a opposed second side of an aircraft fuselage.
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.
Enter your name and phone number, and Peter will call you back as soon as possible.
Disclaimer: The hiring of a lawyer is an important decision that should not be based solely upon advertisements. Before you decide, ask us to send you free written information about our qualifications and experience. Read More >
