An aircraft wing turbine engine is designed to increase the ground clearance for larger modernized engines mounted under the wings of an airfoil. To this end, the aircraft wing turbine engine includes a hot flow generator with a turbine engine rotating about a first central axis, a cold flow blower rotating about a second central axis, and a pod surrounding the hot flow generator and cold flow blower. The first and second central axes are offset and non-collinear with each other such that the cold flow blower can be moved farther away from the ground to increase the ground clearance of the turbine engine.
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 >
