Aircraft systems having thrust reversers with support members are disclosed herein. In one embodiment, an aircraft system includes a thrust reverser having a nozzle inner wall, a nozzle outer wall radially outward of the inner wall, and a blocker door carried by the outer wall. The blocker door is movable between a deployed position and a stowed position. The thrust reverser further includes a support member extending between a forward section of a nozzle inner wall and a forward section of the nozzle outer wall. The support member is positioned such that at least a portion of the support member is forward of the blocker door when the blocker door is in the stowed position.
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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