An aircraft brake rotor includes a circular rotor disk (10) having first and second walls (12) and a peripheral wall (14) connecting the first and second walls (12), the peripheral wall (14) including at least one notch (16) having a bottom wall (18) and first and second side walls (20) extending away from the bottom wall (18), an insert (22, 50, 60) having a first portion (24, 62) mounted against the first side wall (20) and a retainer (30, 74) connected to the rotor disk (10) and having at least one projection (38, 82), a portion of the at least one insert (22, 50, 60) extending between the at least projection (38, 82) and the first side wall (20), thus limiting movement of the insert (22, 50, 60) in a direction perpendicular to the first side wall (20).
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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