U.S. Patent Specifications

Abstract

A drop — centre aeroplane wheel comprising two main cast sections, a hub portion carried by each section, screw threads formed in a portion of one of said hub sections locking means including a threaded sleeve having an abutment slidable through a portion of the other of said hub sections and engaging the threads in said hub section, and means including a pin to lock the sleeve against rotation, relative to said other hub section.

Citation

(1938), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 10 No. 5, pp. 160-160. https://doi.org/10.1108/eb030318