U.S. Patent Specifications

Abstract

1. In a combination in an aeroplane shock absorber, a liquid damping means for absorbing the initial shock of landing and a resilient frictional device for resiliently supporting the load and effective to resiliently support the load only alter initial shock of landing has been absorbed by said liquid damping means.

Citation

(1936), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 8 No. 7, pp. 208-208. https://doi.org/10.1108/eb030076