REDUCTION OF VULNERABILITY OF AIRCRAFT HYDRAULIC SYSTEMS

Format:

Other

Author/Creator:

Field, Howard, author.

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1945

Summary:

SUMMARYThe problem of the reduction of the vulnerability to damage of aircraft hydraulic systems is divided into two catagories.Various methods of attack upon each catagory are outlined and the suggestion made that the problem be attacked from both sides and by several methods simultaneously. When all engineers cooperate they can design hydraulic systems having very low relative vulnerability thus permitting full enjoyment of the weight savings, reliability, ease of repair, flexibility, and accuracy of control, which hydraulic systems provide.This paper is presented in the hope that it will stimulate thought by all aircraft engineers to the end that our airplanes will be not only better but safer

Notes:

Vendor supplied data

Publisher Number:

450074

Access Restriction:

Restricted for use by site license