TY  - JOUR
AB  - In an aircraft an engine mounting device comprising essentially an adaptor ring unitary with said engine and having only three shock absorbing engine connection fittings unitary therewith and extending outwardly therefrom in spaced relation there around, a pair of pyramidal frames composed of strut means connected respectively at their apex ends to two of said iittings and extending into rigid connexion at the other of their ends with said aircraft, and a triangular frame composed of strut means connected at its apex end to the other of said fittings and extending therefrom into rigid connexion at its base end with said aircraft.
VL  - 14
IS  - 3
SN  - 0002-2667
DO  - 10.1108/eb030887
UR  - https://doi.org/10.1108/eb030887
PY  - 1942
Y1  - 1942/01/01
TI  - U.S. Patent Specifications
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 89
EP  - 90
Y2  - 2024/04/18
ER  -