Preliminary design studies are reported on engine mounting and the mounting of the throughflow nacelle for wind tunnel testing. The following problems are mentioned: possibilities for separate engine mounting and synchronous incidence adjustment, adjustment possibilities, adjustment drive, and adjustment control.
Civil Components Program 'Wing Section'. Preliminary Design of Engine Mounting
1977
35 pages
Report
Keine Angabe
Englisch
ADAPTER RING FOR ABOVE-WING MOUNTING OF BELOW-WING ENGINE
Europäisches Patentamt | 2021
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