A helicopter construction is provided in which conventional vertical upward occupant-seat ejection apparatus may be used for ejecting the pilot. A hatch or door is provided in the fuselage above the pilot's seat. Explosive charges are provided so that the hub and its associated rotating blades may be rapidly removed to provide clearance for ejection through the door.
Emergency Removal of Aircraft Sustaining Means
1966
1 pages
Report
No indication
English
Rotary systems for sustaining aircraft
Engineering Index Backfile | 1931
|Sustaining Aircraft Structural Integrity: Risk and Value Management
British Library Conference Proceedings | 2011
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