Ordnance ejector system

Ordnance – Bomb – flare and signal dropping

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Details

74 8915, 227131, 244137R, F41F 502

Patent

active

045720533

ABSTRACT:
An energy storage and release system (10) in combination with an aircraft (11) for ejecting an ordnance from the aircraft, the system (10) including a housing (22) mounted in the aircraft (11) and a drive shaft (24) having an outer end (26) and inner end (28) supported within the housing (22) for reciprocating axial movement of the outer end (26) into and out of the housing (22). An energy storage system including a flywheel (30) rotatably mounted within the housing (22) and operatively connected to the drive shaft (24) moves the outer end (26) of the drive shaft (24) axially out of the housing (22) to eject an ordnance (18). A linear induction motor (16) powers the flywheel (30).

REFERENCES:
patent: 2499712 (1950-03-01), Armstrong
patent: 2829561 (1958-04-01), Granfelt
patent: 2992594 (1961-07-01), Anderson et al.
patent: 3924692 (1975-12-01), Saari
patent: 3983783 (1976-10-01), Maxey
patent: 4031805 (1977-06-01), Puttinger et al.
patent: 4042036 (1977-08-01), Smith
patent: 4129240 (1978-12-01), Geist
patent: 4149430 (1979-04-01), F'Geppert
patent: 4323127 (1982-04-01), Cunningham
patent: 4487173 (1984-12-01), Maucher et al.

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