Magnetic gyro-projectile device with electronic combustion,...

Details Magnetic gyro-projectile device with electronic combustion,... Magnetic gyro-projectile device with electronic combustion,...

2006-10-12

2009-06-02

Gregory, Bernarr E (Department: 3662)

Aeronautics and astronautics

Missile stabilization or trajectory control

C244S003230, C089S001510, C089S001550, C102S200000, C102S206000, C102S207000, C102S208000, C102S209000, C102S473000, C102S501000

Reexamination Certificate

active

07541563

ABSTRACT:
A hollow cylinder has an electromagnet to hold back a canister and either an induction heating linear actuator or a firing pin to ignite the primer-containing combustive material inside the canister to eject a locked piston from the cylinder. There is a motor-included turbogenerator around the cylinder, which converts the energy of the post-combustion gases into electricity to get stored and to power an integrated or separate annular stator assembly to give the ejected piston a rotatory motion for stability in projectile motion. Another device has a helically arranged, multi-pole permanent magnet assembly annularly integrated around the cylinder to give the ejected piston a rotatory motion for stability in projectile motion. In other forms, an annular stator assembly around the cylinder is supplied with switched, externally generated electric power without either a turbogenerator or the motor-included turbogenerator to respectively produce electricity or to provide gyroscopic stability to the cylinder.

REFERENCES:
patent: 2853009 (1958-09-01), Bianchi
patent: 2882824 (1959-04-01), Larsen et al.
patent: 2892412 (1959-06-01), Mullins et al.
patent: 3877378 (1975-04-01), Clark et al.
patent: 3886867 (1975-06-01), Krupen
patent: 3967141 (1976-06-01), Gawlick et al.
patent: 4037517 (1977-07-01), Briggs et al.
patent: 5485788 (1996-01-01), Corney
patent: 6082267 (2000-07-01), Cooper

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