Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Reexamination Certificate
2008-06-04
2011-12-20
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
C244S003210, C244S003100
Reexamination Certificate
active
08080772
ABSTRACT:
A modular electromechanical actuation system assembly is provided that includes an electronic control unit housing having a plurality of motor receptacles and a plurality of battery receptacles formed in an outer surface thereof. Each of the motor receptacles has an associated motor electrical interface, and each of the battery receptacles has an associated battery electrical interface. An electronic control unit is disposed within the electronic control unit housing and is electrically coupled to each of the motor electrical interfaces and each of the battery electrical interfaces. A plurality of motors are supported, one each, within one of the motor receptacles, and a plurality of batteries are supported, one each, within one of the battery receptacles.
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Benson Dwayne M.
Geck Kellan
Sarlioglu Bulent
Woessner George
Benedik Justin
Dinh Tien
Honeywell International , Inc.
Ingrassia Fisher & Lorenz P.C.
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