Means and method for uncaging a gyroscope rotor

Claim 2

For a gyroscope adapted for use in a vehicle intended for a single usage, the gyroscope having a rotor and means for rotationally accelerating the rotor upon its spin axis, relative to a supporting structre, to a predetermined rotational velocity, apparatus for permitting rotational acceleration of the rotor about its spin axis while constraining the rotor against rotation about another axis and, upon the rotor being accelerated to a predetermined rotational velocity, for releasing the rotor to permit its rotation about at least one other axis relative to the supporting structure, the apparatus comprising: a housing; a first bearing means, mounted on the housing, for permitting rotation of the rotor upon the rotor spin axis and upon at least one other axis intersecting the spin axis; constraining means, mounted on the housing and spaced from the first bearing means, for initially constraining the rotor from rotation relative to the housing about the at least one other axis while permitting rotation of the rotor about its spin axis, and for subsequently releasing the rotor, upon the rotor being accelerated to its predetermined rotational velocity, to permit rotation of the rotor relative to the housing about the at least one other axis, the constraining means having a solid propellant structure which comprises a means for caging the rotor prior to release of the rotor; and means for igniting the solid propellant structure for causing the solid propellant structure to be consumed subsequent to the rotor being accelerated to its predetermined rotational velocity, whereby the rotor is permitted to rotate about the at least one other axis relative to the housing.

Claim 3

The apparatus of claim 1, wherein the rotor includes an axisymmetrical portion extending coaxially along the spin axis and within the constraining means.

Claim 4

The apparatus of claim 2, wherein the solid propellant structure defines an opening, the axisymmetrical rotor portion extending within the opening and being constrained within the solid propellant structure prior to ignition of the solid propellant structure.

Claim 5

The apparatus of claim 3, wherein the constraining means includes an annular, second bearing, the second bearing being mounted on the housing coaxially of the spin axis of the rotor, the solid propellant structure comprising an annular sleeve coaxially and rotatably mounted within the second bearing, the axisymmetrical rotor structure being immovably seated within the solid structure, propellant body, whereby the solid propellant structure is caused to rotate with the rotor during rotational acceleration of the rotor.

Claim 8

For a gyroscope adapted for use in a vehicle intended for a single usage, the gyroscope having a rotor adapted to be rotationally accelerated upon its spin axis, relative to a supporting structure, apparatus for rotationally accelerating the rotor about its spin axis while constraining the rotor against rotation about another axis and, upon the rotor being accelerated to a predetermined rotational velocity, for releasing the rotor to permit its rotation about at least one other axis relative to the supporting structure, the apparatus comprising: a housing; a first bearing means, mounted on the housing, for permitting rotation of the rotor upon the rotor spin axis and upon at least one other axis intersecting the spin axis; means for rotationally accelerating the rotor about its spin axis, the means for rotationally accelerating the rotor comprising a solid propellant charge, means for igniting the charge, means for directing the resultant gasses toward the rotor, and means on the rotor for reacting against the gasses; constraining means, mounted on the housing and spaced from the first bearing means, for initially constraining the rotor from rotation relative to the housing about the at least one other axis while permitting rotation of the rotor about its spin axis, and for subsequently releasing the rotor, upon the rotor being accelerated to its predetermined rotational velocity, to permit rotation of the rotor relative to the housing about the at least one other axis, the constraining means having a solid propellant structure which comprises a means for caging the rotor prior to release of the rotor; and means for igniting the solid propellant structure for causing the solid propellant structure to be consumed subsequent to the rotor being accelerated to its predetermined rotational velocity, whereby the rotor is permitted to rotate about the at least one other axis relative to the housing.

Claim 9

For a gyroscope adapted for use in a vehicle intended for a single usage, the gyroscope having a rotor adapted to be rotationally accelerated upon its spin axis, relative to a supporting structure, apparatus for rotationally accelerating the rotor about its spin axis while constraining the rotor against rotation about another axis and, upon the rotor being accelerated to a predetermined rotational velocity, for releasing the rotor to permit its rotation about at least one other axis relative to the supporting structure, the apparatus comprising: a housing; a first bearing means, mounted on the housing, for permitting rotation of the rotor upon the rotor spin axis and upon at least one other axis intersecting the spin axis; means for rotationally accelerating the rotor about its spin axis, the means for rotationally accelerating the rotor comprising a solid propellant charge, means for igniting the charge, means for directing the resultant gasses toward the rotor, and means on the rotor for reacting against the gasses; constraining means, mounted on the housing and spaced from the first bearing means, for initially constraining the rotor from rotation relative to the housing about the at least one other axis while permitting rotation of the rotor about its spin axis, and for subsequently releasing the rotor, upon the rotor being accelerated to its predetermined rotational velocity, to permit rotation of the rotor relative to the housing about the at least one other axis, the constraining means having a solid propellant structure which comprises a means for caging the rotor prior to release of the rotor; and means for igniting the solid propellant structure for causing the solid propellant structure to be consumed subsequent to the rotor being accelerated to its predetermined rotational velocity, whereby the rotor is permitted to rotate about the at least one other axis relative to the housing.