Gyroscopically stabilized apparatus

• US 5,184,521 A
• Filed: 11/18/1991
• Issued: 02/09/1993
• Est. Priority Date: 11/18/1991
• Status: Expired due to Fees

• Current Assignee: Nelson Tyler
• Original Assignee: Nelson Tyler
• Inventors: Tyler, Nelson
• Primary Examiner(s): Bonck, Rodney H.
• Application Number:
  US07/794,000
• Time in Patent Office: 449 Days
• Field of Search: 74/5.34, 74/5.22, 74/5.44, 74/5.42, 74/5.1, 352/243, 354/70, 354/81, 248/612, 248/323, 248/324
• US Class Current: 74/5.34
• CPC Class Codes: G01C 21/18 Stabilised platforms, e.g. by gyroscope
• CPC Class Codes: G03B 15/006 Apparatus mounted on flying objects
• CPC Class Codes: Y10T 74/1204 with caging or parking means
• CPC Class Codes: Y10T 74/1218 Combined
• CPC Class Codes: Y10T 74/1221 Multiple gyroscopes
• CPC Class Codes: Y10T 74/1236 by plural diverse forces
• CPC Class Codes: Y10T 74/1243 by weight

Abstract

A gyroscopically stabilized apparatus for aiming an instrument at a target object. An external yoke is attached to the ends of a hub assembly which supports the gyro and camera platforms for rotation about pan, tilt and roll axes. The yoke is associated with an externally located vibration damping system interposed between the yoke and the support arm attached to the helicopter or other transporting vehicle. This makes possible a greater degree of helicopter pitch and roll without having any support structure impact the gyro and camera. In one embodiment the platforms are associated with separately rotatable hemispheres joined to provide a spherical fairing. In another embodiment the hemispheres are attached together for common rotation about pan and tilt axes.

Claims

1. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means including a pair of hub shafts disposed along a first axis and having opposite extremities, respectively;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and comprising a yoke having a half circle configuration, a midportion and opposite extremities, and coupled at its midportion to the support means, and coupled at its opposite extremities to the opposite extremities of the pair of hub shafts, and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes.

2. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means including a pair of hub shafts disposed along a first axis and having opposite extremities, respectively;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and comprising a yoke having a central portion having a half circle configuration, and coupled at its central portion to the support means, the yoke further having opposite extremities oppositely horizontally offset, with the ends of the opposite extremities coupled to the opposite extremities of the pair of hub shaft, and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes.

3. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means including a hub shaft disposed along a first axis and having an outer extremity;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and comprising a yoke having a quarter circle configuration and opposite extremities, and coupled at its opposite extremities to the support means and to the outer extremity of the hub shaft, respectively, and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes.

4. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means disposed along a first axis;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means;

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes; and

fairing means in surrounding relation to the instrument platform and the gyro platform, with the yoke means being located exteriorly of the fairing means, the fairing means comprising a first hemisphere coupled to and movable with the instrument platform, and a second hemisphere coupled to and movable with the gyro platform.

5. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means disposed along a first axis;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means;

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes; and

fairing means in surrounding relation to the instrument platform and the gyro platform, with the yoke means being located exteriorly of the fairing means, the fairing means comprising a first hemisphere coupled to and movable with the instrument platform, and a second hemisphere coupled to the first hemisphere for rotation therewith.

6. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means disposed along a first axis;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

fairing means in surrounding relation to the instrument platform and the gyro platform;

yoke means coupled to the hub shaft means and located exteriorly of the fairing means and outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means;

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes, the support means including a support arm adapted for connection to a vehicle; and

vibration isolating and damping means interposed between the yoke means and the support arm and located exteriorly of the fairing means.

7. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means disposed along a first axis;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space, the gyro platform mounting a gyro housing for rotation about a fourth axis, and mounting a third axis motor having a driving element operative to develop a driving torque tending to rotate the housing about the fourth axis whereby, upon stabilization of the gyro housing, the stabilized gyro housing resists the driving torque and instead the instrument platform rotates about the third axis;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes.

8. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means disposed along a first axis;

an instrument platform for supporting an instrument, and mounting a driven element for rotation about a second axis;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space, the gyro platform mounting a second axis motor having a driving element operative to develop a driving torque tending to rotate the housing about the second axis whereby, upon stabilization of the gyro housing, the stabilized gyro housing resists the driving torque and instead the instrument platform rotates about the second axis;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes.

9. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means disposed along a first axis;

an instrument platform for supporting an instrument, and mounting a second axis motor operative to develop a driving torque;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including second bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space, the gyro platform mounting a gyro housing for rotation about a fourth axis, the gyro platform tending to be rotated about the second axis by the driving torque of the second axis motor of the instrument platform whereby, upon stabilization of the gyro housing, the stabilized gyro housing resists the driving torque and instead the instrument platform rotates about the second axis;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes.

10. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

hub shaft means disposed along a first axis;

an instrument platform for supporting an instrument;

a hub assembly including first bearing means defining the first axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the first axis, the hub assembly including bearing means defining a second axis perpendicular to the first axis and supporting the instrument platform upon the hub assembly for rotation of the instrument platform along a rotational path extending about the second axis;

a gyro platform including at least three gyroscopes tending in operation to stabilize the gyro platform in space, each gyroscope comprising a gyro frame, a gyro wheel carried by a gyro housing for rotation about a spin axis, the gyro housing being carried by the gyro frame for rotation about a precession axis; and

three releveling means associated with the three gyroscopes, respectively, for immediate releveling of the gyro platform when desired, each releveling means comprising camming means carried by the gyro housing for rotation with the gyro housing about the precession axis;

a projection means having a normal position out of the path of the camming means, and a relevel position in the path of rotation of the camming means, the projection means in the relevel position engaging the camming means and preventing the gyro housing from rotating, whereby simultaneous engagement of all of the camming means by the projection means prevents rotation of all of the gyro housings about their precession axes;

third bearing means supporting the gyro platform upon the instrument platform for rotation of the gyro platform along a rotational path extending about the second axis;

yoke means coupled to the hub shaft means and located outwardly of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and the gyro platform are rotatable about the first and second axes without engaging the yoke means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a third axis perpendicular to the first and second axes.

11. An apparatus according to claim 10 and including three erection motors for moving the three projection means into their relevel positions for engagement with the three camming means, respectively.

12. An apparatus according to claim 11 wherein each camming means includes camming surfaces for engagement by the associated projection means in any position of rotation of the camming means, whereby movement of the projection means toward its relevel position engages the projection means upon the camming surfaces and rotates the gyro housing about the precession axis until the projection means reaches its relevel position.

13. A gyroscopically stabilized apparatus for aiming a camera at a target object, the apparatus comprising:

hub shaft means disposed along a roll axis;

a camera platform for supporting a camera;

a hub assembly including first bearing means defining the roll axis and supporting the hub assembly upon the hub shaft means for rotation of the hub assembly about the roll axis, the hub assembly including second bearing means defining a tilt axis perpendicular to the roll axis and supporting the camera platform upon the hub assembly for rotation of the camera platform about the tilt axis;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

third bearing means supporting the gyro platform upon the camera platform for rotation of the gyro platform about the tilt axis;

a pair of hemispherical fairings in adjacent relation and surrounding the camera platform and the gyro platform;

yoke means located exteriorly of the pair of fairings, and coupled to the hub shaft means; and

support means coupled to the yoke means for supporting the hub assembly for rotation of the hub assembly about a pan axis perpendicular to the roll and tilt axes.

14. An apparatus according to claim 13 wherein the hub shaft means includes a pair of hub shafts having outer extremities, respectively, and the yoke means comprises a yoke having a half circle configuration, coupled at its midportion to the support means, and coupled at its opposite extremities to the opposite extremities of the pair of hub shafts.

15. An apparatus according to claim 13 wherein the hub shaft means includes a pair of hub shafts having outer extremities, respectively, and the yoke means comprises a yoke having a central portion having a half circle configuration and coupled at its midportion to the support means, the yoke further having opposite extremities oppositely horizontally offset, with the ends of the opposite extremities coupled to the opposite extremities of the pair of hub shafts.

16. An apparatus according to claim 13 wherein the hub shaft means includes a hub shaft having an outer extremity, and the yoke means comprises a yoke having a quarter circle configuration coupled at its opposite extremities to the support means and to the outer extremity of the hub shaft, respectively.

17. An apparatus according to claim 13 wherein one of the fairings is coupled to and movable with the camera platform, and the other one of the fairings is coupled to and movable with the gyro platform.

18. An apparatus according to claim 13 wherein one of the fairings is coupled to and movable with the camera platform, and the pair of fairings are coupled together for common rotation.

19. An apparatus according to claim 18 wherein the camera platform mounts a level balance motor operative to move a weight between a raised position and a lowered position for shifting downwardly the center of gravity of the fairings and the apparatus located interiorly of the fairings.

20. An apparatus according to claim 13 wherein the support means includes a support arm adapted for connection to a vehicle, and including vibration isolating and damping means interposed between the yoke means and the support arm exteriorly of the pair of fairings.

21. An apparatus according to claim 13 wherein the gyro platform mounts a gyro housing for rotation about a vertical axis, and wherein the gyro platform mounts a pan axis motor having a driving element operative to develop a driving torque tending to rotate the housing about the vertical axis whereby, upon stabilization of the gyro housing, the stabilized gyro housing resists the driving torque and instead the camera platform rotates about the pan axis.

22. An apparatus according to claim 13 wherein the camera platform mounts a driven element for rotation about the tilt axis, and wherein the gyro platform mounts a tilt axis motor having a driving element operative to develop a driving torque tending to rotate the camera platform about the tilt axis whereby, upon stabilization of the gyro housing, the stabilized gyro housing resists the driving torque and instead the camera platform rotates about the tilt axis.

23. An apparatus according to claim 13 wherein the gyro platform mounts a gyro housing for rotation about a vertical axis, and wherein the gyro platform mounts a driven element for rotation about the tilt axis, and wherein the camera platform mounts a tilt axis motor having a driving element operative to develop a driving torque tending to rotate the gyro platform about the tilt axis whereby, upon stabilization of the gyro housing, the stabilized gyro housing resists the driving torque and instead the camera platform rotates about the tilt axis.

24. An apparatus according to claim 13 and wherein each gyroscope comprises a gyro frame, a gyro wheel carried by a gyro housing for rotation about a spin axis, the gyro housing being carried by the gyro frame for rotation about a precession axis;

and three releveling means associated with the three gyroscopes, respectively, for immediate releveling of the gyro platform when desired, each releveling means comprising camming means carried by the gyro housing for rotation with the gyro housing about the precession axis;

a projection means having a normal position out of the path of the camming means, and a relevel position in the path of rotation of the camming means, the projection means in the relevel position engaging the camming means and preventing the gyro housing from rotating, whereby simultaneous engagement of all of the camming means by the projection means prevents rotation of all of the gyro housings about their precession axes.

25. An apparatus according to claim 24 and including three erection motors for moving the three projection means into their relevel positions for engagement with the three camming means, respectively.

26. An apparatus according to claim 25 wherein each detent means includes camming surfaces for engagement by the associated projection means in any position of rotation of the camming means, whereby movement of the projection means toward its relevel position engages the projection means upon the camming surfaces and rotates the gyro housing about the precession axis until the projection means reaches its relevel position.

27. An apparatus according to claim 13 wherein the gyro platform mounts a level balance motor operative to move a weight between a raised position and a lowered position for shifting downwardly the center of gravity of the fairings and the apparatus located interiorly of the fairings.

28. An apparatus according to claim 13 and including a camera mounted to the camera platform, and wherein one of the hemispherical fairings is a camera platform fairing which includes a camera window, the camera platform fairing being coupled to and movable with the camera platform whereby the camera and the camera window move in unison.

29. A gyroscopically stabilized apparatus for aiming an instrument at a target object, the apparatus comprising:

an instrument platform for supporting an instrument;

a gyro platform including a plurality of gyroscopes tending in operation to stabilize the gyro platform in space;

yoke means and hub means supporting the instrument platform and the gyro platform for rotation along rotational paths extending about a first axis, the hub means further supporting the instrument platform for rotation along a rotational path extending about a second axis perpendicular to the first axis, and the instrument platform further supporting the gyro platform for rotation along a rotational path extending about the second axis, the yoke means being located outwardly of all of the rotational paths of the instrument platform and the gyro platform whereby the instrument platform and gyro platform are freely rotatable about the first and second axes without striking the yoke means; and

support means coupled to the yoke means for supporting the yoke means and hub means for rotation about a third axis perpendicular to the first and second axes.

30. An apparatus according to claim 29 and including a spherical fairing means in surrounding relation to the instrument platform and the gyro platform, with the yoke means being located interiorly of the fairing means.

31. An apparatus according to claim 30 wherein the first, second and third axes intersect at a point located within the fairing.