Cardan joint for inertially stabilizing a payload

Patent metadata

Field	Value
Publication number	US-11243082-B2
Application number	US-201916721662-A
Country	US
Kind code	B2
Filing date	Dec 19, 2019
Priority date	Dec 19, 2019
Publication date	Feb 8, 2022
Grant date	Feb 8, 2022

Abstract

A cardan joint includes a cross-elevation assembly comprising a cross-elevation housing, a roll-elevation assembly comprising a roll-elevation housing, a payload interface assembly comprising a payload interface housing, and a suspension interface yoke comprising a suspension interface that couples the suspension interface yoke to one or more suspension bars. The roll-elevation assembly is rotatably connected to the cross-elevation assembly along a first rotation axis via a radial roller bearing and a thrust roller bearing. The payload interface assembly is rotatably connected to the roll-elevation assembly along a second rotation axis via a radial roller bearing and a thrust roller bearing. The suspension interface yoke is rotatably connected to the cross-elevation assembly along a third rotation axis via one or more radial roller bearings and one or more thrust roller bearings. The payload interface housing comprises a payload interface operable to couple the payload interface housing to an inertially stabilized payload.

First claim

What is claimed is:

1. A cardan joint comprising:
a cross-elevation assembly comprising a cross-elevation housing;
a roll-elevation assembly comprising a roll-elevation housing, and rotatably connected to the cross-elevation assembly along a first rotation axis via one or more radial roller bearings and one or more thrust roller bearings supported between the cross-elevation housing and the roll-elevation housing;
a payload interface assembly comprising a payload interface housing, and rotatably connected to the roll-elevation assembly along a second rotation axis offset from the first rotation axis via one or more radial roller bearings and one or more thrust roller bearings supported between the roll-elevation housing and the payload interface housing; and
a suspension interface yoke comprising a suspension interface operable to couple the suspension interface yoke to one or more suspension bars, wherein the suspension interface yoke is rotatably connected to the cross-elevation assembly along a third rotation axis, offset from both the first rotation axis and the second rotation axis, via one or more radial roller bearings and one or more thrust roller bearings supported between the cross-elevation housing and the suspension interface yoke,
wherein the payload interface housing comprises a payload interface operable to couple the payload interface housing to an inertially stabilized payload.

2. The cardan joint of claim 1 , further comprising:
a pair of first axles along the first rotation axis that rotatably connect the roll-elevation housing to the cross-elevation housing;
a pair of second axles along the second rotation axis that rotatably connect the payload interface housing to the roll-elevation housing; and
a pair of third axles along the third rotation axis that rotatably connect the suspension interface yoke to the cross-elevation housing.

3. The cardan joint of claim 2 ,
wherein the pair of first axles are inserted through holes formed in the roll-elevation housing and into holes formed in the cross-elevation housing;
the pair of second axles are inserted through holes in the payload interface housing and into holes formed in the roll-elevation housing; and
the pair of third axles are inserted through holes formed in the suspension interface yoke and into holes formed in the cross-elevation housing.

4. The cardan joint of claim 2 ,
wherein the one or more radial roller bearings and the one or more thrust roller bearings supported between the cross-elevation housing and the fine elevation housing are supported on each of the pair of first axles;
the one or more radial roller bearings and the one or more thrust roller bearings supported between the roll-elevation housing and the payload interface housing are supported on each of the pair of second axles; and
the one or more radial roller bearings and the one or more thrust roller bearings supported between the cross-elevation housing and the suspension interface yoke are supported on each of the pair of third axles.

5. The cardan joint of claim 4 , wherein each of the plurality of radial roller bearings are needle radial roller bearings; and each of the plurality of thrust roller bearings are needle thrust roller bearings.

6. The cardan joint of claim 4 , wherein, on each of the pairs of first, second, and third axles, the one or more radial roller bearings are disposed closer to a center of the cardan joint than the one or more thrust roller bearings.

7. The cardan joint of claim 4 , further comprising:
a plurality of inner washers; and
a plurality of outer washers,
wherein, on each of the first, second, and third axles, at least one inner washer of the plurality of inner washers is disposed between the at least one radial roller bearing and the at least one thrust roller bearing, and at least one outer washer of the plurality of outer washers is disposed on a side of the thrust roller bearing that faces away from the inner washer.

8. The cardan joint of claim 1 ,
wherein, the first rotation axis is perpendicular to the second rotation axis and the third rotation axis,
the second rotation axis is perpendicular to the first rotation axis and the third rotation axis, and
the third rotation axis is perpendicular to the first rotation axis and the second rotation axis.

9. The cardan joint of claim 1 , wherein, the cross-elevation assembly, the roll-elevation assembly, and the payload interface assembly are substantially in plane with each other.

10. The cardan joint of claim 1 ,
wherein the roll-elevation housing is disposed around a perimeter of the cross-elevation housing,
the payload interface housing is disposed around a perimeter of the roll-elevation housing, and
the cross-elevation assembly, the roll-elevation assembly, and the payload interface assembly are at least partially surrounded by the suspension interface yoke.

11. The cardan joint of claim 1 further comprising:
an integral angle measurement system comprising a positioning target supported between the suspension interface yoke and at least one of the cross-elevation, the roll-elevation, or the payload interface housings, and a positional measuring sensor supported by the suspension interface yoke and positioned adjacent the positioning target,
wherein the integral angle measurement system operates to measure movement or positional displacement of the positioning target resulting from movement of the at least one of the cross-elevation, the roll-elevation, or the payload interface housings relative to the suspension interface yoke.

12. The cardan joint of claim 11 , wherein the integral angle measurement system further comprises a plurality of positioning targets supported between the suspension interface yoke and the at least one of the cross-elevation; the roll-elevation, or the payload interface housings.

13. The cardan joint of claim 12 , wherein the integral angle measurement system further comprises a plurality of positional measuring sensors supported by the suspension interface yoke, each positional measuring sensor being positioned adjacent at least one of the plurality of positioning targets.

14. The cardan joint of claim 13 ,
wherein at least two positioning targets of the plurality of positioning targets are supported between the suspension interface yoke and the at least one of the cross-elevation, the roll-elevation, or the payload interface housings at directions that are offset from each other, and
at least two positional measuring sensors of the plurality of positional measuring sensors are supported by the suspension interface yoke at positions adjacent the at least two positioning targets.

15. The cardan joint of claim 14 , wherein, the at least two positioning targets face in directions that are perpendicular to each other.

16. The cardan joint of claim 13 , wherein, the integral angle measurement system is a three-channel differential eddy current measurement bridge.

17. A system for inertially stabilizing a payload, comprising:
a support structure comprising one or more suspension bars;
a cardan joint rotatably coupled to the support structure via the one or more suspension bars;
a payload supported by the cardan joint, the cardan joint comprising:
a cross-elevation assembly having a cross-elevation housing;
a roll-elevation assembly comprising a roll-elevation housing, and rotatably connected to the cross-elevation assembly along a first rotation axis via one or more radial roller bearings and one or more thrust roller bearings supported between the cross-elevation housing and the fine ele

Assignees

• Raytheon Co

Inventors

• Miller Kirk A
• Lavine Jason R

Classifications

• G03B17/561 Primary

  Support related camera accessories · CPC title

• G01C21/18 Primary

  Stabilised platforms, e.g. by gyroscope · CPC title

• G01D11/30

  Supports specially adapted for an instrument; Supports specially adapted for a set of instruments · CPC title

• F16M13/022

  repositionable · CPC title

• F16M11/123

  the axis of rotation intersecting in a single point, e.g. by using gimbals · CPC title