Vibration damping gimbal sleeve for an aerial vehicle

Patent metadata

Field	Value
Publication number	US-10150576-B2
Application number	US-201615268147-A
Country	US
Kind code	B2
Filing date	Sep 16, 2016
Priority date	Sep 16, 2016
Publication date	Dec 11, 2018
Grant date	Dec 11, 2018

Abstract

A gimbal sleeve for connecting to a camera gimbal may float between a floor surface and a ceiling surface of an aerial vehicle chassis such that the gimbal sleeve has freedom of motion in yaw, pitch, and roll directions relative to the vehicle chassis. The gimbal sleeve may comprise a pair of connection points to the lower dampers on a floor surface of the vehicle chassis and a pair of connection points to upper dampers on a ceiling surface of the vehicle chassis. The connection points include spring forces that enable the gimbal sleeve to return to an equilibrium position in response to external vibrations and reduce the magnitude of vibrations transferred from the aerial vehicle to the gimbal and camera systems.

First claim

The invention claimed is:

1. An aerial vehicle with a floating gimbal connector, the aerial vehicle comprising:
a vehicle chassis comprising:
a floor surface comprising a pair of lower dampers;
a ceiling surface comprising a pair of upper dampers, the ceiling surface substantially parallel to the floor surface;

a gimbal sleeve at least partially extending into the vehicle chassis between the floor surface and the ceiling surface, the gimbal sleeve comprising:
a tube structured to couple with a gimbal connector, the tube comprising a substantially cylindrical shape, the tube having a longitudinal axis substantially parallel to the floor surface and the ceiling surface;
a pair of upper flanges extending in opposite directions from an outer surface of the cylindrical tube and aligned along an upper axis, the upper axis substantially perpendicular to the longitudinal axis of the tube and substantially parallel to the floor surface and the ceiling surface, and the upper axis offset in an upper direction from the longitudinal axis of the tube towards the ceiling surface;
a pair of lower flanges extending in opposite directions from the outer surface of the tube and aligned along a lower axis, the lower axis substantially perpendicular to the longitudinal axis of the tube and substantially parallel to the floor surface and the ceiling surface, the lower axis offset in a lower direction from the longitudinal axis of the tube towards the floor surface;
a pair of upper pins extending from the pair of upper flanges towards the floor surface and mating with the pair of lower dampers; and
a pair of lower pins extending from the pair of lower flanges towards the ceiling surface and mating with the pair of upper dampers;

a pair of upper springs around the pair of upper pins and the pair of lower dampers, the pair of upper springs applying a spring force between the pair of upper flanges and the floor surface; and
a pair of lower springs around the pair of lower pins and the pair of upper dampers, the pair of lower springs applying a spring force between the pair of lower flanges and the ceiling surface.

2. The aerial vehicle of claim 1 , wherein the pair of lower dampers and the pair of upper dampers each comprise a fluid-filled chamber to absorb motion of the respective upper and lower pins.

3. The aerial vehicle of claim 1 , wherein each of the upper and lower pins comprise a ball end that mates with a corresponding socket of respective lower and upper dampers, the ball end having rotational freedom of motion with the corresponding socket.

4. The aerial vehicle of claim 1 , wherein couplings between the upper and lower pins with respective lower and upper dampers are the only mechanical connections between the vehicle chassis and the gimbal sleeve.

5. The aerial vehicle of claim 1 , wherein the lower dampers are positioned near a front edge of the vehicle chassis and wherein the upper dampers are positioned behind the lower dampers.

6. The aerial vehicle of claim 1 , wherein the gimbal sleeve extends from a front edge of the vehicle, the gimbal sleeve to receive the gimbal connector of a mechanical gimbal structured to support a camera.

7. The aerial vehicle of claim 1 , wherein the gimbal sleeve further comprises:
an upper brace partially covering an upper portion of the tube, wherein the upper flanges extend from the upper brace.

8. The aerial vehicle of claim 1 , wherein the gimbal sleeve further comprises:
a lower brace having a tube portion partially extending into the tube, wherein the lower flanges extend from the lower brace.

9. The aerial vehicle of claim 8 , further comprising:
an upper brace partially covering an upper portion of the tube, wherein the upper flanges extend from the upper brace, wherein the upper brace is coupled to the lower brace.

10. The aerial vehicle of claim 1 , wherein the gimbal sleeve comprises a cantilever to support a weight of the gimbal.

11. A floating gimbal connector for connecting a gimbal to a mounting platform, the floating gimbal connector comprising:
a tube structured to couple with a gimbal connector, the tube comprising a substantially cylindrical shape, the tube having a longitudinal axis;
a pair of upper flanges extending in opposite directions from an outer surface of the tube and aligned along an upper axis, the upper axis substantially perpendicular to the longitudinal axis of the tube, and the upper axis offset in an upper direction from the longitudinal axis of the tube;
a pair of lower flanges extending in opposite directions from the outer surface of the cylindrical tube and aligned along a lower axis, the lower axis substantially perpendicular to the longitudinal axis of the cylindrical tube, the lower axis offset in a lower direction from the longitudinal axis of the tube;
a pair of upper pins extending downward from the pair of upper flanges;
a pair of lower dampers mating with the pair of upper pins;
a pair of lower pins extending upward from the pair of lower flanges;
a pair of upper dampers mating with the pair of lower pins;
a pair of upper springs around the pair of upper pins and the pair of lower dampers; and
a pair of lower springs around the pair of lower pins and the pair of upper dampers.

12. The floating gimbal connector of claim 11 , wherein the pair of lower dampers and the pair of upper dampers each comprise a fluid-filled chamber to absorb motion of the respective upper and lower pins.

13. The floating gimbal connector of claim 11 , further comprising:
an upper brace partially covering an upper portion of the tube, wherein the upper flanges extend from the upper brace.

14. The floating gimbal connector of claim 11 , further comprising:
a lower brace having a tube portion partially extending into the tube, wherein the lower flanges extend from the lower brace.

15. The floating gimbal connector of claim 14 , further comprising:
an upper brace partially covering an upper portion of the tube, wherein the upper flanges extend from the upper brace, wherein the upper brace is coupled to the lower brace.

16. The floating gimbal connector of claim 11 , wherein the pair of upper pins and the pair of lower pins each comprise a ball end that mates with a corresponding socket of respective lower and upper dampers, the ball end having rotational freedom of motion within the corresponding socket.

17. An aerial vehicle, comprising:
a floor surface comprising a pair of lower dampers;
a ceiling surface comprising a pair of upper dampers, the ceiling surface substantially parallel to the floor surface;
a gimbal sleeve at least partially between the floor surface and the ceiling surface, the gimbal sleeve comprising a mount connector to connector a gimbal, the gimbal sleeve floating between the floor surface and the ceiling surface such that the gimbal sleeve has freedom of motion in yaw, pitch, and roll directions relative to the floor surface and the ceiling surface, the gimbal sleeve comprising a pair of connection points to the lower dampers and a pair of connection points to the upper dampers; and
a gimbal connected to the mount connector of the gimbal sleeve.

18. The aerial vehicle of claim 17 , wherein the pair of connection points to the lower dampers and the pair of connection points to the upper dampers each comprise a pin having a ball end that mates with a corresponding socket of respective lower and upper dampers, the ball end having rotational freedom of motion within the corresponding socket.

19. The aerial vehicle of claim 17 , wherein th

Assignees

• Gopro Inc

Inventors

• Saika Noriaki
• Fruhauf Christopher Bramley
• Kennedy Daniel Francis

Classifications

• B64U2101/30

  for imaging, photography or videography · CPC title

• B64C1/06

  Frames; Stringers; Longerons {; Fuselage sections} · CPC title

• F16M11/06

  allowing pivoting · CPC title

• G03B15/006 Primary

  Apparatus mounted on flying objects · CPC title

• B64C2201/127

  Operations & Transport · mapped topic