Slip ring having a liquid metal contact between a stationary element and a rotatable element

Patent metadata

Field	Value
Publication number	US-9871334-B2
Application number	US-201715434739-A
Country	US
Kind code	B2
Filing date	Feb 16, 2017
Priority date	Feb 23, 2016
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

A slip ring assembly includes a stationary element, a rotatable element rotatable relative to the stationary element, and a liquid metal contact electrically coupling the rotatable element to the stationary element. The liquid metal contact includes a metallic material having a melting temperature that is less than zero degrees Celsius and a boiling temperature that is greater than four-hundred degrees Celsius to electrically couple an electrical device fixed relative to the rotatable element to an electrical device fixed relative to the stationary element through the liquid metal contact.

First claim

What is claimed is:

1. A slip ring assembly, comprising:
a stationary element;
a rotatable element rotatable relative to the stationary element; and
a liquid metal contact electrically coupling the rotatable element to the stationary element, wherein the liquid metal contact includes a metallic material that is a melting point that is below zero (0) degrees Celsius and a boiling point that is about four-hundred (400) degrees Celsius.

2. A slip ring assembly as recited in claim 1 , wherein the metallic material has a boiling temperature that is greater than about one-thousand (1000) degrees Celsius.

3. A slip ring assembly as recited in claim 1 , wherein the metallic material has an electrical conductivity that is greater than 3.0×10 6 siemens per meter at twenty (20) degrees Celsius.

4. A slip ring assembly as recited in claim 1 , wherein the metallic material includes a eutectic alloy comprising gallium, indium, and tin.

5. A slip ring assembly as recited in claim 1 , wherein the metallic alloy comprises 68% gallium by total weight, 22% indium by total weight, and 10% tin by total weight.

6. A slip ring assembly as recited in claim 1 , wherein the rotating element includes a rotor shaft defining a rotation axis, a bus bar radially outward from the rotor shaft, and a static mast circumferentially surrounding the bus bar and rotor shaft.

7. A slip ring assembly as recited in claim 1 , wherein the rotating element defines a rotation axis, and further including a ferrofluidic seal disposed between the rotatable element and the stationary element.

8. A slip ring assembly as recited in claim 1 , wherein the rotating element defines a gravity well extending about the stationary element.

9. A slip ring assembly as recited in claim 8 , wherein the gravity well extends radially outward and axially downward relative to the rotatable element.

10. A slip ring assembly as recited in claim 8 , wherein the stationary element includes a stationary annular contact extending radially outward from axially downward relative the rotatable element.

11. A slip ring assembly as recited in claim 1 , further including a dry seal disposed on a radially inner end of the liquid metal contact and hermetically sealing the metallic material of the liquid metal contact within the rotatable element.

12. A slip ring assembly as recited in claim 11 , wherein the dry seal includes an annular seal race extending about the stationary element with a polished stainless steel surface.

13. A slip ring assembly as recited in claim 12 , wherein the annular seal race defines a hermetic feed through, and further including a stationary annular contact extending through the hermetic feed through.

14. A slip ring assembly as recited in claim 11 , wherein the dry seal hermetically bounds a gravity well housing the metallic material.

15. A rotorcraft, comprising:
a rotor assembly rotatable about a rotation axis and having an electrical device;
a bus bar extending axially along the rotation axis; and
a slip ring assembly as recited in claim 1 coupling the electrical device to the electrical bus,
wherein the stationary element is connected to the electrical bus,
wherein the rotatable element is connected to the electrical device, and wherein the liquid metal contact electrically couples the electrical device to the electrical bus during rotation of the rotor assembly about the rotation axis.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Dempsey Patrick J
• Welsh William A
• Kellner Aaron

Classifications

• B64C27/04 Primary

  Helicopters · CPC title

• H01R39/646 Primary

  through an electrical conductive fluid · CPC title

• B64C27/32

  Rotors · CPC title

• B64D2221/00

  Electric power distribution systems onboard aircraft · CPC title