Sealed rotary joint for turret rotator

• US 7,090,178 B2
• Filed: 08/10/2004
• Issued: 08/15/2006
• Est. Priority Date: 08/10/2004
• Status: Active Grant

• Current Assignee: Teledyne FLIR LLC (Teledyne Technologies Incorporated)
• Original Assignee: FLIR Systems, Inc. (Teledyne Technologies Incorporated)
• Inventors: Hughes, Michael R., Sommer, Thomas M., Rosi, Ronald J.
• Primary Examiner(s): Friedman, Carl D.
• Assistant Examiner(s): EPPS, TODD MICHAEL
• Application Number:
  US10/915,503
• Publication Number:
  US 20060033288A1
• Time in Patent Office: 735 Days
• Field of Search: 248/187.1, 248/177.1, 277/412, 277/411, 454/29
• US Class Current: 248/187.1
• CPC Class Codes: F16J 15/43 kept in sealing position by magnetic force
• CPC Class Codes: F16J 15/4476 with radial path
• CPC Class Codes: F16M 11/10 around a horizontal axis F16M11/12 takes precedence
• CPC Class Codes: F16M 11/2014 around a vertical axis F16M11/2035 takes precedence

Abstract

A rotatable payload support turret for operation in a potentially hazardous environment includes a fixed element attached to a vehicle or fixed structure and a rotatable element, supported for rotation with respect to the fixed element. The turret includes a camera payload having a pointing direction configured to be upwardly pointing. An annular clearance gap formed between the fixed element and the rotatable element is sealed by a conventional gas tight magnetic fluid seal element. A wiper seal is also provided in the clearance gap between the location of the magnetic fluid and the external environment to prevent breakdown of the magnetic fluid by elements of the potentially hazardous environment. The clearance gap may also form a labyrinth seal having up to three legs that are oriented to oppose a gravitational force direction. In addition, the fixed element may include a fluid repelling feature for repelling streams of incoming fluids thereby deflecting elements of the potentially hazardous environment away from an outer opening of the clearance gap.

Claims

1. A rotatable payload support turret for operation in a potentially hazardous environment, the support turret comprising a fixed element and a rotatable element, supported by the fixed element, for rotation with respect thereto, comprising:

an annular rotary seal attached to the fixed element in an annular clearance gap formed between said fixed element and said rotatable element, said annular rotary seal comprising a magnetic circuit formed to capture a magnetic fluid in the annular clearance gap thereby sealing the clearance gap with a gas tight seal; and

,

an annular wiper seal assembly positioned in said annular clearance gap between said potentially hazardous environment and said annular rotary seal for sealing the clearance gap to prevent elements of said potentially hazardous environment from contaminating said magnetic fluid, the annular wiper seal comprising;

an annular flexible member attached to the rotatable element for rotation therewith, and an annular sealing surface attached to said fixed element, said annular flexible member being forced into contact with said annular sealing surface during rotation of said rotatable element.

2. The rotatable payload support turret of claim 1 wherein each of said fixed element and said rotatable element are configured with opposing surfaces for forming said clearance gap there between, and further wherein said opposing surfaces are configured to form a labyrinth seal comprising at least one leg of the clearance gap formed to resist infiltration of said potentially harmful elements.

3. The rotatable payload support turret of claim 2 wherein said opposing surfaces are configured to form the labyrinth seal with three legs of the clearance gap formed to resist infiltration of said potentially harmful elements.

4. The rotatable payload support turret of claim 1 wherein the clearance gap includes an annular outer opening formed between opposing surfaces of the fixed element and the rotatable element and further wherein said fixed element is configured with a surface sloping downwardly toward said annular opening for draining potentially hazardous elements from the clearance gap.

5. The rotatable payload support turret of claim 1 wherein the clearance gap includes an annular outer opening formed between opposing surfaces of the fixed element and the rotatable element and further wherein said fixed element is configured with an annular fluid repelling feature positioned adjacent to said annular opening for repelling an incoming fluid stream away from the annular outer opening.

6. The rotatable payload support turret of claim 5 wherein the fluid repelling feature comprises an annular recess formed by opposing surfaces of the fixed element, the annular recess having an radially outward facing open end and a radially inward facing closed end, said inward facing closed end being formed by a radius between the opposing surfaces, and wherein the outward facing open end is positioned adjacent to said clearance gap annular outer opening.

7. The rotatable payload support turret of claim 1 wherein said fixed element comprises an azimuth housing having an internal cavity formed therein and wherein said rotatable element comprises a yoke for supporting the payload for rotation about an elevation axis, said yoke including a shaft extending from a bottom end thereof for mating with rotary bearings installed in the azimuth housing further comprising:

a cascade hood attached to the yoke and rotatable therewith, the cascade hood including an annular cover portion extending radially outward from the shaft and overhanging upward facing surfaces of the azimuth housing for protecting an annular clearance gap formed between the azimuth housing and the cascade hood from downwardly directed elements of the potentially hazardous environment.

8. The rotatable payload support turret of claim 7 wherein the cascade hood further comprises a first annular lip extending substantially vertically downward from a radially distal end of the annular cover portion to oppose a circumferential surface of the azimuth housing thereby forming an annular opening of the annular clearance gap.

9. The rotatable payload support turret of claim 8 wherein the cascade hood further comprises a second annular lip positioned radially inward from the first annular lip, said second annular lip having surfaces opposed to a substantially vertical surface of the azimuth housing for forming a leg of the clearance gap that is formed to resist infiltration of said potentially harmful elements.

10. The rotatable payload support turret of claim 9 wherein the azimuth housing includes a substantially upwardly extending third annular lip positioned radially between the first annular lip and the second annular lip, said third annular lip including a plurality of surfaces formed opposed to surfaces of an underside of the annular cover portion and to surfaces of said first annular lip and said second annular lip for defining the shape and dimension of the clearance gap and particularly for forming two additional legs of the clearance gap that are formed to resist infiltration of said potentially harmful elements.

11. The rotatable payload support turret of claim 9 wherein the third annular lip is formed with a plurality of drain openings passing therethrough for draining portions of the clearance gap that are radially inward of said third annular lip.