Ram air turbine lip seal sealing surface sleeve cap

Patent metadata

Field	Value
Publication number	US-9970526-B1
Application number	US-201514620603-A
Country	US
Kind code	B1
Filing date	Feb 12, 2015
Priority date	Feb 2, 2015
Publication date	May 15, 2018
Grant date	May 15, 2018

Abstract

Described herein is a system for increasing the robustness of a sealing surface and eliminating an expensive plating operation. The system includes an axially rotatable object comprising a first material that is subject to corrosion. The system also includes a radial shaft seal positioned radially outward from the axially rotatable object. The system also includes a sleeve coupled to the axially rotatable object, positioned between the axially rotatable object and the radial shaft seal and comprising a second material that is corrosion resistant.

First claim

What is claimed is:

1. A system for increasing robustness of a seal, comprising:
an axially rotatable object comprising a first material that is subject to corrosion;
a radial shaft seal positioned radially outward from the axially rotatable object; and
a sleeve coupled to the axially rotatable object, positioned between the axially rotatable object and the radial shaft seal and comprising a second material that is corrosion resistant,
wherein:
the radial shaft seal is located radially outward from the sleeve and contacts the sleeve to reduce the likelihood of fluid leakage, and
the axially rotatable object is a bevel gear of a ram air turbine and the sleeve is coupled to an aft end of the bevel gear and positioned between an aft bearing and the bevel gear.

2. The system of claim 1 , wherein the second material is a stainless steel alloy comprising between 0.9 and 1.35% aluminum, between 12.25 and 13.25% chromium, 76% iron, and 7.5 to 8.5% nickel by weight.

3. The system of claim 1 , wherein the sleeve rotates relative to the radial shaft seal.

4. The system of claim 1 , wherein the axially rotable object includes a gear of a gear set of the ram air turbine and the gear set is produced at a single location before being assembled on the ram air turbine.

5. The system of claim 1 , wherein the sleeve has an outer surface configured to contact the radial shaft seal that is ground to reduce surface irregularities of the outer surface.

6. The system of claim 5 , wherein the outer surface of the sleeve is ground after the sleeve is coupled to the axially rotatable object.

7. A system for increasing robustness of a seal, comprising:
an axially rotatable portion of a gear of a ram air turbine;
a radial shaft seal positioned radially outward from the axially rotatable portion of the gear; and
a sleeve coupled to the axially rotatable portion of the gear, positioned between the axially rotatable portion of the gear and the radial shaft seal and comprising a second material that is corrosion resistant,
wherein:
the radial shaft seal is located radially outward from the sleeve and contacts the sleeve to reduce the likelihood of fluid leakage, and
the axially rotatable portion of the gear is at least one of an aft end of a bevel gear or an end of a shaft of a pinion gear.

8. The system of claim 7 , wherein the second material is a stainless steel alloy comprising between 0.9 and 1.35% aluminum, between 12.25 and 13:25% chromium, 76% iron, and 7.5 to 8.5% nickel.

9. The system of claim 8 , wherein the second material is heat treated to at least 35 on the Rockwell C Scale.

10. The system of claim 7 , wherein the sleeve is press fit onto the axially rotatable portion of the gear.

11. The system of claim 7 , wherein an outer surface of the sleeve is ground after the sleeve is coupled to the axially rotatable portion of the gear.

12. A system for increasing robustness of a seal, comprising:
an axially rotatable object comprising a first material that is subject to corrosion;
a radial shaft seal positioned radially outward from the axially rotatable object; and
a sleeve coupled to the axially rotatable object, positioned between the axially rotatable object and the radial shaft seal and comprising a second material that is corrosion resistant,
wherein:
the radial shaft seal is located radially outward from the sleeve and contacts the sleeve to reduce the likelihood of fluid leakage, and
the axially rotatable object is a shaft of a pinion gear of a ram air turbine and the sleeve is coupled to a distal end of the shaft and configured to be held in position by a protrusion of the shaft.

13. The system of claim 12 , wherein the second material is a stainless steel alloy comprising between 0.9 and 1.35% aluminum, between 12.25 and 13.25% chromium, 76% iron, and 7.5 to 8.5% nickel by weight.

14. The system of claim 12 , wherein the sleeve rotates relative to the radial shaft seal.

15. The system of claim 12 , wherein the axially rotable object includes a gear of a gear set of the ram air turbine and the gear set is produced at a single location before being assembled on the ram air turbine.

16. The system of claim 12 , wherein the sleeve has an outer surface configured to contact the radial shaft seal that is ground to reduce surface irregularities of the outer surface.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Bortoli Stephen Michael
• Russ David Everett
• Konicek Timothy Scott

Classifications

• C22C38/40

  with nickel · CPC title

• C22C38/06

  containing aluminium · CPC title

• B64D41/007

  Ram air turbines · CPC title

• F16J15/3204 Primary

  with at least one lip · CPC title

• F16H57/038

  Gearboxes for accommodating bevel gears (F16H57/037 takes precedence) · CPC title