Oval O-ring groove for aircraft wheels

Patent metadata

Field	Value
Publication number	US-10144245-B2
Application number	US-201514939340-A
Country	US
Kind code	B2
Filing date	Nov 12, 2015
Priority date	Nov 12, 2015
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

Systems and apparatus for an oval O-ring groove for aircraft wheels may generally comprise an inboard wheel portion and an inboard O-ring groove. The inboard wheel portion may include an inboard rim located opposite of an inboard tubewell. The inboard tubewell may have an inboard mating surface located on an axially outward edge of the inboard tubewell. The inboard O-ring groove may be formed as a partial oval-shaped recess located on an outer edge of the inboard mating surface.

First claim

The invention claimed is:

1. A wheel for an aircraft, comprising:
an inboard wheel portion having an inboard rim located opposite of an inboard tubewell, the inboard tubewell comprising an inboard mating surface;
an outboard wheel portion comprising an outboard register on an outer an outer edge of an outboard mating surface, wherein the outboard register comprises a recess at a radially inner surface;
an inboard O-ring groove defining an inboard recess on an outer edge of the inboard mating surface, wherein the inboard O-ring groove and outboard register recess comprise partially oval shapes in order to increase a thickness between an inboard tubewell radius of the inboard tubewell and the O-ring groove.

2. The wheel of claim 1 , wherein the outboard wheel portion comprises an outer rim located opposite of an outboard tubewell, the outboard tubewell comprising the outboard mating surface, wherein the outboard wheel portion is configured to removably couple to the inboard wheel portion.

3. The wheel of claim 1 , wherein the outboard register is configured to align with the inboard O-ring groove in response to the outboard wheel portion being coupled to the inboard wheel portion.

4. The wheel of claim 3 , further comprising an O-ring located between the inboard O-ring groove and the outboard register.

5. The wheel of claim 1 , wherein a radius of the inboard recess of the inboard O-ring groove is in a 1:1 ratio to a radius of the outboard recess of the outboard register.

6. An aircraft wheel, comprising:
an inboard wheel portion having an inboard rim located opposite of an inboard tubewell, the inboard tubewell having an inboard mating surface on the inboard tubewell;
an at least one inboard O-ring groove formed as a recess located on an outer edge of the inboard mating surface;
an outboard wheel portion having an outboard rim located opposite of an outboard tubewell, the outboard tubewell having an outboard mating surface on the outboard tubewell, wherein the outboard mating surface is configured to removably couple to the inboard mating surface; and
an at least one outboard register comprising a recess at a radially inner surface, the outboard register protruding axially beyond the outboard mating surface;
wherein the at least one inboard O-ring groove and recess of the outboard register comprise a partially oval shape in order to increase a thickness between an inboard tubewell radius of the inboard tubewell and the O-ring groove.

7. The aircraft wheel of claim 6 , wherein the at least one inboard O-ring groove and the at least one outboard register substantially align when the inboard mating surface is coupled to the outboard mating surface.

8. The aircraft wheel of claim 6 , further comprising an at least one O-ring located between the at least one inboard O-ring groove and the at least one outboard register.

9. The aircraft wheel of claim 6 , wherein a radius of the recess of the at least one inboard O-ring groove is in a 1:1 ratio to a radius of the recess of the at least one outboard register.

10. A wheel assembly, comprising:
an inboard wheel portion having an outer rim located opposite of an inboard tubewell, the inboard tubewell having an inboard mating surface on the inboard tubewell;
an inboard O-ring groove located on an outer edge of the inboard mating surface;
an outboard wheel portion having an outer rim located opposite of an outboard tubewell, the outboard tubewell having an outboard mating surface on the outboard tubewell, wherein the outboard mating surface is configured to removably couple to the inboard mating surface; and
an outboard register comprising a recess at a radially inner surface, the outboard register protruding axially beyond the outboard mating surface;
wherein the inboard O-ring groove and recess of the outboard register comprise a partially oval shape in order to increase a thickness between an inboard tubewell radius of the inboard tubewell and the O-ring groove.

11. The wheel assembly of claim 10 , wherein the inboard O-ring groove and the outboard register align when the inboard mating surface is removably coupled to the outboard mating surface.

12. The wheel assembly of claim 11 , further comprising an O-ring located between the inboard O-ring groove and the outboard register.

Assignees

• Goodrich Corp

Inventors

• Stevenson John

Classifications

• B60B3/087

  Discs having several mutual contact regions · CPC title

• B60B25/22

  Other apurtenances, e.g. for sealing the component parts enabling the use of tubeless tyres · CPC title

• B64C25/36

  Arrangements or adaptations of wheels, tyres or axles in general · CPC title

• B60B25/006

  Rims split symmetrically · CPC title

• B60B2900/325

  Reliability · CPC title