IP Library Patent Application 10599291
Patent Application
App. No. 10/599,291

Aircraft Wheel Assembly

Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US None
App. No.
10/599,291
Abstract

An aircraft wheel assembly including an axle housing means for sensing wheel speed, one end of the axle being covered by a cap member ( 10 ), the cap member ( 10 ) comprising a generally cuplike body ( 16 ) having an end wall ( 14 ) towards the free end of the axle, the cap including means for driving the wheel speed sensing means, the side wall of the body having at least one stiffening deformation.

Claims (13)

1 - 12 . (canceled)

13 . An aircraft wheel assembly including an axle housing means for sensing wheel speed, one end of the axle being covered by a cap member, the cap member comprising a generally cup-like body having an end wall towards the free end of the axle and means for driving the wheel speed sensing means, the side wall of the body having at least one stiffening formation arranged to influence the flow of air around the exposed exterior of the cap member in flight whereby to reduce the level of noise generated.

14 . An assembly according to claim 13 , wherein at least one formation comprises a rib or fin on the side wall of the cup-like body.

15 . An assembly according to claim 13 , wherein at least one formation extends from the end wall to an open end of the cup-like body and increase in thickness towards the open end.

16 . An assembly according to claim 13 , wherein at least one formation is hollow.

17 . An assembly according to claim 13 , wherein there is a plurality of said surface formations and said formations are spaced substantially evenly about the cap member.

18 . An assembly according to claim 13 , wherein the cup-like body tapers radially outwardly away from the end wall.

19 . An assembly according to claim 13 , wherein the axle protrudes beyond a wheel rim of a wheel of the wheel assembly.

20 . An assembly according to claim 13 , wherein the assembly is a main wheel assembly incorporating tire pressure sensing means and the cap member includes means for mounting said tire pressure sensing means.

21 . An aircraft incorporating at least one wheel assembly according to claim 13 .

22 . A hubcap for an aircraft wheel assembly which has an axle housing means for sensing wheel speed and means for sensing tire pressure, the hub cap comprising a generally cup-like body having an end wall, the body having a mouth and a flange at said mouth for engagement with clamping means by which the hub cap is fixed on to a free end of the axle and a slot extending from the flange into the side wall of the body to receive components of the means for sensing tire pressure, the inner surface of the end wall having formations for engagement with the wheel speed sensing means, ribs being spaced about the exterior of the side wall of the body.

23 . A hubcap according to claim 22 , wherein said ribs are hollow.

24 . A hubcap according to claim 22 , wherein the side wall of the body flares radially outwardly from the end wall to the flange.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 4, 2008
From: FISHER, MARTIN JAMES
To: DUNLOP AEROSPACE LIMITED
Reel/Frame 021925/0253 →
CORRECTIVE NAME CHANGE. THE NAME CHANGE (PREVIOUSLY RECORDED AT REEL/FRAME 020794/0906 ON APRIL 15, 2008) USED AN INCORRECT EXECUTION DATE OF DECEMBER 9, 1997. THE CORRECT EXECUTION DATE SHOULD BE JANUARY 4, 2008. Recorded Nov 24, 2008
From: DUNLOP AEROSPACE LIMITED
To: MEGGITT AEROSPACE LIMITED
Reel/Frame 021876/0456 →
CHANGE OF NAME Recorded Apr 15, 2008
From: DUNLOP AEROSPACE LIMITED
To: MEGGITT AEROSPACE LIMITED
Reel/Frame 020794/0906 →