Application of Richard Cleminson Cussons and Douglas Dewar

354 F.2d 384, 53 C.C.P.A. 836
CourtCourt of Customs and Patent Appeals
DecidedJanuary 13, 1966
DocketPatent Appeal 7494
StatusPublished
Cited by2 cases

This text of 354 F.2d 384 (Application of Richard Cleminson Cussons and Douglas Dewar) is published on Counsel Stack Legal Research, covering Court of Customs and Patent Appeals primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Application of Richard Cleminson Cussons and Douglas Dewar, 354 F.2d 384, 53 C.C.P.A. 836 (ccpa 1966).

Opinions

MARTIN, Judge.

This appeal is from the decision of the Board of Appeals affirming the examiner’s rejection of claims 7 through 11 and 13 of appellants’ application serial No. 39,664, filed June 29, 1960, for Cooling Means for Wheel and Brake Assembly. The rejection of two other claims was reversed by the board.

The sole issue is obviousness over the prior art under 35 U.S.C. § 103.

Appellants’ invention relates to an assembly of a wheel with a disc brake for aircraft landing gear. In order to dis[385]*385sipate the heat produced in the brake on landing of the aircraft, appellants provide an electric motor driven fan arranged to draw cooling air through the assembly.

The construction embodies a wheel rim having a centrally-located radial flange member which is rotatably supported by means of bearings on a hollow axle. The axle in turn is fixedly secured to the leg of the landing gear. Such construction results in an annular space being defined between the wheel rim and the axle at each side of the central flange. The disc brake is located in the inner of those annular spaces, that is, the one adjacent the leg of the landing gear. It comprises a plurality of annular rotor discs mounted to slide axially on splines on the inner surface of the wheel rim interleaved with annular stator disc. mounted with splines on an annular torque member secured to the axle. Operation of the brake is through a fluid pressure cylinder which forces the assembly of. rotor and stator discs into frictional engagement against an annular backing plate.

The annular space accommodating the brake structure is open to the atmosphere at its inner end. Openings are provided in the rim flange communicating with the interior of a tubular shield disposed about the axle in the other or outer annular space. That shield is of conical configuration having its smaller end at the outer end of the assembly to provide an annular passage about the axle, which passage is open to the atmosphere at that end of the assembly. Within the hollow axle is an electric motor operative to drive a fan having blades extending radially across the annular passage between the shield and the axle. Operation of the motor, which may be initiated either automatically or manually upon landing of the aircraft, draws air into the annular space at the inner end of the rim with the brake structure therein, through the openings in the central flange, through the annular passage within the shield, and finally out of the outer end of the latter passage.

Claims 7 and 9, which are representative, read:

7. An aircraft landing gear which comprises a non-rotatable axle, a wheel rim rotatably mounted on said axle and enclosing an axially extending passage located about said axle, a disc brake assembly in said passage, a fan positioned at one end of said passage to pass an axially directed current of cooling air through said passage and an electric driving motor for said fan.
9. An aircraft landing gear which comprises a non-rotatable hollow axle, a wheel rim rotatably supported on said axle and spaced concentrically from the axle to form an open ended axially extending annular passage, a disc brake mounted in said passage and connected to said axle and said rim to provide passages for air axially of said passage, a motor in said axle operable independently of said wheel and a fan driven by said motor and having blades extending radially across said annular passage to pass an axially directed flow of cooling air through said passage and about said brake assembly.

The appealed claims stand rejected on the combination of the following patents:

Griswold 2,922,495 January 26, 1960

White 2,959,255 November 8, 1960

Griswold also relates to a wheel and disc brake assembly for aircraft landing gear. That construction includes a fixed hollow hub having plate-like annular extensions at its inner and outer ends to form an axle.1 The wheel rim is rotatably mounted on those extensions near its inner and outer ends, providing an annular space between it and the hub with its extensions for receiving the friction discs of the brake. The inner of the annular extensions of the axle, that is, the one at the end of the axle secured to a leg of the landing gear, is provided with a [386]*386plurality of circumferentially spaced openings, “whereby cooling air is free to circulate through * * * [those] openings * * * into the area of the friction discs.” In addition, the central hub portion of the axle is provided with circumferential spaced openings providing communication between the annular passage where the brake is located and the hollow interior of the axle with the latter communicating through a central opening in the outer end with the atmosphere. That opening is disclosed as permitting ingress of air into the axle from whence it may also pass upwardly through the circumferential openings into the area of the brake discs to cool the same. Gris-wold does not disclose the use of a fan for providing forced air circulation.

The White patent relates to an arrangement for cooling a conventional drum type brake for a motor vehicle wheel by flowing air over the braking elements. The brake comprises a brake drum rotatable with the wheel and a stationary backing plate which together form a housing for conventional brake elements including brake shoes. The cooling arrangement involves a port in the backing plate near the drum surface, a fan in the port for blowing air into the brake housing and an opposing exhaust port in the brake drum for the exit of cooling air after it passes over the braking elements. The fan is driven through a driving wheel which expands into contact with the flange of the brake drum to be driven thereby upon a predetermined temperature being reached due to the heat generated by braking action. The patent states that the fan need not be driven from the brake drum and that any number of fans and exhausts may be used.

The appealed claims were held unpatentable over Griswold in view of White. The board observed that Gris-wold shows an axially extending passage with a disc brake therein and stated that air is free to pass through openings into the passage to cool the brake discs. It regarded the use of a fan to force circulation of cooling air through the brake of White as making it obvious to one skilled in the art to use a fan for a similar purpose in the basic reference, and stated that such a fan could just as well be placed in the hub cavity of Griswold as at the end of the axial passage. It was also the board’s view that it would be obvious to operate the fan through an independently driven motor, such as an electric or hydraulic motor, instead of from the brake drum.

So far as claims 7 and 8 are concerned, we find no error in the decision of the board. White’s disclosure of use of a fan for forcing cooling air through a vehicle brake would certainly suggest to one skilled in the art that a fan be employed to improve the air cooling of Gris-wold’s disc brake. We also think that such person would find it obvious that an independently powered motor, such as an electric motor, could be used.

In making the suggested modification, it would be obvious to position the fan within the hub or axle of Griswold adjacent the central opening at the outer end thereof with blades of the fan projecting radially at said opening.

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Related

Endevco Corporation v. Chicago Dynamic Industries, Inc.
268 F. Supp. 640 (N.D. Illinois, 1967)
Application of Richard Cleminson Cussons and Douglas Dewar
354 F.2d 384 (Customs and Patent Appeals, 1966)

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354 F.2d 384, 53 C.C.P.A. 836, Counsel Stack Legal Research, https://law.counselstack.com/opinion/application-of-richard-cleminson-cussons-and-douglas-dewar-ccpa-1966.