Pin centered brake

Claim 2

An improved multiple disc aircraft wheel brake circumferentially disposed in a complete annulus about an aircraft axle and having a brake housing attached to aircraft landing gear structure, a plurality of brake discs rotationally fixed to said housing while axially moveable, a plurality of wheel discs located alternately and adjacently to said brake discs and radially fixed to an aircraft wheel while axially moveable, means to axially engage the brake discs with the wheel discs, wherein the improvement comprises: attachment of said brake housing to said aircraft landing gear structure by only two pins attached to said landing gear structure and extending parallel to the axis of said axle, said two pins being located on a centerline coincident with the diameter of said axle and being symmetrical about a line drawn through the center of said aircraft axle and perpendicular to said centerline, said two pins slideably engaging mating apertures in said brake housing so that said two pins provide radial restraint while providing axial freedom for said brake housing, said brake housing unrestrained by said axle, and said wheel and said brake housing being retained on said axle in an axially stacked fashion by only a single fastener secured to said axle.

Claim 3

The aircraft brake attachment as set out in claim 1 wherein said aircraft wheel is mounted on bearings having an inner and outer race, said two pins are cylindrical pins in said aircraft structure engaging said mating apertures in said brake housing, said brake housing having a support point contacting said aircraft axle and engaging said aircraft wheel bearing inner race, said fastener retaining said wheels, said bearings, and said brake housing in said axially stacked fashion.

Claim 4

The aircraft brake attachment as set out in claim 2 wherein said fastener is a single nut threadably engaging said axle whereby to provide a true quick-change brake assembly.

Claim 5

The aircraft brake attachment as set out in claim 3 wherein one of said pins is mounted on a rotatable link pivotally connected to said aircraft structure whereby the distance between said two pins is adjustable.

Claim 6

The aircraft brake attachment as set out in claim 3 wherein one of said pins is provided with a pair of parallel flats with said flats oriented parallel to a line drawn between the centers of said two pins, a slotted spacer having a cylindrical outer surface and provided with an aperture having parallel flat sides joining cylindrical portions to match and engage said one of said pins, a clearance being provided between said cylindrical portions of said aperature and said one of said pins to accommodate tolerance in the spacing between said pins.

Claim 7

An aircraft wheel brake which is circumferentially disposed in a complete annulus about an aircraft axle attached to aircraft shock strut structure comprising: only two pins installed in said aircraft structure and protruding from said structure parallel to the axis of said axle, said two pins being located on a centerline coincident with the diameter of said axle and being symmetrical about a line drawn through the center of said aircraft axle and perpendicular to said centerline; a brake housing having two mating apertures to slideably engage said pins so as to provide radial restraint to braking torque while providing axial freedom for said brake housing, a clearance bore to clear said aircraft axle and a flange containing a bearing surface located near the end of said brake housing opposite said two apertures and engaging said axle; brake means located in said brake housing having at least two engaging brake elements, the first of which engages said brake housing and the second which engages an aircraft wheel; said wheel mounted on bearings, having an inner and outer race, on said aircraft axle, with said inner race bearing against said brake housing flange in a stacked arrangement; and said wheel, said wheel bearings, and said brake housing being retained on said axle in an axially stacked fashion by only a single fastener secured to said axle.

Claim 8

An aircraft wheel brake which is circumferentially disposed in a complete annulus about an aircraft axle attached to aircraft shock strut structure comprising: only two pins installed in said aircraft structure and protruding from said structure parallel to the axis of said axle, said two pins being located on a centerline coincident with the diameter of said axle and being symmetrical about a line drawn through the center of said aircraft axle and perpendicular to said centerline; a brake housing having two mating apertures to slideably engage said pins so as to provide radial restraint to braking torque while providing axial freedom for said brake housing, a clearance bore to clear said aircraft axle and a flange containing a bearing surface located near the end of said brake housing opposite said two apertures and engaging said axle; brake means located in said brake housing having at least two engaging brake elements, the first of which engages said brake housing and the second which engages an aircraft wheel; said wheel mounted on bearings, having an inner and outer race, on said aircraft axle, with said inner race bearing against said brake housing flange in a stacked arrangement; and said wheel, said wheel bearings, and said brake housing being retained on said axle in an axially stacked fashion by only a single fastener secured to said axle.

Claim 9

The aircraft wheel brake as set out in claim 6 wherein said brake housing flange is provided with a plurality of apertures so as to permit air to circulate through said brake.

Claim 10

The aircarft wheel brake as set out in claim 6 wherein one of said two pins is provided with means for adjustment to accommodate tolerances and differential expansion between said pins and said apertures in said brake housing.

Claim 11

The aircraft wheel brake as set out in claim 8 wherein said means for adjustment of one of said two pins is provided by mounting one of said pins to a rotatable link pivotally connected to said aircraft structure.

Claim 12

The aircraft wheel brake as set out in claim 8 wherein said fastener retaining said wheel and said brake to said axle is a threaded nut, engaging and locked to the outer end of said aircraft axle.