Pin centered brake
AssigneeMcDonnell Douglas Corporation
InventorLouis T. Kramer
Life of this patent
Estimating the term…
Abstract
An aircraft brake which is circumferentially disposed about the aircraft axle and supported at two points symmetrical about a line perpendicular to a center line drawn through the aircraft axle. Clearance between the brake housing and the axle in the direction of the reacting couple to the braking load is essential in the geometry of mounting the brake to the shock strut and axle structure.
Claims10
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.
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.
Dependencies are inferred from the claim text.