Patent ID: 8444324

Claim:
A wheel bearing for an aircraft landing gear, comprising: a rim, which is mounted rotatably about an axis via a bearing arrangement, haying two anti-friction bearings; a bearing outer housing which is designed as a single piece part, and outer running surfaces of the anti-friction bearings are directly formed on the bearing outer housing; and two inner rings on which the two anti-friction bearings respectively roll, the inner rings configured to be mounted on an axle and clamped in series between an axle nut and a shoulder, the two anti-friction bearings each comprising tapered rollers, wherein an integral component of the hearing outer housing forms a part of the rim, and the hearing outer housing is connected releasably to a rest of the rim, the bearing outer housing having a radially outwardly extending projection that has a radially outer circumferential surface disposed so that the circumferential surface is in an interior of a tire that is finable onto the rim.