Aircraft actuator with no-back, load detent assembly
US-2017313409-A1 · Nov 2, 2017 · US
US8991359B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8991359-B2 |
| Application number | US-201113819576-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 2, 2011 |
| Priority date | Sep 3, 2010 |
| Publication date | Mar 31, 2015 |
| Grant date | Mar 31, 2015 |
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An intake camshaft device 1 includes an intake camshaft, a first rolling bearing and a second rolling bearing for rotatably supporting both end parts of the intake camshaft, and a first sliding bearing and a second sliding bearing for rotatably supporting the intake camshaft between the first and second rolling bearings. The first rolling bearing is arranged in a same plane as a rotation plane of a sprocket for an intake cam. In other words, the first rolling bearing is positioned in a plane which is overlapped with a plurality of teeth of the sprocket for the intake cam, and perpendicular to a center axis. The first sliding bearing is disposed adjacent to the first rolling bearing backward in an axial direction.
Opening claim text (preview).
The invention claimed is: 1. A camshaft device comprising: a camshaft including a shaft body, and a plurality of cams which are provided along an axial direction of the shaft body; a gear having a plurality of teeth, and mounted on the camshaft so as to rotate around a center axis of the camshaft; and a plurality of bearings rotatably supporting the camshaft, wherein a transmitting member transmitting driving power is wound around the gear, the bearings include a roiling b…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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