Blade Dovetail and Retention Apparatus
AssigneeGeneral Electric Company
InventorsNicholas Joseph Kray, Ian F. Prentice
Life of this patent
Estimating the term…
Loading patent…
AssigneeGeneral Electric Company
InventorsNicholas Joseph Kray, Ian F. Prentice
Estimating the term…
Methods, apparatus, systems, and articles of manufacture are disclosed to adjust a pitch axis of a blade of an engine. An example blade apparatus includes: a hub to facilitate movement of blades in an engine, the engine having a radial center line; and a trunnion connected to the hub. The example trunnion includes a slot to accommodate a first blade, and at least one of the trunnion or the first blade is positioned with at least one of a tilt or a lean with respect to the radial center line to form a pitch axis offset from the radial center line such that the pitch axis is not parallel to or co-linear with the radial center line. The example hub is to rotate the first blade about the pitch axis.
A blade apparatus comprising:
A rotor apparatus comprising:
A computer-implemented method to determine blade position to set a pitch axis relative to a radial engine axis, the method comprising:
Dependencies are inferred from the claim text.