US4029434A — Variable pitch mounting for airfoil blades of a w…

Claim 1

Independent Claim 313 words

An airfoil blade mounting comprising a hub rotatable about an axis, two co-axially disposed and spaced-apart sleeve bearings supported on said hub and having a common axis disposed offset from the axis of rotation of said hub and at an angle to the plane of rotation of said hub, an airfoil blade having two cylindrical portions at one end thereof and with said portions being respectively rotatably disposed in said sleeve bearings for rotation of said blade about its longitudinal axis for changing the pitch of said blade, said blade extending from said hub to the other end of said blade and with said blade being hollow along its length and terminating in a terminal end portion disposed away from said hub, said one end of said blade having two spaced-apart and mutually facing thrust surfaces disposed transverse to the longitudinal axis of said blade and in respective abutting relationship with said hub and in restrictive movement relative to said hub and along said longitudinal axis, a tension member extending through the hollow of said blade and having one end thereof connected with said terminal end portion of said blade and with the other end of said tension member being anchored with said hub for supporting said blade against centrifugal force acting on said blade in the rotation of said blade and said hub about the axis of said hub and permitting the changes in pitch of said blade, and a spring operatively interconnected between said tension member and said hub and arranged to create a tensile force in said tension member to yieldingly restrain said blade against the influence of centrifugal force and thereby for yieldingly urging the radially inner one of said blade thrust surfaces away from abutting relationship with said hub, for rendering said blade free to rotate about its longitudinal axis in the changes in pitch of said blade.

Claim 2

Dependent Claim 313 words

An airfoil blade mounting comprising a hub rotatable about an axis, two co-axially disposed and spaced-apart sleeve bearings supported on said hub and having a common axis disposed offset from the axis of rotation of said hub and at an angle to the plane of rotation of said hub, an airfoil blade having two cylindrical portions at one end thereof and with said portions being respectively rotatably disposed in said sleeve bearings for rotation of said blade about its longitudinal axis for changing the pitch of said blade, said blade extending from said hub to the other end of said blade and with said blade being hollow along its length and terminating in a terminal end portion disposed away from said hub, said one end of said blade having two spaced-apart and mutually facing thrust surfaces disposed transverse to the longitudinal axis of said blade and in respective abutting relationship with said hub and in restrictive movement relative to said hub and along said longitudinal axis, a tension member extending through the hollow of said blade and having one end thereof connected with said terminal end portion of said blade and with the other end of said tension member being anchored with said hub for supporting said blade against centrifugal force acting on said blade in the rotation of said blade and said hub about the axis of said hub and permitting the changes in pitch of said blade, and a spring operatively interconnected between said tension member and said hub and arranged to create a tensile force in said tension member to yieldingly restrain said blade against the influence of centrifugal force and thereby for yieldingly urging the radially inner one of said blade thrust surfaces away from abutting relationship with said hub, for rendering said blade free to rotate about its longitudinal axis in the changes in pitch of said blade.

Claim 3

Dependent Claim 45 words

The airfoil blade mounting as claimed in claim 1, including blade pitch means operatively associated with said hub and said blade for inducing selective pitch in said blade, and with said tension member being capable of twisting for accommodating the pitch adjustment of said blade.

Claim 4

Dependent Claim 86 words

The airfoil blade mounting as claimed in claim 2, wherein said blade pitch means includes an automatically operative governor element mounted on said hub and responsive to the speed or rotation of said hub and being capable of changing the pitch of said blade in response to changes in speed of rotation and within a selected speed range within which aerodynamic forces developed by said blade are transmitted to said hub mainly by said tension member rather than by forces on said bearing supporting said blade.

Claim 5

Dependent Claim 52 words

The airfoil blade mounting as claimed in claim 1, wherein said blade thrust surfaces are at disposed adjacent respective opposite ends of one of said bearings, and said thrust surfaces being slightly spaced from said bearing and arranged to allow longitudinal movement of said blade along the rotation axis of said bearings.

Claim 6

Dependent Claim 126 words

The airfoil blade mounting as claimed in claim 1, wherein there is a multiple of at least two of said blades and said bearings and said tension members, and with said blades being mounted in a pair arranged in opposed axial positions on said hub to have the longitudinal axis of each of said blades offset an equal distance from the rotation axis of said hub and with said blades thereby being disposed at an angle relative to the plane of rotation of said hub such that the thrust of said blades relative to said hub and which results from the aerodynamic forces on said blades is a component of the centrifugal force on said blades and is transmitted to said hub by said tension members.

Claim 7

Dependent Claim 84 words

The airfoil blade mounting as claimed in claim 5, wherein said bearings are symmetrically supported on said hub, and a lever system in said hub and said tension members being anchored with said lever system and capable of transmitting the forces to each other of said tension members and through said lever system, and springs operative between said hub and said lever system to hold said blades at equal radial positions within a predetermined axial float provided by said bearings locating each said blade.

Annuity Stage	Window Opens	Payment Deadline	Surcharge Period Until	Estimated Fee	Status
3.5 Years (Year 4)	1980-06-13	1980-12-13	1981-06-14	$2000.00	Window Closed / Lapsed
7.5 Years (Year 8)	1984-06-13	1984-12-13	1985-06-14	$3760.00	Window Closed / Lapsed
11.5 Years (Year 12)	1988-06-13	1988-12-13	1989-06-14	$7700.00	Window Closed / Lapsed

Variable pitch mounting for airfoil blades of a windmill or propeller

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