Composite spar structure having integral fitting for rotational hub mounting
AssigneeStructural Composite Industries, Inc.
InventorsOscar Weingart, Edgar E. Morris
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AssigneeStructural Composite Industries, Inc.
InventorsOscar Weingart, Edgar E. Morris
Estimating the term…
Hollow filament wound spar structure is provided adapted for rotational hub mounting under centrifugal and bending loads. The structure comprises an integrally wound, filament and resin composite spar of a predetermined wall thickness, a fitting integrally wound therein, the fitting defining rotational hub fastening means and comprising a plug having a mechanical engagement groove circumferentially of its longitudinal axis into which the opposing spar wall portion is deflected responsive to winding fabrication of the spar wall on the fitting. Belt means additionally are provided opposite the groove locally peripherally confining the deflected spar wall portion in mechanical engagement reinforcing relation, against relative dislodgement of the spar wall portion from the plug groove in the mounted condition of the spar structure, under centrifugal and bending loads.
A hollow, filament wound spar structure adapted for rotational hub mounting under centrifugal and bending loads, said structure comprising an integrally wound, filament and resin composite spar of a predetermined wall thickness, a fitting integrally wound therein, said fitting defining rotational hub fastening means and comprising a plug having mechanical engagement groove and land means circumferentially of the longitudinal axis to the surface contour of which the opposing spar wall portion conforms responsive to winding fabrication of the spar wall on said fitting, and separately formed belt means opposite said groove and land means locally peripherally confining said conformed spar wall portion and the axially adjacent spar wall portion in said groove means and against said plug respectively in mechanical engagement reinforcing relation against relative dislodgement of said spar wall portion in the mounted condition of the spar structure, under centrifugal and bending loads.
A hollow, filament wound spar structure adapted for rotational hub mounting under centrifugal and bending loads, said structure comprising an integrally wound, filament and resin composite spar of a predetermined wall thickness, a fitting integrally wound therein, said fitting defining rotational hub fastening means and comprising a plug having axially spaced mechanical engagement grooves circumferentially of the longitudinal axis into which the opposing spar wall portion is deflected responsive to winding fabrication of the spar wall on said fitting, and first and second belt means respectively opposite said first and second grooves and locally peripherally confining respective deflected spar wall portions in mechanical engagement reinforcing relation against relative dislodgement of said spar wall from said plug in the mounted condition of the spar structure, under centrifugal and bending loads, said first belt means defining a torus of a first greater diameter coplanar and coaxial with and radially beyond said first groove, and said second belt means defining a torus of a second lesser diameter coplanar and coaxial with with and radially beyond said second groove, said first belt torus having an axially continued extent encircling said second belt means torus in confining relation.
A hollow, longitudinally extended blade-shaped spar structure adapted for mounting on a wind turbine rotational hub for wind responsive movement under centriugal and bending loads, said structure comprising an integrally wound predominantly longitudinally disposed glass filament and thermosetting resin composite cross-sectionally D-shaped spar of a predetermined wall thickness pattern and having a circular inner terminus, and integral therewith a glass and resin afterbody defining with said spar a blade shape;
Dependencies are inferred from the claim text.