Rotor for rotating wing type aircraft

• US 3,967,918 A
• Filed: 05/10/1974
• Issued: 07/06/1976
• Est. Priority Date: 05/10/1973
• Status: Expired due to Term

• Current Assignee: Aerospatiale Societe Nationale Industrielle
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Mao, Daniel, Hancart, Michel Aime, Coffy, Rene Louis, Mouille, Rene Louis
• Primary Examiner(s): Powell, Jr., Everette A.
• Application Number:
  US05/469,045
• Time in Patent Office: 788 Days
• Field of Search: 416/134, 416/135, 416/138, 416/140, 416/141, 416/134 A, 416/139, 416/136, 416/244, 416/241 A
• US Class Current: 416/141
• CPC Class Codes: B64C 27/35 having elastomeric joints

Abstract

An improved rotor for a helicopter comprises a yoke at the inner end of each arm engaging the rotor hub by way of a spherical abutment.

Claims

1. A rotor for a rotating-wing craft comprising a driving shaft, a flat star-shaped rotor hub made of resin-reinforced glass fibres and substantially extending in a plane perpendicular to said driving shaft, said rotor having a central part adapted for being secured to the end of said driving shaft and a plurality of flat arms extending each from said hub central part substantially along a radial axis in said plane, said hub central part and flat arms having, in the direction perpendicular to said plane, respective thickness of substantially different values so that said central part is rigid and said flat arms are flexible in said direction, a same plurality of rotor blades having each a root part, disposed in closed relationship to the outer end of one of said hub arms, each rotor blade extending from its root part substantially along said radial axis, first and second means for connecting the root part of each rotor blade to said hub central part and to the outer end of said hub arm respectively, said first and second connecting means being adapted for permitting resiliently limited rotations and sliding displacement of said blade root part around and along said radial axis in relation to said hub central part and arm, and said first connecting means being further adapted for transmitting centrifugal radial forces from said rotor blade directly to said rigid hub central part, whereby flapping movements of the rotor blades in said direction are permitted by the flexible hub flat arms and said connecting means.

2. A rotor according to claim 1, wherein a same plurality of apertures having each an inside edge and an outside edge is arranged in said hub central part substantially on the respective radial axes of said hub arms, and said first connecting means comprises for each rotor blade a yoke having an end part connected to the root part of the respective blade and two arms extending from said end part along the radial axis of the respective hub arm to the central part aperture on said radial axis, said yoke arms passing at a distance from the two faces of said hub flat arm respectively, and a spherical abutment having an elastically deformable member inserted between the inner ends of said yoke arms and the outside edge of said aperture.

3. A rotor according to claim 2, wherein a cylindrical spigot is formed in the outer end of each hub arm, said spigot extending along the radial axis of said hub arm, and said second connecting means comprises a ball swivel mounted in said yoke end part, between the outer ends of said yoke arms, said ball swivel comprising a spherical bearing and a ball having a cylindrical recess extending all along a diameter thereof, said ball being mounted to freely rotate, in said spherical bearing and said hub arm end spigot being engaged in said ball recess to freely rotate therein.

4. A rotor according to claim 3, wherein said yoke end part consists of two parallel rigid metal plates extending substantially in planes parallel to the plane of the flat rotor hub, from the respective outer ends of said yoke arms to the respective blade root part, to which the outer ends of said rigid plates are connected, and said ball swivel is inserted between said rigid plates with the interposition of visco-elastic damping means.

5. A rotor according to claim 4, wherein the ball swivel comprises a casing having two opposite faces substantially parallel to said rigid metal plates, and two plates of a visco-elastic substance are inserted between said rigid metal plates and said casing faces respectively.

6. A rotor according to claim 5, wherein rigid cross-members are mounted between said rigid metal plates, the length of said cross-members being superior to the distance between said casing opposite faces by a predetermined amount slightly inferior to the sum of the respective thicknesses of said visco-elastic plates, whereby said visco-elastic plates are submitted to a predetermined compressive deformation.

7. A rotor according to claim 6, wherein a pair of said cross-members is disposed to form abutments for the edges of the respective hub arm so as to limit the displacements of the respective rotor blade in the plane of the rotor hub in relation to said hub arm.

8. A rotor according to claim 6, wherein a blade pitch control lever is connected to one of said cross-members.

9. A rotor according to claim 8, wherein the free end of said blade pitch lever is disposed in a plane substantially perpendicular to the axis of the respective hub arm and rotor blade, said plane passing through the center of said spherical abutment.

10. A rotor according to claim 5, wherein each visco-elastic plate if secured by vulcanization on one side to a thin plate applied on the respective rigid metal plate, and, on the other side, to a cover disposed on the respective face of said swivel casing.

11. A rotor according to claim 4, wherein the outer ends of said rigid metal plates are connected to the respective blade root part by two spindles disposed in a substantially symmetrical relationship to the axis of the respective blade, one of said spindle being releasable.

12. A rotor according to claim 2, wherein the blade yoke is a sleeve formed with two divisions opposite one another, the deformable member bearing on terminal inside shoulders of the sleeve, a pitch control lever being secured to an outside collar of the sleeve end.