Soft inplane bearingless helicopter rotor
AssigneeBell Helicopter Textron Inc.
InventorsRobert W. Metzger, William D. Neathery, Peter A. Reyes, Patrick R. Tisdale, Cecil E. Covington, Willem Broekhuizen
Life of this patent
Estimating the term…
Abstract
This invention relates to helicopter rotors and more particularly to rotor mounting involving a composite fiber-reinforced unitary yoke with resilient inplane restraints.
Claims13
A soft inplane bearingless rotor to be rigidly mounted on a helicopter mast comprising:
- (a) a unitary yoke having a flat hub section adapted to be anchored to the end of said mast and having diametrically opposed blade-supporting arms extending from said hub section, each arm having a thin flapping section adjacent said hub section and a feathering section extending from said flapping section with blade attachments at the end of each of said arms, said arms including a plurality of fiber reinforced composite parallel ribs extending span-wise with predetermined inplane spacing;
- (b) a blade secured to each attachment with a cuff extending inboard to said flapping section;
- and
- (c) bearing structure interconnecting the inboard end of said cuff and said flapping section and including inplane resilient structure for soft inplane restraint of said blade.
A soft inplane bearingless rotor to be rigidly mounted on a helicopter mast comprising:
- (a) a unitary yoke having a flat hub section adapted to be anchored to the end of said mast and having an even number of diametrically opposed blade-supporting arms extending from said hub section, each arm having a thin flapping section adjacent said hub section and a feathering section extending from said flapping section with blade attachments at the end of each of said arms, said arms comprising plural fiber reinforced composite ribs with inplane spacing;
- (b) a blade secured to each said blade attachment with cuff extending inboard to said flapping section;
- and
- (c) bearing structure interconnecting the inboard end of said cuff and said flapping section and including inplane resilient structure for soft inplane restraint of said blade.
A soft inplane bearingless rotor to be rigidly mounted on a helicopter mast comprising:
- (a) a unitary yoke having a flat hub section adapted to be anchored to the end of said mast and having at least three uniformly spaced radial blade-supporting arms extending from said hub section, each arm having a thin flapping section adjacent said hub section and a feathering section extending from said flapping section with blade attachments at the end of each of said arms, said arms comprising plural fiber-epoxy composite parallel ribs with predetermined inplane spacing and unified by a medial fiber-epoxy flange structure;
- (b) a blade secured to each said blade attachment with a cuff extending inboard to said flapping section;
- and
- (c) bearing structure interconnecting the inboard end of said cuff and said flapping section and including inplane resilient structure for soft inplane restraint and damping of said blade.
A soft inplane bearingless rotor to be rigidly mounted on a helicopter mast comprising:
- (a) a unitary yoke having a thick flat hub section adapted to be anchored to the end of said mast and having diametrically opposed blade-supporting arms extending from said hub section, each arm having a thin flapping section adjacent said hub section and a feathering section extending from said flapping section with blade attachments at the end of each of said arms, said arms including a plurality of fiber-epoxy parallel ribs extending span-wise and interconnected to maintain inplane spacing of said ribs;
- (b) means for securing a blade to each said blade attachments and for securing a cuff as to extend inboard to said flapping section;
- and
- (c) bearing structure interconnecting the inboard end of said cuff and said flapping section and including inplane resilient structure for soft inplane restraint of said blade.
A soft inplane bearingless rotor to be rigidly mounted on a helicopter mast with foldable blades comprising:
- (a) a unitary yoke having a flat hub section adapted to be anchored to the end of said mast and having diametrically opposed blade-supporting arms extending from said hub section, each arm having a thin flapping section adjacent said hub section and a feathering section extending from said flapping section with a pair of tangentially spaced blade bolt attachments at the end of each of said arms, said arms including a plurality of fiber reinforced composite parallel ribs extending span-wise with predetermined inplane spacing;
- (b) a blade secured to each said blade bolt attachments;
- (c) a cuff secured to said attachments and extending inboard to said flapping section;
- and
- (d) bearing structure interconnecting the inboard end of said cuff and said flapping section and including inplane resilient structure for soft inplane restraint of said blade through said cuff.
A soft inplane bearingless rotor to be rigidly mounted on a helicopter mast comprising:
- (a) a unitary yoke having a flat hub section adapted to be anchored to the end of said mast and having an even number of diametrically opposed blade-supporting arms extending from said hub section, each arm having a thin flapping section adjacent said hub section and a feathering section extending from said flapping section with blade attachments at the end of each of said arms, said feathering section formed of plural stacked loops of fiber-epoxy material forming inplane spaced ribs with said loops encircling said blade attachments on diametrically opposed arms;
- (b) a blade secured to each said blade attachments with cuff extending inboard to said flapping section;
- and
- (c) bearing structure interconnecting the inboard end of said cuff and said flapping section and including inplane yieldable structure for soft inplane restraint of said blade.
A yoke for a soft inplane bearingless rotor to be rigidly mounted on a helicopter mast comprising:
- (a) a flat hub section adapted to be anchored to the end of said mast;
- (b) an even number of diameterically opposed blade-supporting arms extending from said hub section;
- (c) each said arm having a thin flapping section adjacent said hub section and a feathering section extending from said flapping section;
- and
- (d) blade attachments at the end of each of said arms and said feathering sections including a plurality of looped fiber-epoxy material stacked to form a plurality of ribs spaced apart inplane with each said loop encircling said blade attachments on diametrically opposed arms.
Dependencies are inferred from the claim text.