Soft inplane bearingless helicopter rotor

• US 4,427,340 A
• Filed: 06/24/1982
• Issued: 01/24/1984
• Est. Priority Date: 06/24/1982
• Status: Expired due to Term

• Current Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Original Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Inventors: Covington, Cecil E., Broekhuizen, Willem, Reyes, Peter A., Neathery, William D., Tisdale, Patrick R., Metzger, Robert W.
• Primary Examiner(s): Powell, Jr., Everette A.
• Application Number:
  US06/373,525
• Time in Patent Office: 579 Days
• Field of Search: 416/134 A, 416/141, 416/138 A, 416/244 R, 416/230 A
• US Class Current: 416/141
• CPC Class Codes: B64C 27/33 having flexing arms
• CPC Class Codes: B64C 27/51 Damping of blade movements

Abstract

This invention relates to helicopter rotors and more particularly to rotor mounting involving a composite fiber-reinforced unitary yoke with resilient inplane restraints.

Claims

1. 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.

2. The combination set forth in claim 1 wherein said ribs are medially joined by a common flat web of cured fiber-epoxy broad goods.

3. The combination set forth in claim 1 wherein said bearing structure includes a shear restraint mounted in a port extending through said thin flapping section and anchored in cuff-mounted resilient inplane elastomeric bearings above and below said flapping section.

4. The combination set forth in claim 1 in which said cuffs are tubular and elliptical in cross-sections to be stiff inplane for working said bearing structures when said arms undergo lead-lag motion.

5. The combination set forth in claim 4 in which four pitch horns are attached to the inboard end of said cuffs for change of pitch of said blades by forcing flexure of said arms.

6. 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.

7. 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.

8. 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.

9. 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.

10. The combination set forth in claim 9 wherein said ribs are medially joined by a common flat web of cured fiber-epoxy broad goods.

11. The combination set forth in claim 9 wherein said bearing structure includes a shear restraint mounted in a port extending through said thin flapping section and anchored in cuff-mounted resilient inplane elastomeric bearings above and below said flapping section.

12. 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.

13. 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.