Bearingless main rotor assembly torque tube

• US 5,242,267 A
• Filed: 01/08/1993
• Issued: 09/07/1993
• Est. Priority Date: 08/28/1991
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Cullen, I. Lawrence III, Byrnes, Francis E.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): LARSON, JAMES
• Application Number:
  US08/001,943
• Time in Patent Office: 242 Days
• Field of Search: 416/134 A, 416/140, 416/141, 416/230, 156/169, 156/171, 156/173, 156/175, 156/286
• US Class Current: 416/134.00A
• CPC Class Codes: B64C 27/48 Root attachment to rotor head

Abstract

A composite torque tube for a bearingless main rotor (BMR) assembly that is optimally fabricated to meet torsional stiffness, fatigue strength, and buckling strength design constraints at minimal unit weight. The composite torque tube includes a strengthened inboard section for mechanically coupling the torque tube in combination with the hub structure of the BMR assembly, a strengthened outboard section for mechanically coupling the torque tube in combination with a corresponding main rotor blade, and an intermediate section that is operative to accommodate the pitch, flapwise, and/or edgewise loads acting on the BMR assembly during operation thereof. The intermediate section of the torque tube has a constant wall thickness and is formed from continuous filament windings having a predetermined fiber orientation within a broad range of about +/-18° to about +/-40° and/or a narrow range of about +/-26° to about +/-35°. The torque tube is preferably formed from continuous filament windings having an optimal fiber orientation of about +/-35° to provide an intermediate section having a minimal torque tube wall thickness.

Claims

1. A composite torque tube for a bearingless main rotor assembly that is optimally fabricated for minimal weight with respect to predetermined torsional stiffness, fatigue strength, and buckling strength design constraints of the bearingless main rotor assembly, comprising:

a hollow, elongated, tapered structural member formed from a combination of continuous filament windings, wound filaments, fibrous wraps, and fibrous laminates, said structural member including

an inboard section configured for mechanically coupling said composite torque tube in combination with the bearingless main rotor assembly, said inboard section including a snubber subsection and an inboard transition subsection;

an outboard section, and

an intermediate section continuous with said inboard and outboard sections and configured to accommodate pitch, flapwise, and edgewise loads acting on the bearingless main rotor assembly during operation thereof, said intermediate section being formed solely by said continuous filament windings, each of said continuous filament windings forming said intermediate section having a predetermined fiber orientation selected from a range of fiber orientations of about ±

18°

to about ±

40°

to provide a minimal, constant torque tube wall thickness for said intermediate section that accommodates the predetermined torsional stiffness, fatigue strength, and buckling strength design constraints of the bearingless main rotor assembly;

said inboard and outboard sections including each of said continuous filament windings forming said intermediate section, each of said continuous filament windings in said snubber subsection having a ±

45°

fiber orientation; and

wherein

each of said continuous filament windings forming said intermediate section transitions from said predetermined fiber orientation of said intermediate section to said ±

45°

fiber orientation of said snubber subsection over said inboard transition subsection.

2. The composite torque tube of claim 1 wherein said intermediate section is formed solely by said continuous filament windings, each of said continuous filament windings having said predetermined fiber orientation selected from a range of fiber orientations of about ±

26°

to about ±

35°

to provide said minimal, constant torque tube wall thickness for said intermediate section that accommodates the predetermined torsional stiffness, fatigue strength, and buckling strength design constraints of the bearingless main rotor assembly.

3. The composite torque tube of claim 1 wherein said intermediate section is formed solely by said continuous filament windings, each of said continuous filament windings having an optimal fiber orientation of about ±

35°

to provide said minimal, constant torque tube wall thickness for said intermediate section that accommodates the predetermined torsional stiffness, fatigue strength, and buckling strength design constraints of the bearingless main rotor assembly.

4. The composite torque tube of claim 3 wherein each of said continuous filament windings having said ±

35°

optimal fiber orientation transition to said ±

45°

fiber orientation in said snubber subsection of said inboard section over said inboard transition subsection.

5. The composite torque tube of claim 1 wherein said outboard section includes said fibrous laminates having a 0°

fiber orientation to react mechanical coupling loads of the bearingless main rotor assembly.

6. The composite torque tube of claim 1 wherein said outboard section includes said fibrous laminates and fibrous wraps having a ±

45°

fiber orientation to accommodate load transfers in the bearingless main rotor assembly.

7. The composite torque tube of claim 1 wherein said inboard section includes said wound filaments having a 90°

fiber orientation to accommodate hoop stresses in the bearingless main rotor assembly.

8. The composite torque tube of claim 1 wherein said inboard section includes said fibrous wraps having a ±

45°

fiber orientation to accommodate bearing loads in the bearingless main rotor assembly.

9. The composite torque tube of claim 1 wherein said inboard section has aligned snubber apertures formed in ventral and dorsal surfaces thereof.