IP Library Granted Patent US 10,569,867
Granted Patent B2
US 10,569,867 · App. 16/100,499 · Granted Feb 25, 2020

Composite rotor system using two race track style cantilevered yokes

Inventors: Andrew Maresh (Lewisville, TX); Frank Bradley Stamps (Colleyville, TX); Patrick Ryan Tisdale (Keller, TX); Robert Patrick Wardlaw (Keller, TX); Andrew Haldeman (Fort Worth, TX); Drew Alan Sutton (Georgetown, KY)
Assignee: BELL HELICOPTER TEXTRON INC.
B64C27/33B64C11/02B64C11/12B64C27/35B64C27/48
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Quick Facts
Patent No.
US 10,569,867
App. No.
16/100,499
Granted
Feb 25, 2020
Kind
B2
Abstract

A hub system comprises at least one yoke, at least one shear bearing, and at least one mast adapter. The at least one mast adapter is configured to support the at least one yoke and the at least one shear bearing, and the at least one yoke has a flapping hinge that is non-coincident with a flapping hinge of the at least one shear bearing. Another hub system comprises a stacked yoke and a mast adapter. The mast adapter is configured to transfer rotation from a rotor mast to the hub system to rotate the hub system about a central axis of rotation. The mast adapter is further configured to support the stacked yoke such that each yoke in the stacked yoke is configured to accommodate at least some amount of rotation about an axis that is perpendicular to or about perpendicular to the central axis of rotation.

Claims (9)

1. A hub system comprising:

a mast adapter;

a stacked yoke comprising at least a first race-track style yoke and a second race-track style yoke;

a spring mechanism; and

wherein the mast adapter is configured to support the stacked yoke and the spring mechanism, wherein the mast adapter is configured to restrain the stacked yoke in in-plane and out-of-plane directions, and wherein the spring mechanism is configured to control a bent shape of yokes in the stacked yoke, and

wherein the spring mechanism comprises a cantilevered plate that is parallel to a yoke arm and that is affixed to the mast adapter, wherein the mast adapter is a cantilevered support structure that is configured to apply force in a flapping direction.

2. The hub system of claim 1 , wherein the spring mechanism comprises a leaf spring.

3. The hub system of claim 1 , wherein the spring mechanism is selected from a group consisting of a coil, a torsional, an elastomeric, or a flexure spring mechanism.

4. The hub system of claim 1 , wherein the spring mechanism comprises multiple spring mechanisms, and wherein the multiple spring mechanisms are spaced along a span of a flexure of the stacked yoke to create multiple virtual hinge points in the stacked yoke.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 13, 2021
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 056228/0183 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 10, 2018
From: MARESH, ANDREW; STAMPS, FRANK BRADLEY; TISDALE, PATRICK RYAN; WARDLAW, ROBERT; HALDEMAN, ANDREW; SUTTON, DREW
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 046612/0334 →
Continuity (3)
Division 15362424 · Nov 28, 2016
Division 13801733 · Mar 13, 2013
Related Publication 20180346109A1 · Dec 6, 2018