Elastomeric Double Hooke's Joint for Rotor 2P Vibration Reduction

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Rotary-wing aircraft using a Hooke's joint as a rotor gimbal experience 2P vibration due to the lengthening and shortening of the gimbal during flapping, which existing configurations fail to adequately address.

Innovation Solution

A double Hooke's joint system is employed, comprising an upper and lower Hooke's joint with elastomeric journal bearings, allowing the hub plane to float vertically and eliminating axial load generation, thereby reducing vibration and weight while maintaining a compact design.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single Hooke's joint is used as a rotor gimbal, then the structure is simple and compact, but 2P vibration occurs due to lengthening and shortening of the gimbal during flapping

Engineering Contradiction:
Improvegimbal structureVSAvoid2P vibration
Core Design Contradiction:
Device complexityVSObject-affected harmful factors

Solution Approach 1:

The single Hooke's joint is divided into two separate Hooke's joints (upper and lower) that are coupled together. This segmentation allows each joint to handle specific rotational movements independently, preventing the lengthening and shortening that causes 2P vibration while maintaining overall structural compactness.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A spherical bearing is introduced as an intermediary component between the upper and lower Hooke's joints. This spherical bearing allows the upper Hooke's joint to float and move laterally along the mast, accommodating flapping motion without transmitting axial loads that would cause vibration.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Stability of the object's composition

If traditional rigid bearings are used in the Hooke's joint, then structural stability is maintained, but axial load generation causes increased vibration and weight

Engineering Contradiction:
Improvejoint stabilityVSAvoidaxial load vibration
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The bearing type is changed from rigid to elastomeric, fundamentally altering the mechanical parameters of the joint. Elastomeric bearings provide flexibility that allows accommodation of flapping motion without generating axial loads, thereby reducing vibration while maintaining joint stability through elastic deformation.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

Elastomeric materials are used in the bearings to combine the properties of flexibility and load-bearing capability. This composite material approach allows the bearing to deform elastically under load, absorbing flapping motions without transmitting harmful axial loads to the rotor system.

Inventive Principle:
Principle #40Composite materials

3Strength

If the hub plane is constrained vertically, then structural support is provided, but vibration increases due to axial load generation during flapping

Engineering Contradiction:
Improvestructural supportVSAvoidvibration
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The hub plane is given dynamic freedom to float vertically through the spherical bearing rather than being rigidly constrained. This dynamic capability allows the system to adapt to flapping motions in real-time, maintaining structural support while eliminating the axial loads that generate vibration during operational cycles.

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The double Hooke's joint system effectively reduces 2P vibration and weight, enabling a more efficient and compact rotor assembly that maintains constant angular velocity during rotation.

Implementation Method 1

a first set of bearings coupled to each arm on the second axis of the upper Hooke's joint and to each arm on the fourth axis of the lower Hooke's joint, wherein the first set of bearings comprise an elastomer

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

elastomeric journal bearings

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 3

an upper Hooke's joint having four arms extending radially outward to define first and second axes, the upper Hooke's joint adapted to be coupled to a rotor system yoke; a lower Hooke's joint having four arms extending radially outward to define third and fourth axes

Methodology Applied
Scientific EffectHooke's joint mechanism:

Implementation Method 4

a spherical bearing configured to allow the upper Hooke's joint to move laterally along a mast

Methodology Applied
Scientific EffectSpherical bearing:

Data Source

PatentUS11136116B2Elastomeric double Hooke's joint
Publication Date: 2021.10.05 TEXTRON INNOVATIONS INC
  • US11136116B2 patent drawing
  • US11136116B2 patent drawing
  • US11136116B2 patent drawing

AI summary

Embodiments are directed to a double Hooke's joint gimbal in a rotor system. An upper Hooke's joint has four arms extending radially outward to define first and second axes, and a lower Hooke's joint has four arms extending radially outward to define third and fourth axes. A pair of connectors couple the upper Hooke's joint and the lower Hooke's joint. A first set of bearings are positioned between arms on the upper and lower Hooke's joints and the connectors. The first set of bearings comprise an elastomer, such as elastomeric journal bearings. The upper Hooke's joint is coupled to a yoke and rotor blades by a driver assembly that allows rotor blade flapping. The lower Hooke's joint is coupled to and driven by a mast. A spherical bearing allows the upper Hooke's joint to move laterally along the mast.