Composite over wrap

Patent metadata

Field	Value
Publication number	US-10247273-B2
Application number	US-201615180334-A
Country	US
Kind code	B2
Filing date	Jun 13, 2016
Priority date	Aug 28, 2015
Publication date	Apr 2, 2019
Grant date	Apr 2, 2019

Abstract

A composite wrap is provided for damping vibration in an elongated quill shaft having a cylindrical body. The composite wrap includes interior layering for disposition about a cylindrical body, exterior layering configured to define an exterior composite wrap shape and sequential cured-in-place, vibration damping, fibrous epoxy layers. The sequential cured-in-place, vibration damping, fibrous epoxy layers are radially interposed between the interior and exterior layering to dampen vibrations of and/or to adjust a resonance frequency of the cylindrical body.

First claim

What is claimed is:

1. A composite wrap for damping vibration in an elongated quill shaft having a cylindrical body, the composite wrap comprising:
interior layering including a release coating for disposition about the cylindrical body;
exterior layering configured to define an exterior composite wrap shape; and
sequential cured-in-place, vibration damping, fibrous epoxy layers radially interposed between the interior layering and the exterior layering to dampen vibrations of and/or to adjust a resonance frequency of the cylindrical body, wherein the fibrous epoxy layer positioned adjacent the exterior layering includes overwrap portions proximate a first longitudinal end and a second longitudinal end of the composite wrap.

2. The composite wrap according to claim 1 , wherein:
the interior layering further comprises a rubber interface layer; and
the exterior layering further comprises a tape wrap layer of varying fiber orientations and a nylon layer.

3. The composite wrap according to claim 1 , wherein the sequential cured-in-place, vibration damping, fibrous epoxy layers comprise layers of fibers suspended within epoxy matrixes.

4. The composite wrap according to claim 3 , wherein the layers of the fibers comprise layers of woven or unidirectional graphite, fiberglass, or aramid fibers suspended within the epoxy matrixes with varying fiber orientations.

5. The composite wrap according to claim 3 , wherein:
a first one of the layers of the fibers comprises fibers having first degree fiber orientations,
a second one of the layers of the fibers comprises fibers having second degree fiber orientations, and
a third one of the layers of the fibers comprises fibers having third degree fiber orientations,
at least one of the first, second and third degree fiber orientations being unique from the others.

6. The composite wrap according to claim 5 , wherein the third one of the layers of the fibers includes the overwrap portions.

7. A quill shaft, comprising:
an elongate shaft member having a central portion and first and second opposite longitudinal ends; and
a composite wrap, the composite wrap comprising:
interior layering including a release coating for disposition about the central portion;
exterior layering configured to define an exterior composite wrap shape; and
sequential cured-in-place, vibration damping, fibrous epoxy layers radially interposed between the interior layers and the exterior layering to dampen quill shaft vibrations and/or to adjust a quill shaft resonance frequency, wherein the fibrous epoxy layer positioned adjacent the exterior layering includes overwrap portions proximate a first longitudinal end and a second longitudinal end of the composite wrap.

8. The quill shaft according to claim 7 , wherein:
the elongate shaft member comprises metallic material,
the first longitudinal end comprises a first cylindrical body having a larger diameter than the central portion, a first curved interface and a splined distal end, and
the second longitudinal end comprises a second cylindrical body having a larger diameter than the central portion, a second curved interface and a distal end.

9. The quill shaft according to claim 7 , wherein,
the first longitudinal end comprises a first cylindrical body having a larger diameter than the central portion, a first curved interface and a splined distal end, and
the second longitudinal end comprises a second cylindrical body having a larger diameter than the central portion, a second curved interface and a distal end.

10. The quill shaft according to claim 9 , wherein the composite wrap comprises:
an interior surface to abut with an exterior surface of the central portion;
curved axial surfaces to abut with respective exterior surfaces of the first and second curved interfaces; and
an exterior surface coplanar with respective planes of exterior surfaces of the first and second cylindrical bodies.

11. The quill shaft according to claim 7 , wherein:
the interior layering further comprises a rubber interface layer; and
the exterior layering further comprises a tape wrap layer of varying fiber orientations and a nylon layer.

12. The quill shaft according to claim 7 , wherein the sequential cured-in-place, vibration damping fibrous epoxy layers comprise layers fibers suspended within epoxy matrixes.

13. The quill shaft according to claim 12 , wherein the layers of the fibers comprise layers of woven or unidirectional graphite, fiberglass, aramid fibers suspended within the epoxy matrixes with varying fiber orientations.

14. The quill shaft according to claim 12 , wherein:
a first one of the layers of the fibers comprises fibers having first degree fiber orientations,
a second one of the layers of the fibers comprises fibers having second degree fiber orientations, and
a third one of the layers of the fibers comprises fibers having third degree fiber orientations,
at least one of the first, second and third degree fiber orientations being unique from the others.

15. An aircraft comprising a first gear and a second gear connected by the quill shaft of claim 7 which transmits torsional energy between the first and second gears.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Bremmer Jonathan
• Sauer Jeffrey G
• Lacko Robert A
• Song Shihong G
• Meeson Jr John H

Classifications

• B32B2260/046

  Synthetic resin · CPC title

• B32B5/02

  characterised by structural features of a {fibrous or filamentary} layer {(layer formed of metallic wires B32B15/02; layer formed of natural mineral fibres B32B19/02; layer formed of wood fibres B32B21/02)} · CPC title

• B32B5/26

  another layer {next to it} also being fibrous or filamentary {(relative arrangement of fibres or filaments of different layers B32B5/12)} · CPC title

• B32B5/12

  characterised by the relative arrangement of fibres or filaments of {different layers, e.g. the fibres or filaments being parallel or perpendicular to each other} · CPC title

• B32B7/06

  permitting easy separation · CPC title