High speed composite drive shaft

Patent metadata

Field	Value
Publication number	US-9759252-B2
Application number	US-201314018782-A
Country	US
Kind code	B2
Filing date	Sep 5, 2013
Priority date	Sep 5, 2013
Publication date	Sep 12, 2017
Grant date	Sep 12, 2017

Abstract

A shaft assembly includes one or more axially-arranged plies having a plurality of bundles of strands. Each strand is formed of a ultra-high modulus carbon fiber material. One or more strands of glass fiber are wrapped around each bundle of the plurality of bundles. A volume of resin injected into the one or more axially-arranged plies and the assembly is cured via a resin transfer molding process. A method of forming a shaft assembly includes arranging a plurality of strands of ultra-high modulus carbon fiber material into a plurality of bundles. Each bundle of the plurality of bundles is wrapped with one or more strands of glass fiber material. The plurality of bundles are arranged into one or more axially-extending plies at a mandrel. A volume of resin is injected into the plurality of bundles and is cured to form the shaft assembly.

First claim

The invention claimed is:

1. A shaft assembly having a shaft axis and comprising:
one or more axially-arranged plies arranged along the shaft axis including:
a plurality of bundles arranged adjacent to each other in each of the one or more axially-arranged plies, the plurality of bundles extending in an axial direction of the shaft axis and in parallel with the shaft axis, each bundle of the plurality of bundles including:
a plurality of carbon fiber strands arranged at least substantially parallel to each other and in the axial direction of the shaft axis, the plurality of carbon fiber strands formed of an ultra-high modulus carbon fiber material having a tensile modulus of at least 70 Mpsi; and
one or more wrap strands of glass fiber wrapped around the plurality of carbon fiber strands of each bundle of the plurality of bundles; and
a volume of resin injected into the one or more axially-arranged plies;
wherein the one or more axially-arranged plies are arranged in a tubular shape about the shaft axis,
further comprising one or more end fittings secured to one or more axial ends of the shaft assembly, the end fitting being connectible to a drive train.

2. The shaft assembly of claim 1 , wherein the one or more axially-arranged plies include a plurality of radially arranged plies that are radially arranged with respect to each other, and further comprising one or more bias plies of carbon fiber material disposed between adjacent radially arranged plies, and the one or more bias plies of carbon fiber material extending in the axial direction.

3. The shaft assembly of claim 2 , wherein a bias modulus of the one or more bias plies is lower than the tensile modulus of the ultra-high modulus carbon fiber material.

4. The shaft assembly of claim 3 , wherein the tensile modulus is about 85 Mpsi.

5. The shaft assembly of claim 1 , wherein the tensile modulus of the ultra-high modulus carbon fiber material is about 85 Mpsi.

6. The shaft assembly of claim 1 , wherein the volume of resin is a bismaleimide resin.

7. The shaft assembly of claim 1 , wherein the one or more wrap strands of glass fiber are oriented at +/−45 degrees relative to the shaft axis.

8. A rotary-winged aircraft comprising:
an airframe;
an engine disposed at the airframe, the engine operably connected to and driving a rotor assembly; and
a drive shaft having a shaft axis and connecting the engine to the rotor assembly, the drive shaft including:
one or more axially-arranged plies including:
a plurality of bundles arranged adjacent to each other in each of the one or more axially-arranged plies, the plurality of bundles extending in an axial direction of the shaft axis and in parallel with the shaft axis, each bundle of the plurality of bundles including:
a plurality of carbon fiber strands arranged at least substantially parallel to each other and in the axial direction of the shaft axis, the plurality of carbon fiber strands formed of a ultra-high modulus carbon fiber material having a tensile modulus of at least 70 Mpsi; and
one or more wrap strands of glass fiber wrapped around the plurality of carbon fiber strands of each bundle of the plurality of bundles; and
a volume resin injected into the one or more axially-arranged plies;
wherein the one or more axially arranged plies and the volume of resin are cured via a resin transfer molding process,
further comprising one or more end fittings secured to one or more axial ends of the drive shaft.

9. The aircraft of claim 8 , wherein the one or more axially-arranged plies include a plurality of radially arranged plies that are radially arranged with respect to each other, and further comprising one or more bias plies of carbon fiber material disposed between adjacent radially arranged plies, and the one or more bias plies of carbon fiber material extending in the axial direction.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Nguyen Dean
• Davis Geoffrey Clive Robert

Classifications

• B29K2309/08

  Glass · CPC title

• B29K2101/10

  Thermosetting resins · CPC title

• B29C70/48

  and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title

• B29K2307/04

  Carbon · CPC title

• B29L2031/75

  Shafts · CPC title