Rotor assemblies and other composite structures with aligned bearing supports and methods of manufacture

Patent metadata

Field	Value
Publication number	US-9533342-B1
Application number	US-201313923795-A
Country	US
Kind code	B1
Filing date	Jun 21, 2013
Priority date	Jun 21, 2013
Publication date	Jan 3, 2017
Grant date	Jan 3, 2017

Abstract

Methods of co-curing aligned annular supports in a tubular region of a composite structure, such as a rotor blade, are disclosed. Methods include assembling an uncured composite structure by positioning an inboard annular support and an outboard annular support around an arbor, forming reinforcement fiber into a tubular region in contact with the supports, and applying a matrix material to the reinforcement fiber. The inboard and outboard annular supports are substantially composed of metal. Methods also include concentrically aligning the arbor and the supports along a common axis by applying heat to cause differential expansion of the arbor with respect to the supports, wherein the differential expansion causes an interference fit of the supports against the arbor. Methods also include curing the uncured composite structure to form the composite structure.

First claim

The invention claimed is:

1. A method of co-curing aligned annular supports in a tubular region of a rotor blade, the method comprising:
assembling an uncured composite structure, comprising:
positioning an inboard annular support around an arbor;
positioning an outboard annular support around the arbor, spaced apart from the inboard annular support;
positioning a rotational orientation support proximate to the arbor;
forming reinforcement fiber into a tubular region in contact with the inboard annular support, the outboard annular support, and the rotational orientation support; and
applying a matrix material to the reinforcement fiber;

concentrically aligning the arbor, the inboard annular support, and the outboard annular support along a common axis by applying heat to cause differential expansion of the arbor and the inboard annular support, and to cause differential expansion of the arbor and the outboard annular support, wherein the differential expansion causes an interference fit of the inboard annular support against the arbor and an interference fit of the outboard annular support against the arbor;
curing the uncured composite structure to form the rotor blade, wherein curing includes the applying heat to cause differential expansion; and
forming an aperture, at a predefined angle with respect to the orientation feature, through the rotor blade and the rotational orientation support.

2. A method of co-curing aligned annular supports in a tubular region of a composite structure, the method comprising:
assembling an uncured composite structure, comprising:
positioning an inboard annular support around an arbor, wherein the inboard annular support is substantially composed of metal;
positioning an outboard annular support around the arbor, wherein the outboard annular support is substantially composed of metal;
forming reinforcement fiber into a tubular region in contact with the inboard annular support and the outboard annular support; and
applying a matrix material to the reinforcement fiber;

concentrically aligning the arbor, the inboard annular support, and the outboard annular support along a common axis by applying heat to cause differential expansion of the arbor and the inboard annular support, and to cause differential expansion of the arbor and the outboard annular support, wherein the differential expansion causes an interference fit of the inboard annular support against the arbor and an interference fit of the outboard annular support against the arbor; and
curing the uncured composite structure to form the composite structure.

3. The method of claim 2 , wherein the curing includes heating the uncured composite structure.

4. The method of claim 3 , wherein the heating the uncured composite structure includes the applying heat to cause differential expansion.

5. The method of claim 2 , further comprising:
separating the arbor from the composite structure after curing by cooling the arbor.

6. The method of claim 2 , wherein a coefficient of thermal expansion of the arbor is significantly greater than a coefficient of thermal expansion of the inboard annular support and significantly greater than a coefficient of thermal expansion of the outboard annular support.

7. The method of claim 2 , wherein the arbor has a coefficient of thermal expansion greater than 20 ppm/° C.

8. The method of claim 2 , wherein the arbor includes aluminum alloy.

9. The method of claim 2 , wherein the inboard annular support has a coefficient of thermal expansion less than 10 ppm/° C., and wherein the outboard annular support has a coefficient of thermal expansion less than 10 ppm/° C.

10. The method of claim 2 , wherein the inboard annular support includes titanium alloy, and wherein the outboard annular support includes titanium alloy.

11. The method of claim 2 , wherein the positioning an inboard annular support includes positioning the inboard annular support proximate to an inboard alignment surface of the arbor, wherein the inboard alignment surface is substantially cylindrical,
wherein the positioning an outboard annular support includes positioning the outboard annular support proximate to an outboard alignment surface of the arbor, and wherein the outboard alignment surface is substantially cylindrical.

12. The method of claim 2 , wherein the arbor is sufficiently rigid to maintain the common axis during the curing.

13. The method of claim 2 , wherein the arbor includes an inboard shoulder, and wherein the positioning the inboard annular support includes positioning the inboard annular support in contact with the inboard shoulder.

14. The method of claim 2 , wherein the arbor includes an outboard shoulder, and wherein the positioning the outboard annular support includes positioning the outboard annular support in contact with the outboard shoulder.

15. The method of claim 2 , wherein the positioning the outboard annular support includes spacing the outboard annular support apart from the inboard annular support.

16. The method of claim 2 , further comprising:
molding the uncured composite structure by resin transfer molding.

17. The method of claim 2 , wherein the assembling further comprises:
positioning a rotational orientation support proximate to the arbor,
wherein the rotational orientation support includes an orientation feature, and wherein the forming includes forming the reinforcement fiber into a tubular region in contact with the rotational orientation support.

18. The method of claim 17 , further comprising:
forming an aperture, at a predefined angle with respect to the orientation feature, through the composite structure and the rotational orientation support.

19. The method of claim 17 , wherein the rotational orientation support and the outboard annular support form a monolithic part.

20. A method of co-curing aligned annular supports in a tubular region of a composite structure, the method comprising:
assembling an uncured composite structure, comprising:
positioning an inboard annular support around an arbor;
positioning an outboard annular support around the arbor;
forming reinforcement fiber into a tubular region in contact with the inboard annular support and the outboard annular support; and
applying a matrix material to the reinforcement fiber;

concentrically aligning the arbor, the inboard annular support, and the outboard annular support along a common axis by applying heat to cause differential expansion of the arbor and the inboard annular support, and to cause differential expansion of the arbor and the outboard annular support, wherein the differential expansion causes an interference fit of the inboard annular support against the arbor and an interference fit of the outboard annular support against the arbor;
curing the uncured composite structure to form the composite structure;
detachably securing an inboard pitch bearing in contact with the inboard annular support of the composite structure, wherein the inboard pitch bearing is one of a bushing, a ball bearing assembly, a roller bearing assembly, and a needle bearing assembly; and
detachably securing an outboard pitch bearing in contact with the outboard annular support of the composite structure, wherein the outboard pitch bearing is one of a bushing, a ball bearing assembly, a roller bearing assembly, and a needle bearing assembly.

21. The method of claim 20 , wherein the inboard pitch bearing includes dry PTFE, and wherein the outboard pitch bearing includes dry PTF

Assignees

• Boeing Co

Inventors

• Kennedy Dennis K

Classifications

• B21D53/78 Primary

  propeller blades; turbine blades · CPC title

• B29C37/0064

  of reinforced material · CPC title

• B29C35/02 Primary

  Heating or curing, e.g. crosslinking or vulcanizing {during moulding, e.g. in a mould}(cold vulcanisation B29C35/18 {; vulcanising tyres, presses therefor B29D30/0601}) · CPC title

• B29K2105/243

  Partially cured · CPC title

• B29K2105/246

  Uncured, e.g. green · CPC title