Composite nosecone

Patent metadata

Field	Value
Publication number	US-11078839-B2
Application number	US-201815876574-A
Country	US
Kind code	B2
Filing date	Jan 22, 2018
Priority date	Jan 22, 2018
Publication date	Aug 3, 2021
Grant date	Aug 3, 2021

Abstract

The disclosure describes composite nosecones and techniques for forming composite nosecones including a matrix material, relatively higher-modulus reinforcement elements, and relatively tougher polymer-based reinforcement elements. An example composite nosecone includes a body substantially symmetrical around a central axis. The body includes a side wall defining a diameter of the body that increases from a forward side of the body to an aft side of the body. The body includes a composite material including a plurality of relatively higher-modulus reinforcement elements, a plurality of relatively tougher polymer-based reinforcement elements, and a matrix material substantially encapsulating the plurality of relatively higher-modulus reinforcement elements and the plurality of relatively tougher polymer-based reinforcement elements. The plurality of relatively higher-modulus reinforcement elements are different from the plurality of relatively tougher polymer-based reinforcement elements.

First claim

What is claimed is:

1. A composite nosecone comprising:
a body substantially symmetrical around a central axis, the body including a side wall defining a diameter of the body that increases from a forward side of the body to an aft side of the body,
wherein the body comprises a composite material including a plurality of relatively higher-modulus reinforcement elements, a plurality of relatively tougher polymer-based reinforcement elements, and a matrix material substantially encapsulating the plurality of relatively higher-modulus reinforcement elements and the plurality of relatively tougher polymer-based reinforcement elements,
wherein the plurality of relatively higher-modulus reinforcement elements are different from the plurality of relatively tougher polymer-based reinforcement elements,
wherein the side wall comprises:
a forward annular region comprising a first layer, wherein the forward annular region has a first ratio of relatively higher-modulus reinforcement elements to relatively tougher polymer-based reinforcement elements; and
an aft annular region comprising the first layer and a second layer, wherein the aft annular region has a second ratio of relatively higher-modulus reinforcement elements to relatively tougher polymer-based reinforcement elements, and wherein the first ratio is greater than the second ratio.

2. The composite nosecone of claim 1 , wherein the plurality of relatively higher-modulus reinforcement elements have a tensile modulus of greater than 60 GPa and an elongation at break of less than 6.0%.

3. The composite nosecone of claim 1 , wherein the plurality of relatively higher-modulus reinforcement elements have a tensile modulus of greater than 180 GPa and an elongation at break of less than 6.0%.

4. The composite nosecone of claim 2 , wherein the plurality of relatively higher-modulus reinforcement elements comprise at least one of an aromatic polyamide, a carbon fiber, E-glass, or S-glass.

5. The composite nosecone of claim 1 , wherein the plurality of relatively tougher polymer-based reinforcement elements have an elongation at break of greater than 6.0%.

6. The composite nosecone of claim 5 , wherein the plurality of relatively tougher polymer-based reinforcement elements comprise at least one of a polyamide, a polyester, a polyester terephthalate, a polypropylene, a polyethylene, or a spider silk.

7. The composite nosecone of claim 1 , further comprising at least one attachment area integrally formed with the body, wherein the at least one attachment area comprises the first layer and the second layer, and wherein the at least one attachment area is shaped and positioned to attach the composite nosecone to a fan assembly.

8. The composite nosecone of claim 1 , wherein the plurality of relatively higher-modulus reinforcement elements comprise relatively higher-modulus filaments, wherein the plurality of relatively tougher polymer-based reinforcement elements comprise relatively tougher polymer-based filaments, and wherein the relatively higher-modulus filaments and relatively tougher polymer-based filaments are together in a hybrid or commingled braid, a hybrid or commingled weave, or a hybrid or commingled winding.

9. The composite nosecone of claim 1 , wherein the matrix material comprises a thermoset polymer.

10. The composite nosecone of claim 1 , wherein the aft annular region is a second annular region, wherein side wall further comprises:
a third annular region aft the second annular region, wherein the third annular region comprises the first layer, the second layer, and a third layer, and wherein the third annular region has a third ratio of relatively higher-modulus reinforcement elements to relatively tougher polymer-based reinforcement elements, wherein the second ratio is greater than the third ratio; and
a fourth annular region aft the third annular region, wherein the fourth annular region comprise the first layer, the second layer, the third layer, and a fourth layer, and wherein the fourth annular region has a fourth ratio of relatively higher-modulus reinforcement elements to relatively tougher polymer-based reinforcement elements, wherein the third ratio is greater than the fourth ratio.

11. A method of constructing a composite nosecone, the method comprising:
defining a nosecone shape with a matrix material, a plurality of relatively higher-modulus reinforcement elements, and a plurality of relatively tougher polymer-based reinforcement elements, wherein the plurality of relatively higher-modulus reinforcement elements are different from the plurality of relatively tougher polymer-based reinforcement elements, wherein the composite nosecone comprises a body substantially symmetrical around a central axis, the body including a side wall defining a diameter of the body that increases from a forward side of the body to an aft side of the body, and wherein the side wall comprises:
a forward annular region comprising a first layer, wherein the forward annular region has a first ratio of relatively higher-modulus reinforcement elements to relatively tougher polymer-based reinforcement elements; and
an aft annular region comprising the first layer and a second layer, wherein the aft annular region has a second ratio of relatively higher-modulus reinforcement elements to relatively tougher polymer-based reinforcement elements, and wherein the first ratio is greater than the second ratio; and

curing a matrix material substantially encapsulating the plurality of relatively higher-modulus reinforcement elements and the plurality of relatively tougher polymer-based reinforcement elements to form the composite nosecone.

12. The method of claim 11 , wherein the plurality of relatively higher-modulus reinforcement elements have a tensile modulus of greater than 60 GPa and an elongation at break of less than 6.0%.

13. The method of claim 12 , wherein the plurality of relatively higher-modulus reinforcement elements comprise at least one of an aromatic polyamide, a carbon fiber, E-glass, or S-glass.

14. The method of claim 11 , wherein the plurality of relatively higher-modulus reinforcement elements have a tensile modulus of greater than 180 GPa and an elongation at break of less than 6.0%.

15. The method of claim 11 , wherein the plurality of relatively tougher polymer-based reinforcement elements have an elongation at break of greater than 6.0%.

16. The method of claim 15 , wherein the plurality of relatively tougher polymer-based reinforcement elements comprise at least one of a polyamide, a polyester, a polyester terephthalate, a polypropylene, a polyethylene, or a spider silk.

17. The method of claim 11 , wherein the composite nosecone further comprises at least one attachment area integrally formed with the body, wherein the at least one attachment area comprises the first layer and the second layer, and wherein the at least one attachment area is shaped and positioned to attach the composite nosecone to a fan assembly.

18. The method of claim 11 , wherein the plurality of relatively higher-modulus reinforcement elements comprise relatively higher-modulus filaments, wherein the plurality of relatively tougher polymer-based reinforcement elements comprise relatively tougher polymer-based filaments, and wherein the relatively higher-modulus filaments and relatively tougher polymer-based filaments are together in a hybrid or commingled braid, a hybrid or commingled weave, or a hybrid or commingled winding.

19. The method of claim 11 , wherein the defining the composite nosecone comprises:

Assignees

• Rolls Royce Corp

Inventors

• Heeter Robert
• Kappes Matthew J
• Hodgson Benedict N

Classifications

• F02C7/05

  having provisions for obviating the penetration of damaging objects or particles · CPC title

• B29C70/08 Primary

  comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers · CPC title

• F01D5/282

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• C08J2300/24

  Thermosetting resins · CPC title

• B32B2377/00

  Polyamides · CPC title