Nanoreinforced films and laminates for aerospace structures

Patent metadata

Field	Value
Publication number	US-9511562-B2
Application number	US-201213541028-A
Country	US
Kind code	B2
Filing date	Jul 3, 2012
Priority date	Jul 3, 2012
Publication date	Dec 6, 2016
Grant date	Dec 6, 2016

Abstract

A composite laminate for use on an external part of an aerospace vehicle has improved ultraviolet resistance and resistance to microcracking from thermal cycling. The laminate comprises a nanoreinforcement film, a support veil, and a composite layer. The laminate also can have a lightning strike protection layer and an external paint and primer. The nanoreinforcement film can comprise carbon nanomaterial and a polymer resin, and the composite layer has one or more layers of a reinforcement and a polymer resin. The carbon nanomaterial can be carbon nanofibers, and the nanoreinforcement film can have an areal weight of less than about 100 g/m2. The carbon nanomaterial can also comprise carbon nanofibers and carbon nanotubes.

First claim

We claim:

1. A composite laminate for use on an external part of an aerospace vehicle, the laminate comprising:
a single-layer nanoreinforcement film comprising carbon nanomaterial, a polymer resin, and a support veil, wherein the support veil is preimpregnated with the carbon nanomaterial and the polymer resin, wherein the support veil is a nonwoven mat of carbon fibers and a binder, the support veil having an areal weight of less than about 10 grams per square meter; and whereby the single-layer nanoreinforecement film provides improved ultraviolet resistance to the composite laminate and resistance to microcracking from thermal cycling of the composite laminate;
wherein the single-layer nanoreinforcement film comprises an areal weight of less than 100 g/m2;
wherein the carbon nanomaterial comprises carbon nanotubes comprising less than 0.5% by weight of the single-layer nanoreinforcement film;

a composite layer comprising one or more layers of a reinforcement and an additional polymer resin; and
a lightning strike layer comprising a metal screen positioned between the singe-layer nanoreinforcement film and the composite layer.

2. The composite laminate of claim 1 , wherein the carbon nanomaterial comprise carbon nanofibers.

3. The composite laminate of claim 1 , wherein the carbon nanomaterial comprise carbon nanofibers and carbon nanotubes.

4. The composite laminate of claim 3 wherein the carbon nanotubes are multi-walled carbon nanotubes, and the carbon nanofibers comprise up to about 5% by weight of the nanoreinforcement film.

5. The composite laminate of claim 3 , wherein the carbon nanotubes are multi-walled carbon nanotubes, and the carbon nanofibers comprise up to about 3% by weight of the nanoreinforcement film.

6. The composite laminate of claim 3 , wherein the carbon nanofibers and nanotubes comprise about up to about 8% by weight of the nanoreinforcement film.

7. The composite laminate of claim 1 , wherein the reinforcement is a braid, knit, woven, nonwoven, unidirectional fiber tow, or any combination thereof, the composite layer having an areal weight of at least 70 grams per square meter.

8. The composite laminate of claim 1 , wherein the reinforcement is a woven carbon fabric, the additional polymer resin is an epoxy resin, the composite layer having an areal weight of at least 70 grams per square meter.

9. The composite laminate of claim 1 , wherein the lightning strike layer comprises aluminum.

10. The composite laminate of claim 1 , wherein the laminate provides resistance to UV absorption from sunlight, or in a laboratory environment with a xenon arc lamp ranging from 250 to 400 nm, 340 nm nominal wavelength for 0.35W/m2 exposure, with alternating light exposure and water spray, for up to 3000 hours.

11. The composite laminate of claim 1 , wherein the nanoreinforcement film is the external, exposed layer of the external part of the aerospace vehicle.

12. The composite laminate of claim 1 , further comprising one or more paint layers forming the external, exposed layer of the external part of the aerospace vehicle, the one or more paint layers being adjacent to the nanoreinforcement film.

Assignees

• Kruckenberg Teresa May
• Pujar Vijay V
• Mazany Anthony M
• Rohr Inc
• Goodrich Corp

Inventors

• Kruckenberg Teresa May
• Pujar Vijay V
• Mazany Anthony M

Classifications

• B32B2307/20

  having particular electrical or magnetic properties, e.g. piezoelectric · CPC title

• B64C2027/4736

  from composite materials · CPC title

• Y10T442/40

  Knit fabric [i.e., knit strand or strip material] · CPC title

• B32B5/16 Primary

  characterised by features of a layer formed of particles, e.g. chips, powder {or granules (layer formed of natural mineral particles B32B19/00; layer being formed of wood fibres, chips or particles B32B21/02)} · CPC title

• B32B2307/71

  Resistive to light or to UV · CPC title