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EP1674671A2 Expired / Lapsed EP ⏱️ 0.0 years remaining

Composite fan containment case for turbine engines

Assignee: General Electric Co
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Filing: 2005-12-20
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Granted: —
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Expires: 2025-12-20
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Abstract

Abstract A composite fan casing (40) for a gas turbine engine (10) is provided includes, in an exemplary embodiment, a core (50) having a plurality of core layers (52) of reinforcing fiber bonded together with a thermosetting polymeric resin (54). Each core layer (52) includes a plurality of braided reinforcing fibers with the braids of reinforcing fibers aligned in a circumferential direction.

Inventors

  • 👤 Ming Xie
  • 👤 Stephen C. Mitchell
  • 👤 Donald G. Lachapelle
  • 👤 Lee A. Blanton
  • 👤 Richard T. Price
  • 👤 David W. Crall
  • 👤 Frank Worthoff

Bibliographic Details

Application Number —
Jurisdiction EP
Data Source google_patents
Last Synchronized 2026-11-04 23:14
CPC Classifications
F; F01; F01D; F01D21/00; F01D21/04; F01D21/045; D; D04; D04C; D04C1/00; D04C1/02; F01D25/00; F01D25/24; D10; D10B; D10B2505/00; D10B2505/02; F05; F05D; F05D2300/00; F05D2300/40; F05D2300/44; F05D2300/60; F05D2300/603; F05D2300/70; F05D2300/702; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 51 words
A composite fan casing for a gas turbine engine, said casing comprising a core having a plurality of core layers of reinforcing fiber bonded together with a thermosetting polymeric resin, each said core layer comprising a plurality of braided reinforcing fibers, said braids of reinforcing fibers aligned in a circumferential direction.
Claim 2
Dependent Claim 21 words
A composite fan casing in accordance with Claim 1 wherein each said core layer comprises a mat of braided reinforcing fibers.
Claim 3
Dependent Claim 61 words
A composite fan casing in accordance with Claim 1 further comprising at least one buildup layer bonded to at least one of an inner surface of said core and an outer surface of said core, each said build-up layer comprising a plurality of braided reinforcing fibers, said braided fibers wound in a spiral pattern and bonded together with said thermosetting resin.
Claim 4
Dependent Claim 23 words
A composite fan casing in accordance with Claim 1 further comprising at least one stiffener bonded to an outer surface of said core.
Claim 5
Dependent Claim 30 words
A composite fan casing in accordance with Claim 1 wherein said reinforcing fibers comprise at least one of carbon fibers, graphite fibers, glass fibers, ceramic fibers, and aromatic polyamid fibers.
Claim 6
Dependent Claim 31 words
A composite fan casing in accordance with Claim 1 wherein said thermosetting polymeric resin comprises at least one of vinyl ester resins, polyester resins, acrylic resins, epoxy resins, and polyurethane resins.
Claim 7
Independent Claim 60 words
A method of fabricating a composite fan casing for a gas turbine engine, said method comprises forming a core having a plurality of core layers of reinforcing fiber bonded together with a thermosetting polymeric resin, each core layer comprising a plurality of braided reinforcing fibers formed from tows of fibers, the braids of reinforcing fibers aligned in a circumferential direction.
Claim 8
Dependent Claim 33 words
A method in accordance with Claim 7 wherein forming a core comprises forming a core having a plurality of core layers of braided reinforcing fiber mats bonded together with a thermosetting polymeric resin.
Claim 9
Dependent Claim 63 words
A method in accordance with Claim 7 further comprising: forming at least one buildup layer comprising a plurality of braided reinforcing fibers, the braided fibers wound in a spiral pattern and bonded together with the thermosetting resin; and bonding the at least one build-up layer to at least one of an inner surface of the core and an outer surface of the core.
Claim 10
Dependent Claim 21 words
A method in accordance with Claim 7 further comprising bonding at least one stiffener to an outer surface of the core.

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