Protective ring for the fan protective casing of a gas turbine engine
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-021/00
F02K-003/04
F02K-003/00
출원번호
US-0733363
(2003-12-12)
우선권정보
DE-102 59 943(2002-12-20)
발명자
/ 주소
Schreiber,Karl
출원인 / 주소
Rolls Royce Deutschland Ltd &
Co KG
인용정보
피인용 횟수 :
11인용 특허 :
11
초록▼
A protective ring (4) for the fan blades (2, 3 ) of a gas turbine engine includes a material combination of metal bands and polymer-bonded fiber-weave layers interconnected in alternating arrangement. The protective ring thus formed, which is characterized by tough-elastic properties and low weight
A protective ring (4) for the fan blades (2, 3 ) of a gas turbine engine includes a material combination of metal bands and polymer-bonded fiber-weave layers interconnected in alternating arrangement. The protective ring thus formed, which is characterized by tough-elastic properties and low weight, can be used as a full containment (4') with sufficiently large wall thickness or as a penetration containment (4") with smaller wall thickness and with a trapping layer arranged on the outer circumference. As a full containment, the protective ring has impact-absorption capacity, as a penetration containment it prevents a further destruction of the broken-through protective ring.
대표청구항▼
What is claimed is: 1. A protective ring for a fan protective casing of a gas turbine engine, comprising a penetration sleeve having an alternation of several, interconnected strata, each comprising a metal band and a polymer-impregnated fiber-weave layer; wherein opposite circumferential ends of e
What is claimed is: 1. A protective ring for a fan protective casing of a gas turbine engine, comprising a penetration sleeve having an alternation of several, interconnected strata, each comprising a metal band and a polymer-impregnated fiber-weave layer; wherein opposite circumferential ends of each respective metal band circumferentially overlap one another and respective ones of the fiber-weave layers extend between the circumferentially overlapped ends of adjacent metal bands. 2. A protective ring in accordance with claim 1, wherein the polymer-impregnated fiber-weave layers comprise at least one of glass fibers, polyethylene fibers, polyamide fibers, aramide fibers and carbon fibers impregnated with at least one of polyester and highly energy-absorbing resins, and the metal bands are constructed of at least one of aluminum, titanium and nickel base alloy. 3. A protective ring in accordance with claim 2, wherein at least one of polyamide and polyethylene fibers known under the trade names KEVLAR and DYNEEMA, respectively, are included in the fiber-weave layers. 4. A protective ring in accordance with claim 3, wherein both an inner and outer circumferential surface are each formed by a metal band. 5. A protective ring in accordance with claim 4, wherein multi-stratum strips of metal bands and fiber-weave layers are joined at the ends by an adhesive to form the protective ring. 6. A protective ring in accordance with claim 5, comprising at least two penetration sleeves with matching diameters assembled into one another to obtain a specific large wall thickness. 7. A protective ring in accordance with claim 1, wherein multi-ply strips of metal bands and polymer-bonded fiber-weave layers are wound spirally to obtain a protective ring of sufficient wall thickness. 8. A protective ring in accordance with claim 1, having sufficiently large wall thickness to act as a full containment. 9. A protective ring in accordance with claim 1, comprising a trapping layer of fiber material positioned outside the penetration sleeve for arresting breakthrough of fan blade fragments. 10. A protective ring in accordance with claim 1, comprising outer and inner bands constructed of sheet metal and at least one metallic intermediate band constructed of a metal weave of at least one of nickel, titanium, iron and aluminum. 11. A protective ring in accordance with claim 1, wherein the fiber layers are wound and comprising two outer flanges being conformally integrated by the wound fiber layers. 12. A protective ring in accordance with claim 1, wherein both an inner and outer circumferential surface are each formed by a metal band. 13. A protective ring in accordance with claim 12, wherein multi-stratum strips of metal bands and fiber-weave layers are joined at the ends by an adhesive to form the protective ring. 14. A protective ring in accordance with claim 13, comprising at least two penetration sleeves with matching diameters assembled into one another to obtain a specific large wall thickness. 15. A protective ring in accordance with claim 1, wherein multi-stratum strips of metal bands and fiber-weave layers are joined at the ends by an adhesive to form the protective ring. 16. A protective ring in accordance with claim 1, comprising at least two penetration sleeves with matching diameters assembled into one another to obtain a specific large wall thickness.
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이 특허에 인용된 특허 (11)
Grooman Edward D. (Walnut Creek CA), Ballistic nylon fabric turbine governor housing shielding means.
Schilling, Jan Christopher; Kray, Nicholas Joseph, Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades.
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