[특허]Mid-mount centerbody heat shield for turbine engine fuel nozzle

United Technologies Corporation

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특허 상세정보

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내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Mid-mount centerbody heat shield for turbine engine fuel nozzle

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02C-001/00 F02G-003/00
미국특허분류(USC)	060/737; 060/740; 060/748
출원번호	UP-0513711 (2006-08-31)
등록번호	US-7658074 (2010-04-02)
발명자 / 주소	Tuttle, Mark E.
출원인 / 주소	United Technologies Corporation
대리인 / 주소	Carlson, Gaskey & Olds
인용정보	피인용 횟수 : 4 인용 특허 : 8

초록

A fuel nozzle for a gas turbine engine includes an engine mount end and a discharge end that discharges an air/fuel mixture into a combustion chamber. The fuel nozzle includes a centerbody and a heat shield. The heat shield is fixed to the centerbody at a mid-mount position that is centrally located between first and second ends of the heat shield to allow the heat shield to remain thermally isolated from radially adjacent components to reduce the adverse effects of thermal stresses.

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What is claimed is: 1. A fuel nozzle comprising: a centerbody having an inlet end and a discharge end for discharging an air/fuel mixture into a combustion chamber; and a heat shield positioned within a central passage of said centerbody and having a first end at said inlet end and a second end at said discharge end, wherein an outer surface of said heat shield is only fixed to an inner surface of said centerbody at a mid-mount position located generally centrally between said first end and said second end. 2. The fuel nozzle according to claim 1 wherein said first and said second ends are movable relative to said centerbody in an axial direction to accommodate thermal expansion. 3. The fuel nozzle according to claim 1 wherein said mid-mount position is generally equally spaced from each of said first and said second ends. 4. The fuel nozzle according to claim 1 including an inner air swirler mounted to an inner surface of said heat shield at one attachment interface and wherein said heat shield is fixed to said centerbody at another attachment interface comprising said mid-mount position which is axially spaced from said one attachment interface. 5. The fuel nozzle according to claim 1 wherein said outer surface of said heat shield is radially spaced apart from an inner surface of said centerbody to form an air gap that extends along a substantial length of said heat shield. 6. The fuel nozzle according to claim 1 wherein said heat shield includes a raised boss portion extending radially outwardly from said outer surface of said heat shield, said raised boss portion being directly attached said inner surface of said centerbody. 7. A fuel nozzle comprising: a centerbody having an inlet end and a discharge end for discharging an air/fuel mixture into a combustion chamber, said centerbody defining a central axis; a heat shield fixed to said centerbody at a first attachment interface between an outer surface of said heat shield and an inner surface of said centerbody, said first attachment interface being located at a mid-mount position, and wherein a first gap is formed between said inner and said outer surfaces on one side of said first attachment interface and a second gap is formed between said inner and said outer surface on an opposite side of said first attachment interface; and an inner air swirler fixed to said heat shield at a second attachment interface axially spaced from said first attachment interface in a direction along said central axis and wherein said first attachment interface is positioned axially between said second attachment interface and said discharge end of said centerbody. 8. The fuel nozzle according to claim 7 wherein said inner air swirler is fixed to an inner surface of said heat shield adjacent said first end to form said second attachment interface and with said outer surface of said heat shield being fixed to said centerbody at a centrally located position between said first and said second ends to form said first attachment interface at said mid-mount position. 9. The fuel nozzle according to claim 8 wherein said first and said second ends of said heat shield have slip fit interfaces with said centerbody to allow said heat shield to expand in an axial direction along said central axis. 10. The fuel nozzle according to claim 7 wherein said heat shield is fixed to said centerbody at said mid-mount position by brazing. 11. The fuel nozzle according to claim 7 wherein said heat shield has a first end adjacent said inlet end and a second end adjacent said discharge end, and wherein said first gap extends from said first attachment interface in an axial direction toward said first end and said second gap extends from said first attachment interface in an axial direction toward said second end. 12. The fuel nozzle according to claim 7 wherein said heat shield is only fixed to said centerbody at said mid-mount position. 13. A fuel nozzle comprising: a centerbody having an inlet end and a discharge end for discharging an air/fuel mixture into a combustion chamber, said centerbody defining a central axis; a heat shield fixed to said centerbody at a first attachment interface wherein said heat shield has a first end at said inlet end and a second end at said discharge end, and wherein an outer surface of said heat shield is radially spaced apart from an inner surface of said centerbody to form an air gap that extends along a substantial length of said heat shield; and an inner air swirler fixed to said heat shield at a second attachment interface axially spaced from said first attachment interface in a direction along said central axis with said inner air swirler being fixed to an inner surface of said heat shield adjacent said first end to form said second attachment interface and with said outer surface of said heat shield being fixed to said centerbody at centrally located position between said first and said second ends to form said first attachment interface, and wherein said first attachment interface is positioned axially between said second attachment interface and said discharge end of said centerbody. 14. A fuel nozzle comprising: a centerbody having an inlet end and a discharge end for discharging an air/fuel mixture into a combustion chamber, said centerbody defining a central axis; a heat shield fixed to said centerbody at a first attachment interface wherein said heat shield includes a raised boss portion extending radially outwardly from an outer surface of said heat shield, said raised boss portion being directly attached to an inner surface of said centerbody; and an inner air swirler fixed to said heat shield at a second attachment interface axially spaced from said first attachment interface in a direction along said central axis and wherein said first attachment interface is positioned axially between said second attachment interface and said discharge end of said centerbody. 15. A gas turbine engine comprising: a fan; a compressor; a turbine; and a combustion section including a plurality of fuel nozzles wherein each fuel nozzle includes a centerbody defining a central axis and having an inlet end and a discharge end for discharging an air/fuel mixture into a combustion chamber, a heat shield fixed to said centerbody at a first attachment interface, and an inner air swirler fixed to said heat shield at a second attachment interface axially spaced from said first attachment interface in a direction along said central axis, and wherein said first attachment interface is positioned axially between said second attachment interface and said discharge end of said centerbody, and wherein said first attachment interface is located at a mid-mount position between an outer surface of said heat shield and an inner surface of said centerbody, and wherein axially extending gaps are formed between said inner surface of said centerbody and said outer surface of said heat shield on opposing sides of said first attachment interface. 16. The gas turbine engine according to claim 15 wherein said heat shield has a first end at said inlet end and a second end at said discharge end with said inner air swirler being fixed to an inner surface of said heat shield adjacent said first end to form said second attachment interface, and with said outer surface of said heat shield being fixed to said centerbody at a centrally located position between said first and said second ends to form said first attachment interface at said mid-mount position. 17. The gas turbine engine according to claim 16 wherein said first and said second ends of said heat shield have slip fit interfaces with said centerbody to allow said heat shield to expand in an axial direction along said central axis. 18. The gas turbine engine according to claim 15 wherein said heat shield is only fixed to said centerbody at said mid-mount position such that first and second ends of said heat shield are movable relative to said centerbody in an axial direction to accommodate thermal expansion. 19. A gas turbine engine comprising: a fan; a compressor; a combustion section including a plurality of fuel nozzles wherein each fuel nozzle includes a centerbody defining a central axis and having an inlet end and a discharge end for discharging an air/fuel mixture into a combustion chamber, a heat shield fixed to said centerbody at a first attachment interface, and an inner air swirler fixed to said heat shield at a second attachment interface axially spaced from said first attachment interface in a direction along said central axis, and wherein said first attachment interface is positioned axially between said second attachment interface and said discharge end of said centerbody; and wherein said first and said second ends of said heat shield have slip fit interfaces with said centerbody to allow said heat shield to expand in an axial direction along said central axis, and wherein said outer surface of said heat shield is radially spaced apart from an inner surface of said centerbody to form an air gap that extends along a substantial length of said heat shield.

인용문헌 (8)

이 특허를 인용한 특허 (4)

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Mid-mount centerbody heat shield for turbine engine fuel nozzle

초록

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특허 상세정보

Mid-mount centerbody heat shield for turbine engine fuel nozzle

초록

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인용문헌 (8)

이 특허를 인용한 특허 (4)

IPC 상위 출원인

과제정보

상세정보조회

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IPC 상세정보(version : 201201)

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