[특허]Turbine blade assembly with pin dampers

The Boeing Company

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특허 상세정보

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Turbine blade assembly with pin dampers

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F04D-005/26
미국특허분류(USC)	416/230; 416/229.A; 416/500
출원번호	US-0120584 (2002-04-11)
발명자 / 주소	Davis, Gary A. Tuttle, Gary E.
출원인 / 주소	The Boeing Company
대리인 / 주소	Black Lowe & Graham
인용정보	피인용 횟수 : 6 인용 특허 : 8

초록

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A turbine blade assembly for a turbine assembly includes a turbine blade having a turbine blade damper cavity formed therein and a plurality of pins positioned within the turbine blade damper cavity. The pins are maintained in the damper cavity during operation of the turbine blade assembly. They reduce vibration of the turbine blade assembly during operation by dissipating energy by friction between adjacent pins and between the pins and the internal surface of the blade that defines the damper cavity. id rotational axis and a surface portion formed by extending said opening to a direction parallel said rotational axis so that every part of said surface portions is accessible from said direction; said surface portion of said connecting channel has a peripheral surface extending from said opening parallel to said rotational axis and curved radially inwardly toward said rotational axis, and a pair of opposing surfaces extended parallel to said rotational axis and positioned on opposite sides of said peripheral surface; and a connecting portion of said peripheral and opposing surfaces is curved. 8. A device in accordance with claim 7, wherein said curved connecting portion has a radius curvature of 0.1 mm or more. 9. The air-driven rotating and cutting device according to claim 1, wherein a peripheral region in which said connecting channels are formed is greater than that in which an inlet through which said air is ejected against said first blades exists. 10. A device in accordance with claim 9, wherein said peripheral region of said connecting channels is extended in an entire peripheral area of said housing. 11. A device in accordance with claim 9, wherein said peripheral region in which said connecting channels are formed includes a first region in which said inlet through which said air is ejected against said first blades and a second region outside said first region, wherein a surface portion of said connecting channel has a peripheral surface extending from said opening parallel to said rotational axis and curved radially inwardly toward said rotational axis, and a pair of opposing surfaces extended parallel to said rotational axis and positioned on opposite sides of said peripheral surface, and wherein each of said opposing surfaces in said first region defines a first angle with a line that crosses said rotational axis and each of said opposing surfaces in said second region defines a second angle with said line, said second angle being different from said first angle. 12. A device in accordance with claim 9, wherein said peripheral region in which said connecting channels are formed includes a first region including said inlet through which said air is ejected against said first blades and a second region outside said first region, wherein said surface portion of said connecting channel has a peripheral surface extending from said opening parallel to said rotational axis and curved radially inwardly toward said rotational axis, and a pair opposing surfaces extended parallel to said rotational axis and positioned on opposite sides of said peripheral surface, and wherein each of said opposing surfaces in said first region is directed so that a line extended inwardly from an innermost end thereof toward said rotational axis defines a first angle with a tangential line extending in a rotational direction of said rotor from said innermost end, and each of said opposing surfaces in said second region is directed so that a line extended inwardly from an innermost end thereof toward said rotational axis defines a second angle with a tangential line extending in a rotational direction of said rotor from said innermost end, said second angle being greater than said first angle. 13. An air-driven rotating and cutting device, comprising: a rotor having an annular hub extending around a rotational axis of said rotor and detachably holding a cutting tool in said annular hub, said hub being farmed with first and second turbine wheels, said first and second turbine wheels being formed with first and second blades, respectively, each of said first blades defining a first channel wit adjacent first blade therebetween and each of said second blade defining a second channel with adjacent second blade therebetween, each of said second blades being extended parallel to said rotational axis; and a housing having a cylindrical casing made from a single member for receiving said rotor for rotation about said rotat ional axis, said casing having channels for fluidly connecting said first and second channels, so that an air is guided from said first channels through said connecting channels to said second channels to rotate said rotor, wherein each of said connecting channels is defined by an opening opened toward a direction parallel to said rotational axis and a surface portion formed by extending said opening to a direction parallel to said rotational axis so that every part of said surface portions is accessible from said direction. 14. An air-driven rotating and cutting device, comprising: a rotor having an annular hub extending around a rotational axis of said rotor and detachably holding a cutting tool in said annular hub, said hub being formed with first and second turbine wheels, said first and second turbine wheels being formed with first and second blades, respectively, each of said first blades defining a first channel with adjacent first blade therebetween and each of said second blade defining a second channel with adjacent second blade therebetween, said second turbine blades being formed in one end surface of said annular hub; and a housing having a cylindrical casing made from a single member for receiving said rotor for rotation about said rotational axis, said casing having channels for fluidly connecting said first and second channels, so that an air is guided from said first channels through said connecting channels to said second channels to rotate said rotor, wherein each of said connecting channels is defined by an opening opened toward a direction parallel to said rotational axis and a surface portion formed by extending said opening to a direction parallel to said rotational axis so that every part of said surface portions is accessible from said direction. 15. An air-driven rotating and cutting device, comprising: a rotor having an annular hub extending around a rotational axis of said rotor and detachably holding a cutting tool in said annular hub, said hub being formed with first and second turbine wheels, said first and second turbine wheels being formed with first and second blades, respectively, each of said first blades defining a first channel with adjacent first blade therebetween and each of said second blade defining a second channel with adjacent second blade therebetween, said second turbine blades being formed in one end surface of said annular hub; and a housing having a cylindrical casing made from a single member for receiving said rotor for rotation about said rotational axis, said casing having channels for fluidly connecting said first and second channels, so that an air is guided from said first channels through said connecting channels to said second channels to rotate said rotor, wherein each of said connecting channels is defined by an opening opened toward a direction parallel to said rotational axis and a surface portion formed by extending said opening to a direction parallel to said rotational axis so that every part of said surface portions is accessible from said direction; and each of said second channels is opened at inward and outward ends thereof. 16. An air-driven rotating and cutting device, comprising: a rotor having a rotational axis and detachably holding a cutting tool along said rotational axis, said rotor being formed with first and second turbine wheels, said first and second turbine wheels being formed with first and second channels, respectively; and a head having a housing portion and a coupling portion, wherein said housing portion having a cylindrical casing made from a single member for receiving said rotor for rotation about said rotational axis, said casing having channels for fluidly connecting said first and second channels, so tat an air is guided from said first channels through said connecting channels to said second channels to rotate said rotor, wherein each of said connecting channels is defined by an opening opened toward a directi on parallel to said rotational axis and a surface portion formed by extending said opening to a direction parallel to said rotational axis so that every part of said surface portions is accessible from said direction, and wherein said coupling portion having a main air supply passage extending parallel to a central axis of said coupling portion and nozzles fluidly connected with said main air supply passage so that said air supplied from said main air supply passage is ejected to said first turbine wheel in a direction perpendicular to said rotational axis of said rotor. 17. A device in accordance with claim 16, wherein said coupling portion of said head further comprises one or more intermediate passages for connecting between said main air supply passage and said nozzles. 18. A device in accordance with claim 17, wherein an effective cross sectional area of said intermediate passages is greater than that of said nozzles. 19. A device in accordance with claim 17, wherein each of said nozzles has a portion where a cross sectional area thereof is reduced. 20. A device in accordance with claim 19, wherein said reduced portion is tapered. 21. A device in accordance wit claim 19, wherein said nozzles are positioned so that each of said nozzle defines a greater angle with said central axis of said coupling portion than another nozzle located on a downstream side with respect to a rotational direction of said rotor. e integral rings thereon for coupling the chandelier thereto and a passage therethrough for electrical wires. 11. The chandelier adaptor defined in claim 10 wherein said upper end is internally threaded for screwing onto the end of the stationary switch box mounting shaft of an existing fan. 12. The chandelier adaptor defined in claim 10 wherein said chandelier adaptor includes a replacement switch box cover adapted to be secured to an existing switch box and having an aperture for said chandelier adaptor. 13. The chandelier adaptor defined in claim 10 wherein said chandelier adaptor is mounted to the switch box of an existing fan.

이 특허에 인용된 특허 (8)

이 특허를 인용한 특허 피인용횟수: 6

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The Boeing Company (1)

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Turbine blade assembly with pin dampers

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Turbine blade assembly with pin dampers

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이 특허에 인용된 특허 (8)

이 특허를 인용한 특허 피인용횟수: 6

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