guide vane material

(PDF) Material Selection Issues for a Nozzle Guide Vane Material Selection Issues for a Nozzle Guide Vane Against Service Induced Failure June 2016 DOI: 101115 guide vane material

guide vane material

  • (PDF) Material Selection Issues for a Nozzle Guide Vane

    Material Selection Issues for a Nozzle Guide Vane Against Service Induced Failure June 2016 DOI: 101115/GT201656120 Conference: ASME Turbo ExpoMaterial Selection Issues for a Nozzle Guide Vane Against ServiceInduced Failure Nozzle guide vanes (NGV) of gas turbine engines are the first components to withstand zle guide vane (withoutMaterial Selection Issues for a Nozzle Guide Vane AgainstThese material alloys are used in a large number of aerospace applications, from lightly loaded components to load carrying structures in aircrafts and aircraft enginesIJSER The choice of material for the outlet guide vane involves a wide range of considerations including manufacturing processes, material costs, and availabilityParametrics Investigation on Material selection for Outlet

  • Guide Vane an overview | ScienceDirect Topics

    Each guide vane should have two sharp edges that behave alternately as leading and trailing edges It is reasonable to adopt, as design conditions, inlet shockfree flow at the leading edges of the blades of both guide vane rows If potential flow is assumed, this means that the flow velocity is to remain finite at the sharp leading edgesEach guide vane should have two sharp edges that behave alternately as leading and trailing edges It is reasonable to adopt, as design conditions, inlet shockfree flow at the leading edges of the blades of both guide vane rows If potential flow is assumed, this means that the flow velocity is to remain finite at the sharp leading edgesGuide Vanes an overview | ScienceDirect Topicsa lightweight, cost effective, composite material fan exit guide vane design having satisfactory structural durability for commercial engine use Based on the results of a previous company supported program, eight graphite/epoxy and graphiteglass/epoxy guide vane designs were evaluated and four were selected for fabrication and testingc APPLICATION OF COMPOSITE MATERIALS TO

  • Material Selection Issues for a Nozzle Guide Vane Against

    Wu, X, Zhang, Z, Jiang, L, & Patnaik, P "Material Selection Issues for a Nozzle Guide Vane Against Service Induced Failure" Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and ExpositionChina Steel turbine blade and steel guide vane catalog of 14418 Forged Forging Hydro Turbine Blade, AISI S165m Forging Hydro Turbine Blade provided by China manufacturer Jiangyin Golden Machinery Equipment Co, Ltd, page1Steel turbine blade and steel guide vane Jiangyin GoldenAluminium Outlet Guide Vanes Outlet guide vane in the motor The outlet guide vane (OGV) has two different purposes: Forming a structural connection between the main engine carcass and the aircraft attachment point Steering the flow coming from the lowpressure turbine into the axial outflow, ie an aerodynamic objectiveAluminium Outlet Guide Vanes | Makino

  • Parametrics Investigation on Material selection for Outlet

    These material alloys are used in a large number of aerospace applications, from lightly loaded components to load carrying structures in aircrafts and aircraft enginesIJSER The choice of material for the outlet guide vane involves a wide range of considerations including manufacturing processes, material costs, and availabilityA composite material guide vane for a gas turbine engine, the composite material including fiber reinforcement densified by a matrix, the fiber reinforcement being formed as a single piece by threedimensional weaving and including an airfoil and at least two fastener flanges extending from a radial end of the vane towards opposite side faces of the airfoil, the fastener flanges being axiallyUSB2 Guide vane made from compositeWu, X, Zhang, Z, Jiang, L, & Patnaik, P "Material Selection Issues for a Nozzle Guide Vane Against Service Induced Failure" Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and ExpositionMaterial Selection Issues for a Nozzle Guide Vane Against

  • Material Selection Issues for a Nozzle Guide Vane Against

    Material Selection Issues for a Nozzle Guide Vane Against ServiceInduced Failure Xijia Wu, Xijia Wu National Research Council Canada, Ottawa, ON K1A 0R6, Canada The material selection scenarios are discussed with regards to damage accumulated during takeoff and cruise The interplay of those deformation mechanisms in the failure processEach guide vane should have two sharp edges that behave alternately as leading and trailing edges It is reasonable to adopt, as design conditions, inlet shockfree flow at the leading edges of the blades of both guide vane rows If potential flow is assumed, this means that the flow velocity is to remain finite at the sharp leading edgesGuide Vane an overview | ScienceDirect TopicsThe guide vane includes a cover portion including a first material and a core portion which is at least partially enclosed by the cover portion Inventors: Jansson, NiklasComposite guide vane GKN Aerospace Sweden AB

  • Failure mechanism of turbine guide vane and oxide

    The material of turbine guide vane The failed turbine guide vane used in this study is made by DZ40M superalloy DZ40M superalloy is a cobalt (Co)based directional solidified superalloy, which has high initial melting temperature and better fatigueApplication of composite materials to turbofan engine fan exit guide vanes A program was conducted by NASA with the JT9D engine manufacturer to develop a lightweight, cost effective, composite material fan exit guide vane design having satisfactory structural durability for commerical engine use Based on the results of a previous company supported program, eight graphite/epoxy and graphiteApplication of composite materials to turbofan engine fanThe blade described herein is primarily intended for use as a compressor inlet guide vane, experiencing service temperatures up to about 121°C (250°F) The composite construction is suitable for other vanes, and including solid, rotating blades, with appropriate changes in materialComposite inlet guide vane GEN ELECTRIC

  • WetReady™ Guide Vane ‐ A special guide vane for FGD

    on the vane surfaces WetReady™ Guide Vane ‐ A special guide vane for FGD Wet Stacks Figure 1: Droplets Passing Through Traditional Turning Vanes David K Anderson1, James Daniel1, Albert de Kreij2 1Alden Research Laboratory, Inc, Holden, MA, USA 2Hadek Protecve Systems, Roerdam, The NetherlandsA guide vane for a gas turbine engine, the guide vane including an airfoil made of composite material having fiber reinforcement densified by a matrix, the fiber reinforcement being obtained from preimpregnated long fibers agglomerated in the form of a mat, the airfoil being provided at least on a leading edge with a reinforcing strip, the reinforcing strip being made from a single strip ofUSA1 A guide vane made of compositeEach guide vane should have two sharp edges that behave alternately as leading and trailing edges It is reasonable to adopt, as design conditions, inlet shockfree flow at the leading edges of the blades of both guide vane rows If potential flow is assumed, this means that the flow velocity is to remain finite at the sharp leading edgesGuide Vane an overview | ScienceDirect Topics

  • Aluminium Outlet Guide Vanes | Makino

    Aluminium Outlet Guide Vanes Outlet guide vane in the motor The outlet guide vane (OGV) has two different purposes: Forming a structural connection between the main engine carcass and the aircraft attachment point Steering the flow coming from the lowpressure turbine into the axial outflow, ie an aerodynamic objectiveWu, X, Zhang, Z, Jiang, L, & Patnaik, P "Material Selection Issues for a Nozzle Guide Vane Against Service Induced Failure" Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and ExpositionMaterial Selection Issues for a Nozzle Guide Vane Againston the vane surfaces WetReady™ Guide Vane ‐ A special guide vane for FGD Wet Stacks Figure 1: Droplets Passing Through Traditional Turning Vanes David K Anderson1, James Daniel1, Albert de Kreij2 1Alden Research Laboratory, Inc, Holden, MA, USA 2Hadek Protecve Systems, Roerdam, The NetherlandsWetReady™ Guide Vane ‐ A special guide vane for FGD

  • Application of composite materials to turbofan engine fan

    Application of composite materials to turbofan engine fan exit guide vanes A program was conducted by NASA with the JT9D engine manufacturer to develop a lightweight, cost effective, composite material fan exit guide vane design having satisfactory structural durability for commerical engine use Based on the results of a previous company supported program, eight graphite/epoxy and graphiteThe material of turbine guide vane The failed turbine guide vane used in this study is made by DZ40M superalloy DZ40M superalloy is a cobalt (Co)based directional solidified superalloy, which has high initial melting temperature and better fatigueFailure mechanism of turbine guide vane and oxideThe material used for the shear pin, which is aluminum subjected to artificial aging, is supposed to be unsuitable for protecting the guide vane This article aims to design and analyze a failsafe mechanism using a shear pin for the guide vaneFailsafe design and analysis for the guide vane of a

  • Multiscale thermodynamic analysis method for 2D SiC/SiC

    The maximum equivalent stress is located at node 3256 near the trailing edge of the guide vane The local coordinate system number of this node is 1251 Different from the turbine guide vane of isotropic metal materials, that of the composite material is orthotropic The properties in normal and inplane directions are differentI claim: 1 A nozzle guide vane assembly for a gas turbine engine comprising: fixed engine structure; inner and outer platform rings, both of said inner and outer platform rings being made substantially entirely of a thin relatively flexible porous sheet material having tortuous passages therethrough whereby cooling air may pass through each of said rings from one surface to the other surfaceNozzle guide vane structure for a gas turbine engine