APPARATUS FOR FABRICATING ROTOR ASSEMBLY
PROBLEM TO BE SOLVED: To provide a rotor assembly capable of reducing a high load in the radial direction and an influence of a vibration response of an airfoil caused by a dynamic response of a blade when the tip of the airfoil hits against an abrasive casing and friction is generated. SOLUTION: Th...
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| creator | SINHA SUNIL KUMAR CORNELL JAY L SCHNEIDER MICHAEL HARVEY RUEHR WILLIAM CARL |
| description | PROBLEM TO BE SOLVED: To provide a rotor assembly capable of reducing a high load in the radial direction and an influence of a vibration response of an airfoil caused by a dynamic response of a blade when the tip of the airfoil hits against an abrasive casing and friction is generated. SOLUTION: The airfoil 42 includes: a first sidewall 44; a second sidewall 46 connected to the first sidewall at a leading edge 48 and a trailing edge 50; a root 54; and an end 60 obliquely extending between the first and second sidewalls by forming an angle facilitating the reduction of a load in the radial direction generated to the airfoil during end friction. COPYRIGHT: (C)2008,JPO&INPIT |
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SOLUTION: The airfoil 42 includes: a first sidewall 44; a second sidewall 46 connected to the first sidewall at a leading edge 48 and a trailing edge 50; a root 54; and an end 60 obliquely extending between the first and second sidewalls by forming an angle facilitating the reduction of a load in the radial direction generated to the airfoil during end friction. 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SOLUTION: The airfoil 42 includes: a first sidewall 44; a second sidewall 46 connected to the first sidewall at a leading edge 48 and a trailing edge 50; a root 54; and an end 60 obliquely extending between the first and second sidewalls by forming an angle facilitating the reduction of a load in the radial direction generated to the airfoil during end friction. 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SOLUTION: The airfoil 42 includes: a first sidewall 44; a second sidewall 46 connected to the first sidewall at a leading edge 48 and a trailing edge 50; a root 54; and an end 60 obliquely extending between the first and second sidewalls by forming an angle facilitating the reduction of a load in the radial direction generated to the airfoil during end friction. COPYRIGHT: (C)2008,JPO&INPIT</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | BLASTING ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS WEAPONS |
| title | APPARATUS FOR FABRICATING ROTOR ASSEMBLY |
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