AIRFOIL PART PROFILE FOR COMPRESSOR

PROBLEM TO BE SOLVED: To provide an airfoil part profile for a manufactured article, i.e., a compressor. SOLUTION: The manufactured article has a reference contour substantially following the values of the Cartesian coordinates of X, Y, Z in table 1 (not shown). In table 1 (not shown), X and Y indic...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	LAMASTER CHRISTOPHER, TOMBERG STEVEN E, MICHENFELDER JENNIFER B
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL 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 WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide an airfoil part profile for a manufactured article, i.e., a compressor. SOLUTION: The manufactured article has a reference contour substantially following the values of the Cartesian coordinates of X, Y, Z in table 1 (not shown). In table 1 (not shown), X and Y indicate distances in inches forming airfoil part profile sections at every distance Z in inches when connected with a smooth continuous circular arc. The profile sections at the distance Z are smoothly connected to one another to form a complete airfoil part profile 22 or 23. COPYRIGHT: (C)2008,JPO&INPIT