The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Mar. 20, 1984
Filed:
Aug. 19, 1982
Ira W Reese, Trenton, NJ (US);
Nello B Compagnucci, Yardville, NJ (US);
Transamerica DeLaval Inc., Princeton, NJ (US);
Abstract
The invention contemplates a technique and machine for completing the assembly of a turbine-rotor stage by precision-peening blade tenons to secure shroud segments to successive blades. In the machine, a turbine-rotor assembly of multiple stages of blades on a rotor shaft is mounted on a horizontal axis, with provision for indexing successive blade tenons of a given-stage into precise horizontal confrontation with tool elements successively presented to the tenon, the tool elements being independently mounted to a compound-axis slide system. A presser foot carried by the slide system locally holds the shroud segment to a seated position against the blade to be secured, while first an induction-heating element and then a riveting tool perform in programmed sequence upon the exposed end of the involved tenon. The compound action of the slide system enables (a) reciprocated horizontal displacement of the tools in and out of operating position, tool action being on a horizontal axis of symmetry which geometrically intersects the turbine-rotor axis, while operating upon the blades of a first turbine stage, and (b) orthogonal offsetting displacement of the slide system and its tools, in order to proceed with a succession of similar shroud-riveting operations at a succeeding stage of the rotor.