Nozzle ring for a gas turbine and method of manufacture thereof

Details Nozzle ring for a gas turbine and method of manufacture thereof Nozzle ring for a gas turbine and method of manufacture thereof

1999-03-29

2000-09-19

Cuda, Irene

Metal working

Method of mechanical manufacture

Impeller making

2988921, B21D 5378

Patent

active

061193399

ABSTRACT:
A worked nozzle ring for a gas turbine, in particular an aircraft engine, having at least one shroud and at least one blade sheet arranged thereon, whereby in order to create a worked nozzle ring that is easy to manufacture, the blade sheet comprises, at the frontal side, at least one two-dimensionally profiled connecting space region that is placed in a profiled opening formed in the shroud by means of beam cutting and is connected therewith.

REFERENCES:
patent: 4827588 (1989-05-01), Meyer
patent: 5031288 (1991-07-01), Sadler
patent: 5174715 (1992-12-01), Martin
patent: 5697152 (1997-12-01), Yamazaki et al.
patent: 5788456 (1998-08-01), Maier

Affiliated with

Also associated with

Rating

Nozzle ring for a gas turbine and method of manufacture thereof does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Nozzle ring for a gas turbine and method of manufacture thereof, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Nozzle ring for a gas turbine and method of manufacture thereof will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1059661