Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received in well or slot
Reexamination Certificate
2006-08-15
2006-08-15
Nguyen, Ninh H. (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
Specific working member mount
Blade received in well or slot
C416S20400A, C416S248000
Reexamination Certificate
active
07090468
ABSTRACT:
A fastening device for fastening moving blades to a disk of a turbomachine rotor includes moving-blade roots which have a mirror-symmetrical cross section with projections, axial disk slots holding the moving-blade roots in a positive-locking manner, and one riveted joint per moving blade for axially fixing the latter. Each blade root and the disk, in the region of each moving-blade root, have axial extensions. The extensions of moving blade and disk are opposite one another in pairs, in each case a hole lying in a radial plane relative to the disk axis is formed half in the extension of the moving blade and half in the extension of the disk. A rivet is inserted into each hole and fixed by plastic deformation.
REFERENCES:
patent: 4389161 (1983-06-01), Brumen
patent: 4444544 (1984-04-01), Rowley
patent: 5302086 (1994-04-01), Kulesa et al.
patent: 5445499 (1995-08-01), Charbonnel
patent: 5727927 (1998-03-01), Luxenburger
patent: 31 48 984 (1982-07-01), None
patent: 31 48 985 (1993-11-01), None
patent: 195 16 694 (1996-11-01), None
patent: 55017616 (1980-02-01), None
International Search Report.
Crowell & Moring LLP
MTU Aero Engines GmbH
Nguyen Ninh H.
LandOfFree
Fastening of moving turbomachine blades does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Fastening of moving turbomachine blades, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fastening of moving turbomachine blades will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3626902