Laminated airfoil and method for turbomachinery

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415115, 416229A, 416231R, F01D 518

Patent

active

042215390

ABSTRACT:
Improved structure and method for an internally cooled, laminated stator or turbine blade for turbomachinery includes internal cooling passage configurations within each lamina which promote different forms of cooling of the internal or external surfaces of the blade.

REFERENCES:
patent: 2956773 (1960-10-01), French
patent: 3301526 (1967-01-01), Chamberlain
patent: 3515499 (1970-06-01), Beer et al.
patent: 3527543 (1970-09-01), Howald
patent: 3767322 (1973-10-01), Durgin et al.
patent: 3778183 (1973-12-01), Luscher et al.
patent: 3844678 (1974-10-01), Sterman et al.
patent: 3864058 (1975-02-01), Womack
patent: 3872563 (1975-03-01), Brown et al.
patent: 3891348 (1975-06-01), Auxier
patent: 4040767 (1977-08-01), Dierberger et al.
patent: 4056332 (1977-11-01), Meloni

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Laminated airfoil and method for turbomachinery does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Laminated airfoil and method for turbomachinery, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Laminated airfoil and method for turbomachinery will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2222752

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.