Coolable airfoil structure

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, F01D 518

Patent

active

054624053

ABSTRACT:
A coolable airfoil having internal cooling passages 82, 84, 74 is disclosed. Various construction details are developed to increase cooling in critical locations of the airfoil. In one embodiment, a pair of side-by-side spanwisely extending passages 82, 84 flow cooling air to the tip passage 74 which extends rearwardly in a flag-like manner.

REFERENCES:
patent: 4278400 (1981-07-01), Yamarik et al.
patent: 4474532 (1984-10-01), Pazder
patent: 4752186 (1988-06-01), Liang
patent: 4753575 (1988-06-01), Levengood et al.
patent: 4992026 (1991-02-01), Ohtomo et al.
Drawing of the first stage turbine blade for the V-2500-A1 engine, International Aero Engines, 1991.

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

Coolable airfoil structure does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-1768479

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