Cooling system for the trailing edge region of a hollow gas turb

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

F01D 518

Patent

active

06056508&

ABSTRACT:
In a cooling system for the trailing edge region of a hollow gas turbine blade, there extends from the blade root (1) to the blade tip (2) a duct (3) through which the flow passes longitudinally and which, in the region of the blade body (4), is delimited by the inner walls of the trailing edge (5), the suction side (6) and the pressure side (7) and by a web (9), the inner walls of the suction side and of the pressure side being provided with a plurality of ribs (8) running at least approximately parallel. The ribs (8) run obliquely from the web (9) in the direction of the trailing edge (5) and are directed radially outward on at least one of the two inner walls. The suction-side ribs and the pressure-side ribs are offset relative to one another over the blade height. The ratio of the height (h) of the ribs (8) to the local height (H) of the duct (4) is constant over the longitudinal extent of the ribs.

REFERENCES:
patent: 3806274 (1974-04-01), Moore
patent: 4474532 (1984-10-01), Pazder
patent: 5002460 (1991-03-01), Lee et al.
patent: 5232343 (1993-08-01), Butts
patent: 5488825 (1996-02-01), Davis et al.
patent: 5536143 (1996-07-01), Jacala et al.
patent: 5634766 (1997-06-01), Cunha et al.
patent: 5695322 (1997-12-01), Jacobson et al.
"Augmented Heat Transfer in Triangular Ducts with Full and Partial Ribbed Walls", Zhang, et al., Journal of Thermophysics and Heat Transfer, vol. 8, No. 3, Jul.-Sep. 1994, pp. 574-579.
"Experimental Study of the Effects of Bleed Holes on Heat Transfer and Pressure Drop in Trapezoidal Passages with Tapered Turbulators", et al., May 24-27, 1993 Presentation at Gas Turbine and Aeroengine Congress and Exposition.

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

Cooling system for the trailing edge region of a hollow gas turb does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Cooling system for the trailing edge region of a hollow gas turb, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling system for the trailing edge region of a hollow gas turb will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1589602

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