Turbine engine rotor blade platform seal

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416193A, F01D 518

Patent

active

055139558

ABSTRACT:
An apparatus for sealing a gap between adjacent blades in a rotor assembly for a gas turbine engine is provided. The rotor assembly includes a plurality of blades circumferentially disposed around a disc. Each of the blades includes an airfoil, a root, and a platform extending outward in a lateral direction in a transition area between the root and the airfoil. The disc includes a plurality of complementary recesses circumferentially distributed around the disc for receiving the blade roots. The gaps are formed between edges of adjacent platforms. The platforms collectively form a flow path for primary fluid flow passing by the airfoil side of the platforms and secondary fluid flow passing by the root side of the platforms. The apparatus comprises a thin plate body and apparatus for conducting secondary flow between the thin plate body and root side surfaces of adjacent blade platforms, and thereafter into the gap. The secondary flow traveling between the thin plate body and the root side surfaces transfers thermal energy away from the platforms.

REFERENCES:
patent: 3112915 (1963-12-01), Morris
patent: 3266770 (1966-08-01), Harlow
patent: 3610778 (1971-10-01), Suter
patent: 3666376 (1972-05-01), Damlis
patent: 3709631 (1973-01-01), Karstensen et al.
patent: 3751183 (1973-08-01), Nichols et al.
patent: 3887298 (1975-06-01), Hess et al.
patent: 4182598 (1980-01-01), Nelson
patent: 4280795 (1981-07-01), Trousdell
patent: 4347040 (1982-08-01), Jones et al.
patent: 4422827 (1983-12-01), Buxe et al.
patent: 4455122 (1984-06-01), Schwarzmann et al.
patent: 4494909 (1985-01-01), Forestier
patent: 4505642 (1985-03-01), Hill
patent: 4568247 (1986-02-01), Jones et al.
patent: 4872810 (1989-10-01), Brown et al.
patent: 4872812 (1989-10-01), Hendley et al.
patent: 5261790 (1993-11-01), Dietz et al.
patent: 5281097 (1994-01-01), Wilson et al.
patent: 5302085 (1994-04-01), Dietz et al.
patent: 5313786 (1994-05-01), Chlus et al.
patent: 5415526 (1995-05-01), Mercadante et al.

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

Turbine engine rotor blade platform seal does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbine engine rotor blade platform seal, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine engine rotor blade platform seal will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1222735

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