Turbine rotor blades

Details Turbine rotor blades Turbine rotor blades

1997-03-25

2000-11-07

Ryznic, John E.

Fluid reaction surfaces (i.e., impellers)

Specific blade structure

Irregular, flanged or channel forming blade surface

416236A, 4151731, 4151735, 415914, B63H 126, F01D 514

Patent

active

06142739&

ABSTRACT:
An unshrouded turbine rotor blade 24 for use particularly in gas turbine engines comprising an aerofoil 30 having a leading edge 32 and a trailing edge 34. The radially outer extremity of the aerofoil 30 having a passage 42 defined by a peripheral wall 44. An aperture is formed within the wall 44 in the proximity of the trailing edge 32 of the aerofoil portion 30. The walled passage 42 is provided to capture and retain air or gas flowing over the tip of the aerofoil 30 and redirect the flow through the aperture 46 at the trailing edge of the aerofoil 30.

REFERENCES:
patent: 4519745 (1985-05-01), Rosman et al.
patent: 4526512 (1985-07-01), Hook
patent: 4761116 (1988-08-01), Braddy et al.
patent: 4893987 (1990-01-01), Lee et al.
patent: 4896122 (1990-01-01), Tahernia et al.
patent: 5503527 (1996-04-01), Lee et al.
patent: 5564902 (1996-10-01), Tomita
patent: 5688107 (1997-11-01), Downs et al.

Affiliated with

Also associated with

Rating

Turbine rotor 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 Turbine rotor blades, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine rotor blades will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1635122