Rotor blade for gas turbine engines

Details Rotor blade for gas turbine engines Rotor blade for gas turbine engines

1975-09-30

1983-11-08

Schafer, Richard E.

Fluid reaction surfaces (i.e., impellers)

With heating, cooling or thermal insulation means

Changing state mass within or fluid flow through working...

416 97R, F01D 518

Patent

active

044139497

ABSTRACT:
A turbine blade for a gas turbine engine has a hollow aerofoil and a root. A first insert for the distribution of cooling air in the aerofoil is inserted thereinto through an opening in the root but due to the relatively high camber of the blade the insert is such that it has to be displaced laterally after insertion. A second insert, also inserted through the opening, is provided to secure the first insert in position and to guide the cooling air from the opening to the first insert.

REFERENCES:
patent: 2780435 (1957-02-01), Jackson
patent: 2873944 (1959-02-01), Wiese et al.

Affiliated with

Also associated with

Rating

Rotor blade for gas turbine engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Rotor blade for gas turbine engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotor blade for gas turbine engines will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2005631