Hybrid mixer for a high bypass ratio gas turbofan engine

Details Hybrid mixer for a high bypass ratio gas turbofan engine Hybrid mixer for a high bypass ratio gas turbofan engine

1976-11-01

1979-03-06

Garrett, Robert E.

Power plants

Reaction motor

Method of operation

60226R, 23926517, 181220, F02K 306

Patent

active

041423658

ABSTRACT:
A high bypass ratio gas turbofan engine provided with a hybrid mixer for mixing that portion of the bypass stream equivalent to a bypass ratio of substantially two with the core engine hot gas stream. The mixture is passed through a common exhaust nozzle.

REFERENCES:
patent: 2726091 (1973-04-01), Tontini
patent: 2979900 (1961-04-01), Hopper
patent: 3377804 (1968-04-01), Wright et al.
patent: 3436020 (1969-04-01), Duthion et al.
patent: 3664455 (1972-05-01), Duvvuri
patent: 3673803 (1972-07-01), MacDonald
Pearson, Journal of Royal Aeronautical Society, Sep., 1958, p. 662.

Affiliated with

Also associated with

Rating

Hybrid mixer for a high bypass ratio gas turbofan engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Hybrid mixer for a high bypass ratio gas turbofan engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Hybrid mixer for a high bypass ratio gas turbofan engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-915659