Blow-off device for a bypass gas turbine engine

Details Blow-off device for a bypass gas turbine engine Blow-off device for a bypass gas turbine engine

1990-06-29

1992-06-09

Bertsch, Richard A.

Power plants

Reaction motor

Interrelated reaction motors

60 3929, F02C 700, F02K 306

Patent

active

051196255

ABSTRACT:
A blow-off device for a gas turbine bypass engine having a primary air flow path separated from an outer secondary air flow path by a partition includes a plurality of discharge passages passing through the partition from the primary air flow path to the secondary air flow path, each of the discharge passages having a first hinged flap in the outer wall of the primary air flow path, a second hinged flap in the inner wall of the secondary air flow path, and a connecting rod mechanically interlinking the first and second flaps, the connecting rod being hinged at one of its end to the first flap and at its other end to the second flap.

REFERENCES:
patent: 3638428 (1972-02-01), Shipley et al.

Affiliated with

Also associated with

Rating

Blow-off device for a bypass gas turbine 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 Blow-off device for a bypass gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Blow-off device for a bypass gas turbine engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1796165