Variable ratio bypass gas turbine engine with flow diverter

Details Variable ratio bypass gas turbine engine with flow diverter Variable ratio bypass gas turbine engine with flow diverter

1974-06-20

1976-08-03

Schwadron, Martin P.

Fluid handling

Systems

Dividing into parallel flow paths with recombining

137612, 415153A, 60226R, F16K 1100, F02K 3.04, F02K 312

Patent

active

039723496

ABSTRACT:
An inverter valve arrangement which comprises a fixed forward duct system having concentric annular passages at its inlet and a fixed after duct system having concentric annular passages at its outlet and each fixed system having selectively shaped adjacent portions which are circumferentially displaced and joined by a plurality of flapper valves. The flapper valves may be actuated so that either series or parallel flow will occur between the concentric annular passages of the systems.

REFERENCES:
patent: 760633 (1904-05-01), Kurzwernhart
patent: 1169448 (1916-01-01), Williams
patent: 1405900 (1922-02-01), Cassalette
patent: 2225071 (1940-12-01), Meyerhoofer
patent: 3147773 (1964-09-01), Matthews et al.
patent: 3319656 (1967-05-01), Reader
patent: 3331394 (1967-07-01), Hefler et al.
patent: 3680597 (1972-08-01), Obermaier
patent: 3779282 (1973-12-01), Klees
patent: 3792584 (1974-02-01), Klees
patent: 3841091 (1974-10-01), Sargisson

Affiliated with

Also associated with

Rating

Variable ratio bypass gas turbine engine with flow diverter does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Variable ratio bypass gas turbine engine with flow diverter, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Variable ratio bypass gas turbine engine with flow diverter will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1923408