Aircraft propulsion system with flight maneuverable exhaust nozz

Details Aircraft propulsion system with flight maneuverable exhaust nozz Aircraft propulsion system with flight maneuverable exhaust nozz

1975-06-30

1976-10-19

Blix, Trygve M.

Aeronautics and astronautics

Aircraft, heavier-than-air

Airplane and fluid sustained

60261, 23926541, 244 52, B64C 1506

Patent

active

039866874

ABSTRACT:
An aircraft propulsion system is provided which incorporates a flight maneuverable exhaust nozzle. In one embodiment, gas turbine engines are mounted on both sides of an aircraft fuselage, each engine having an exhaust duct partially defining an exhaust stream flow path. The duct transists from a substantially cylindrical diffuser section aft of the engine to a relatively high aspect ratio section proximate the trailing edge of the wing. Exhaust gases are expelled through a thrust vectorable nozzle which is contoured within the wing and which is adapted to increase wing lift through the concept of supercirculation. Maximum aerodynamic advantage is achieved by distributing the exhaust flow over a significant portion of the wing span at the trailing edge. Thrust augmentation is provided through use of a long, flat duct burner disposed within the high aspect ratio section proximate the exhaust nozzle thereby minimizing turning losses and cooling air requirements. The exhaust nozzle includes an articulated deflector partially defining both the exhaust stream flow path and the wing upper surface. Synchronous movement of the two flaps comprising the deflector ensures proper internal area control prior to exhaust gas vectoring. The nozzle throat area is varied by a lower flap disposed in general opposition to the articulated deflector. Actuators are provided to vary the throat area and produce the proper thrust vector angle by positioning the lower flap and articulated deflector, respectively.

REFERENCES:
patent: 2420323 (1947-05-01), Meyer et al.
patent: 2479487 (1949-08-01), Goembel
patent: 2756008 (1956-07-01), Davidson
patent: 3148848 (1964-09-01), Price
patent: 3188803 (1965-06-01), Maguire
patent: 3658279 (1972-04-01), Robertson

Affiliated with

Also associated with

Rating

Aircraft propulsion system with flight maneuverable exhaust nozz does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft propulsion system with flight maneuverable exhaust nozz, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft propulsion system with flight maneuverable exhaust nozz will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-98350