Ventral segmented nozzles

Details Ventral segmented nozzles Ventral segmented nozzles

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/00 (2006.01) B64C 15/02 (2006.01) B64C 29/00 (2006.01)

Patent

CA 2009636

File No.: 159-033 CANADA Title: "VENTRAL SEGMENTED NOZZLES" Inventors: Joseph E. Farbridge Douglas Garland A. R. Schexnayder Brian E. Meyer Charles F. Ritchie ABSTRACT OF THE DISCLOSURE A thrust deflector system for VSTOL aircraft. The thrust directing system consists of a number of spaced-apart, downwardly facing openings along the bottom of the fuselage. The openings are fluidly connected with the outlet of the aircraft engine so that pressurized gas from the aircraft engine is discharged through the openings and away from the fuselage in discrete spaced-apart jets.

Affiliated with

Also associated with

Rating

Ventral segmented nozzles does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Ventral segmented nozzles, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ventral segmented nozzles will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1815378