Variable jet engine outlet with a mainly circle sector-formed cross section

Patent metadata

Field	Value
Publication number	US-9341141-B2
Application number	US-201114123379-A
Country	US
Kind code	B2
Filing date	Jun 17, 2011
Priority date	Jun 17, 2011
Publication date	May 17, 2016
Grant date	May 17, 2016

Abstract

The present invention relates to a low signature jet engine outlet comprising movable border segments forming at least one circular arc and being movable radially for controlling the form and area of the outlet, at least one stationary border element for defining the form and area of the outlet, and movable coupling means for connecting the at least one circular arc to the at least one stationary border element. The coupling means are movable along a connection part of the at least one stationary border element, and the connection part of the at least one stationary border element is substantially flat and extending in a substantially radial direction of the at least one circular arc.

First claim

The invention claimed is:

1. A jet engine outlet ( 1 ) comprising:
movable border segments ( 3 ) forming at least one substantially part-circular arc ( 29 ) and being movable radially for controlling the form and area of the outlet ( 1 );
at least one stationary border element ( 27 ) for defining the form and area of the outlet ( 1 ); and
at least one movable coupling ( 31 ) for connecting the at least one substantially part-circular arc ( 29 ) to the at least one stationary border element ( 27 ),
wherein:
the at least one substantially part-circular arc is centered about at least one arc centerline that is proximate to an engine centerline;
the at least one movable coupling ( 31 ) is movable along a connection part ( 45 ) of the at least one stationary border element ( 27 ); and
the connection part ( 45 ) of the at least one stationary border element ( 27 ) is substantially flat and extending in a substantially radial direction of the at least one substantially part-circular arc ( 29 ); and
the at least one stationary border element and the at least one substantially part-circular arc together form a non-circular outlet shape at a cross-section through an axial plane of the outlet.

2. A jet engine outlet according to claim 1 , wherein:
the movable border segments ( 3 ) and the at least one movable coupling ( 31 ) is hingedly connected to a fixed part ( 13 ) of the outlet ( 1 );
the movable border segments ( 3 ) are moved by means of a pressure inducing means ( 19 ) affecting the movable border segments ( 3 ); and
the at least one movable coupling ( 31 ) is moved by means of a linkage system ( 23 ).

3. A jet engine outlet according to claim 1 , wherein the at least one movable coupling ( 31 ) is formed as an oblong segment that is bent approximately 90° in a lengthwise direction to fit tightly to the connection part ( 45 ) of the at least one stationary border element ( 27 ) and to the adjacent movable border segments ( 3 ).

4. A jet engine outlet according to claim 1 , wherein the at least one movable coupling ( 31 ) comprises:
an upper part ( 31 c ) positioned on one side of the at least one stationary border element;
a lower part ( 31 d ) positioned on the other side of the at least one stationary border element; and
at least one connection element ( 41 ) for connecting the upper part ( 31 c ) with the lower part ( 31 d ),
wherein the at least one movable coupling ( 31 ) is movable in a guide channel ( 43 ) in the at least one stationary border element ( 27 ).

5. A jet engine outlet according to claim 1 , wherein the at least one stationary border element ( 27 ) is a part of the aircraft fuselage.

6. A jet engine outlet according to claim 1 , wherein the at least one stationary border element ( 27 ) is protruding rear of the substantially part-circular arc ( 29 ).

7. A jet engine outlet according to claim 1 , wherein stabilizers ( 37 ) are provided on both sides of the outlet ( 1 ).

8. A jet engine outlet according to claim 1 , wherein the outlet is shielded by two structure elements ( 59 ) provided on each side of the outlet.

9. A jet engine outlet according to claim 1 , wherein the movable border segments ( 3 ) form a semicircle.

10. A jet engine outlet according to claim 9 , wherein the at least one stationary border element ( 27 ) is substantially flat.

11. A jet engine outlet according to claim 1 , wherein the at least one substantially part-circular arc ( 29 ) comprises two substantially part-circular arcs ( 29 ), the two substantially part-circular arcs ( 29 ) being located symmetrically on a vertical axis one above the other and with the concave sides of the two substantially part-circular arcs ( 29 ) being directed towards each other.

Assignees

• Bjerkemo Jakob
• Saab Ab

Inventors

• Bjerkemo Jakob

Classifications

• F02K1/80

  Couplings or connections · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F02K1/123 Primary

  of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure · CPC title

• F02K1/822

  Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic