Variable nozzle for aeronautic gas turbine engine

Patent metadata

Field	Value
Publication number	US-9739164-B2
Application number	US-201514866127-A
Country	US
Kind code	B2
Filing date	Sep 25, 2015
Priority date	May 15, 2013
Publication date	Aug 22, 2017
Grant date	Aug 22, 2017

Abstract

A variable nozzle is comprised of: an exhaust duct vectoring a flow of the exhaust gas to the aft end; a plurality of primary flaps arranged to define a primary flow path converging toward the aft end, each of the primary flaps being swingably pivoted on the exhaust duct to regulate a degree of opening the primary flow path and including a first section and a second section forming an angle axially outward relative to the first section; and a plurality of secondary flaps arranged to define a secondary flow path in communication with the primary flow path, the secondary flow path being capable of divergent toward the aft end, the secondary flaps being respectively swingably pivoted on the second sections of the primary flaps to regulate a degree of opening the secondary flow path.

First claim

What is claimed is:

1. A variable nozzle used for ejecting exhaust gas of an aeronautic gas turbine engine along an axis from a fore end toward an aft end, comprising:
an exhaust duct vectoring a flow of the exhaust gas to the aft end;
a plurality of primary flaps arranged to define a primary flow path converging toward the aft end, each of the primary flaps being swingably pivoted on the exhaust duct to regulate a degree of opening of the primary flow path and each of the primary flaps including a first section and each of the primary flaps including a second section, wherein the first section and second section are linear and intersecting such that an angle of 132 degrees or greater and less than 180 degrees is formed between an outer surface of the first section and an outer surface of the second section, wherein an inner surface of the first section and an inner surface of the second section both define the primary flow path and are radially inwards of the outer surface of the first section and the outer surface of the second section respectively relative to the axis, the inner surface of the first section and the inner surface of the second section are linear and are connected continuously such that the inner surface of the first section is directly adjacent to the inner surface of the second section;
a plurality of secondary flaps arranged to define a secondary flow path in communication with the primary flow path, the secondary flow path being capable of divergent toward the aft end, the plurality of secondary flaps being respectively swingably pivoted on the second section of a corresponding primary flap of the plurality of primary flaps to regulate a degree of opening of the secondary flow path, wherein the first section and the second section in each of the primary flaps form a flexure and are immovable relative to each other; and

wherein the plurality of primary flaps is upstream of the plurality of secondary flaps.

2. The variable nozzle of claim 1 , wherein the first sections and the second sections are so dimensioned as to have the second sections divergent toward the aft end when the plurality of primary flaps swing to maximize the degree of opening of the primary flow path.

3. The variable nozzle of claim 1 , wherein the first sections and the second sections of each of the primary flaps are so dimensioned as to make each of the flexures between the first sections and the second sections act as a throat for the flow of the exhaust gas when the plurality of primary flaps swing to increase the degree of opening of the primary flow path.

4. The variable nozzle of claim 1 , further comprising:
a plurality of seals respectively in contact with the plurality of primary flaps and the plurality of secondary flaps to follow movement of the plurality of primary flaps and the plurality of secondary flaps so as to prevent the flow of the exhaust gas from leaking out.

5. The variable nozzle of claim 1 , wherein the second section of each of the primary flaps is substantially in line with a corresponding secondary flap of the plurality of secondary flaps.

6. The variable nozzle of claim 1 , further comprising a driver system for regulating the degree of opening of the primary flow path and the degree of opening of the secondary flow path, the driver system including an actuator, a ring structure, and a linkage, wherein the actuator is coupled to the ring structure, an internal surface of the ring structure slides on a back of one of the plurality of primary flaps, and the linkage is coupled with a backing structure of one of the plurality of secondary flaps such that movement of the linkage causes the one of the plurality of secondary flaps to pivot around a joint between one of the second sections and the one of the plurality of secondary flaps.

7. The variable nozzle according to claim 6 , wherein the back of the one of the primary flaps presents a cam follower structure which is arcuate, and movement of the ring structure on the cam follower structure causes the one of the plurality of primary flaps to pivot around a joint between the exhaust duct and the one of the plurality primary flaps.

8. The variable nozzle according to claim 6 , wherein the ring structure includes a roller.

Assignees

• Ihi Corp

Inventors

• Ooba Yoshinori
• Matsumoto Yuta
• Kimura Takehiko

Classifications

• F01D17/16 Primary

  by means of nozzle vanes · CPC title

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/55

  Seals · CPC title

• F02K1/1223 Primary

  of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series · CPC title