JP2012202242A5 - - Google Patents

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Publication number
JP2012202242A5
JP2012202242A5 JP2011065223A JP2011065223A JP2012202242A5 JP 2012202242 A5 JP2012202242 A5 JP 2012202242A5 JP 2011065223 A JP2011065223 A JP 2011065223A JP 2011065223 A JP2011065223 A JP 2011065223A JP 2012202242 A5 JP2012202242 A5 JP 2012202242A5
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JP
Japan
Prior art keywords
exhaust
inner cylinder
strut
diffuser according
exhaust gas
Prior art date
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Granted
Application number
JP2011065223A
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Japanese (ja)
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JP2012202242A (en
JP5693315B2 (en
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Publication date
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Priority to JP2011065223A priority Critical patent/JP5693315B2/en
Priority claimed from JP2011065223A external-priority patent/JP5693315B2/en
Publication of JP2012202242A publication Critical patent/JP2012202242A/en
Publication of JP2012202242A5 publication Critical patent/JP2012202242A5/ja
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Publication of JP5693315B2 publication Critical patent/JP5693315B2/en
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Description

本発明の排気ディフューザにおいて、内筒の周方向の全域にわたって縮径する縮径部とすることができるが、ストラットが接合される部分及びその周囲にのみ縮径領域を形成した縮径部とすることができる。ストラットに当たった排気ガスの流れは、内筒の外周面などの壁面側に押しやられる。このため、ストラットの近くの領域は、内筒の外周面で排気ガスが剥離しにくい。そこで、ストラットと内筒との接合部分及びその周囲の領域だけを縮径させるものである。
本発明の排気ディフューザにおいて、縮径部は、傾斜角度を5〜15°の範囲とすることが好ましく、また、縮径部における内筒と外筒の間の排気流路の高さTとストラットの前縁から後縁に到る排気ガスが流れる方向の長さLの比(T/L)を、0.5〜2.0の範囲とする、ことが好ましい。
In the exhaust diffuser of the present invention, the reduced diameter portion can be reduced in diameter over the entire circumferential direction of the inner cylinder, but the reduced diameter portion is formed with a reduced diameter region only at the portion where the strut is joined and the periphery thereof. be able to. The flow of the exhaust gas hitting the strut is pushed to the wall surface side such as the outer peripheral surface of the inner cylinder. For this reason, in the area near the strut, the exhaust gas is difficult to peel off on the outer peripheral surface of the inner cylinder. Therefore, only the joint portion between the strut and the inner cylinder and the surrounding area are reduced in diameter.
In the exhaust diffuser of the present invention, the reduced diameter portion preferably has an inclination angle in the range of 5 to 15 °, and the height T of the exhaust flow path between the inner cylinder and the outer cylinder in the reduced diameter portion and the struts. It is preferable that the ratio (T / L) of the length L in the direction in which the exhaust gas from the leading edge to the trailing edge flows is in the range of 0.5 to 2.0.

Claims (6)

内筒と、
前記内筒の周囲に配置され、前記内筒との間に排気流路が形成される外筒と、
前記排気流路内に設けられ、内筒と外筒を繋ぐストラットと、を備え、
前記ストラットは、
前記排気流路を排気ガスが流れる方向の上流側に位置する前縁と、
前記排気ガスが流れる方向の下流側に位置する後縁と、を備え、
前記内筒は、
前記排気ガスが流れる方向の上流側の所定の開始位置から下流側の端部の終了位置にかけて径が縮径する縮径部、を備え、
前記前縁と前記開始位置、及び、前記後縁と前記終了位置、の各々が、前記排気ガスが流れる方向において一致するように設定されている、
ことを特徴とする排気ディフューザ。
An inner cylinder,
An outer cylinder disposed around the inner cylinder and having an exhaust passage formed between the inner cylinder;
A strut provided in the exhaust passage and connecting the inner cylinder and the outer cylinder;
The strut is
A leading edge located upstream of the exhaust gas flow direction in the exhaust flow path;
A rear edge located on the downstream side in the direction in which the exhaust gas flows, and
The inner cylinder is
A diameter-reducing portion whose diameter is reduced from a predetermined start position on the upstream side in the direction in which the exhaust gas flows to an end position on the downstream end,
Each of the front edge and the start position, and the rear edge and the end position are set to coincide with each other in a direction in which the exhaust gas flows.
Exhaust diffuser characterized by that.
前記ストラットは、
前記後縁が、前記外筒から前記内筒に向けて下降するように傾斜される、
請求項1に記載の排気ディフューザ。
The strut is
The trailing edge is inclined so as to descend from the outer cylinder toward the inner cylinder;
The exhaust diffuser according to claim 1.
前記縮径部は、
前記ストラットが接合される部分及びその周囲にのみ形成される、
請求項1又は2に記載の排気ディフューザ。
The reduced diameter portion is
Formed only at and around the part where the struts are joined,
The exhaust diffuser according to claim 1 or 2.
前記縮径部は、傾斜角度を5〜15°の範囲とする、The reduced diameter portion has an inclination angle in a range of 5 to 15 °.
請求項1〜請求項3のいずれか一項に記載の排気ディフューザ。The exhaust diffuser according to any one of claims 1 to 3.
前記縮径部における前記内筒と前記外筒の間の前記排気流路の高さTと前記ストラットの前記前縁から前記後縁に到る前記排気ガスが流れる方向の長さLの比(T/L)を、0.5〜2.0の範囲とする、A ratio of a height T of the exhaust passage between the inner cylinder and the outer cylinder in the reduced diameter portion and a length L in a direction in which the exhaust gas flows from the front edge to the rear edge of the strut ( T / L) is in the range of 0.5 to 2.0,
請求項1〜請求項4のいずれか一項に記載の排気ディフューザ。The exhaust diffuser according to any one of claims 1 to 4.
請求項1〜請求項5のいずれか一項に記載の排気ディフューザを備えることを特徴とするガスタービン。A gas turbine comprising the exhaust diffuser according to any one of claims 1 to 5.
JP2011065223A 2011-03-24 2011-03-24 Exhaust diffuser Active JP5693315B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2011065223A JP5693315B2 (en) 2011-03-24 2011-03-24 Exhaust diffuser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2011065223A JP5693315B2 (en) 2011-03-24 2011-03-24 Exhaust diffuser

Publications (3)

Publication Number Publication Date
JP2012202242A JP2012202242A (en) 2012-10-22
JP2012202242A5 true JP2012202242A5 (en) 2014-04-10
JP5693315B2 JP5693315B2 (en) 2015-04-01

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ID=47183517

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011065223A Active JP5693315B2 (en) 2011-03-24 2011-03-24 Exhaust diffuser

Country Status (1)

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JP (1) JP5693315B2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9611756B2 (en) * 2012-11-02 2017-04-04 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
JP6033154B2 (en) * 2013-03-29 2016-11-30 三菱重工業株式会社 Axial-flow rotating machine and diffuser
US10167782B2 (en) 2013-09-10 2019-01-01 Siemens Aktiengesellschaft Cooling air line for removing cooling air from a manhole of a gas turbine
US11274563B2 (en) * 2016-01-21 2022-03-15 General Electric Company Turbine rear frame for a turbine engine
WO2018124068A1 (en) 2016-12-26 2018-07-05 三菱重工業株式会社 Turbine and gas turbine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR807926A (en) * 1935-05-16 1937-01-25 Improvements in aircraft propulsion systems
US2809491A (en) * 1950-11-27 1957-10-15 Solar Aircraft Co Diffuser tailcone
JPS63100640U (en) * 1986-12-19 1988-06-30
EP0581978B1 (en) * 1992-08-03 1996-01-03 Asea Brown Boveri Ag Multi-zone diffuser for turbomachine
US7272930B2 (en) * 2003-09-25 2007-09-25 Siemens Power Generation Exhaust diffuser assembly with tunable velocity profile

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