JPS59163718U - Swirler in combustor - Google Patents

Swirler in combustor

Info

Publication number
JPS59163718U
JPS59163718U JP5748483U JP5748483U JPS59163718U JP S59163718 U JPS59163718 U JP S59163718U JP 5748483 U JP5748483 U JP 5748483U JP 5748483 U JP5748483 U JP 5748483U JP S59163718 U JPS59163718 U JP S59163718U
Authority
JP
Japan
Prior art keywords
swirler
combustor
blade
pass
fuel injection
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP5748483U
Other languages
Japanese (ja)
Inventor
「まん」代 重實
佐藤 亘男
Original Assignee
三菱重工業株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 三菱重工業株式会社 filed Critical 三菱重工業株式会社
Priority to JP5748483U priority Critical patent/JPS59163718U/en
Publication of JPS59163718U publication Critical patent/JPS59163718U/en
Pending legal-status Critical Current

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Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は従来のガスタービン燃焼器の要部の縦断面図、
第2図aは従来のスワーラの正面図、第2図すは従来の
スワーラの側面図、第3図は従来のスワーラによる空気
軌跡を示す概略図、第4図aは本考案の1実施例のスワ
ーラの正面図、第4図すは本考案の1実施例のスワーラ
6側面図、第5図は本考案のスワーラによる空気軌跡を
示す概略図である。。 1・・・燃料ノズル、2・・・スワーラ、3・・・翼、
4・・・循環流領域、5・・・前面部の領域。
Figure 1 is a longitudinal sectional view of the main parts of a conventional gas turbine combustor.
Fig. 2a is a front view of a conventional swirler, Fig. 2 is a side view of a conventional swirler, Fig. 3 is a schematic diagram showing an air trajectory by a conventional swirler, and Fig. 4a is an embodiment of the present invention. FIG. 4 is a side view of the swirler 6 of one embodiment of the present invention, and FIG. 5 is a schematic diagram showing the air trajectory by the swirler of the present invention. . 1... Fuel nozzle, 2... Swirler, 3... Wing,
4... Circulation flow area, 5... Front area.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃料噴射ノズルの外側に同心環状に配設されたスワーラ
において、同スワーラの翼を取付ける基準となる軸の延
長線が、スワーラ環の中心を通らないようにしたことを
特徴とする燃焼器におけるスワーラ。
A swirler in a combustor, characterized in that, in a swirler arranged in a concentric ring shape outside a fuel injection nozzle, an extension line of an axis on which a blade of the swirler is attached does not pass through the center of the swirler ring. .
JP5748483U 1983-04-19 1983-04-19 Swirler in combustor Pending JPS59163718U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5748483U JPS59163718U (en) 1983-04-19 1983-04-19 Swirler in combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5748483U JPS59163718U (en) 1983-04-19 1983-04-19 Swirler in combustor

Publications (1)

Publication Number Publication Date
JPS59163718U true JPS59163718U (en) 1984-11-02

Family

ID=30187784

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5748483U Pending JPS59163718U (en) 1983-04-19 1983-04-19 Swirler in combustor

Country Status (1)

Country Link
JP (1) JPS59163718U (en)

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