JPS6158572U - - Google Patents

Info

Publication number
JPS6158572U
JPS6158572U JP14259784U JP14259784U JPS6158572U JP S6158572 U JPS6158572 U JP S6158572U JP 14259784 U JP14259784 U JP 14259784U JP 14259784 U JP14259784 U JP 14259784U JP S6158572 U JPS6158572 U JP S6158572U
Authority
JP
Japan
Prior art keywords
inner cylinder
ring
outer periphery
gas turbine
combustor
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
JP14259784U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP14259784U priority Critical patent/JPS6158572U/ja
Publication of JPS6158572U publication Critical patent/JPS6158572U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Description

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

第1図は本考案の第1の実施例の全体の断面図
、第2図は第1図の要部拡大平面図、第3図は第
2図の斜視図、第4図は本考案の第2の実施例の
要部断面図、第5図は従来例の断面図を示す。 1……円筒、2……スクロール、12……段差
面、13……リング、14……スリツト。
Fig. 1 is an overall sectional view of the first embodiment of the present invention, Fig. 2 is an enlarged plan view of the main part of Fig. 1, Fig. 3 is a perspective view of Fig. 2, and Fig. 4 is a cross-sectional view of the first embodiment of the present invention. A sectional view of a main part of the second embodiment, and FIG. 5 shows a sectional view of a conventional example. 1...Cylinder, 2...Scroll, 12...Step surface, 13...Ring, 14...Slit.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 逆流缶形燃焼器の内筒と、タービン入口に連通
する通路とを連結するガスタービンにおいて、軸
方向に多数のスリツトを有し、かつ、段差面を有
するリングを該内筒の端部外周に固着し、該リン
グを介して該内筒の外周と該通路との内周とを摺
動自在に連結嵌合させたことを特徴とするガスタ
ービンの燃焼器。
In a gas turbine that connects an inner cylinder of a counterflow can type combustor and a passage communicating with a turbine inlet, a ring having a large number of slits in the axial direction and a stepped surface is attached to the outer periphery of the end of the inner cylinder. A combustor for a gas turbine, characterized in that the outer periphery of the inner cylinder and the inner periphery of the passage are slidably connected and fitted through the ring.
JP14259784U 1984-09-19 1984-09-19 Pending JPS6158572U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14259784U JPS6158572U (en) 1984-09-19 1984-09-19

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14259784U JPS6158572U (en) 1984-09-19 1984-09-19

Publications (1)

Publication Number Publication Date
JPS6158572U true JPS6158572U (en) 1986-04-19

Family

ID=30700913

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14259784U Pending JPS6158572U (en) 1984-09-19 1984-09-19

Country Status (1)

Country Link
JP (1) JPS6158572U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007212126A (en) * 2006-02-08 2007-08-23 Snecma Turbomachine combustion chamber
FR3045137A1 (en) * 2015-12-11 2017-06-16 Snecma TURBOMACHINE COMBUSTION CHAMBER

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007212126A (en) * 2006-02-08 2007-08-23 Snecma Turbomachine combustion chamber
FR3045137A1 (en) * 2015-12-11 2017-06-16 Snecma TURBOMACHINE COMBUSTION CHAMBER

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