JPH0272332U - - Google Patents

Info

Publication number
JPH0272332U
JPH0272332U JP14963888U JP14963888U JPH0272332U JP H0272332 U JPH0272332 U JP H0272332U JP 14963888 U JP14963888 U JP 14963888U JP 14963888 U JP14963888 U JP 14963888U JP H0272332 U JPH0272332 U JP H0272332U
Authority
JP
Japan
Prior art keywords
duct
inner cylinder
turbine
power turbine
partition plate
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.)
Granted
Application number
JP14963888U
Other languages
Japanese (ja)
Other versions
JPH0622123Y2 (en
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 JP14963888U priority Critical patent/JPH0622123Y2/en
Publication of JPH0272332U publication Critical patent/JPH0272332U/ja
Application granted granted Critical
Publication of JPH0622123Y2 publication Critical patent/JPH0622123Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

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

第1図は本考案によるガスタービンエンジンの
タービンの部分の断面図、第2図は第1図の線
―に沿つた断面図、第3図は圧力仕切り板を溶
接した例を示す図、第4図はガスタービンエンジ
ンの概略構成図である。 16…コンプレツサタービン、18…パワータ
ービン、32…内筒、34…外筒、36…ダクト
、40…圧力仕切り板、48…可変翼ノズル。
Fig. 1 is a cross-sectional view of the turbine part of a gas turbine engine according to the present invention, Fig. 2 is a cross-sectional view taken along the line - in Fig. 1, Fig. 3 is a view showing an example in which a pressure partition plate is welded, FIG. 4 is a schematic configuration diagram of a gas turbine engine. 16... Compressor turbine, 18... Power turbine, 32... Inner cylinder, 34... Outer cylinder, 36... Duct, 40... Pressure partition plate, 48... Variable vane nozzle.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] コンプレツサタービンとパワータービンとの間
に同心円状の内筒と外筒からなるダクトを設け、
該ダクト内に可変翼ノズルを配置したガスタービ
ンエンジンにおいて、前記内筒のパワータービン
側の端部に圧力仕切り板を設けたことを特徴とす
るガスタービンエンジンのダクト構造。
A duct consisting of a concentric inner cylinder and an outer cylinder is installed between the compressor turbine and the power turbine.
A duct structure for a gas turbine engine in which a variable blade nozzle is disposed within the duct, characterized in that a pressure partition plate is provided at an end of the inner cylinder on the power turbine side.
JP14963888U 1988-11-18 1988-11-18 Gas turbine engine duct structure Expired - Lifetime JPH0622123Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14963888U JPH0622123Y2 (en) 1988-11-18 1988-11-18 Gas turbine engine duct structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14963888U JPH0622123Y2 (en) 1988-11-18 1988-11-18 Gas turbine engine duct structure

Publications (2)

Publication Number Publication Date
JPH0272332U true JPH0272332U (en) 1990-06-01
JPH0622123Y2 JPH0622123Y2 (en) 1994-06-08

Family

ID=31422051

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14963888U Expired - Lifetime JPH0622123Y2 (en) 1988-11-18 1988-11-18 Gas turbine engine duct structure

Country Status (1)

Country Link
JP (1) JPH0622123Y2 (en)

Also Published As

Publication number Publication date
JPH0622123Y2 (en) 1994-06-08

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