JPH01152004U - - Google Patents

Info

Publication number
JPH01152004U
JPH01152004U JP4883888U JP4883888U JPH01152004U JP H01152004 U JPH01152004 U JP H01152004U JP 4883888 U JP4883888 U JP 4883888U JP 4883888 U JP4883888 U JP 4883888U JP H01152004 U JPH01152004 U JP H01152004U
Authority
JP
Japan
Prior art keywords
shroud
turbine
bypass hole
blades
blade
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
JP4883888U
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 JP4883888U priority Critical patent/JPH01152004U/ja
Publication of JPH01152004U publication Critical patent/JPH01152004U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案によるパイパス穴付シユラウド
を有するタービンの一例の構造組成を示し、aは
その外観図、bはその平面図、cはその側面図で
ある。第2図は本考案によるタービン翼間の翼通
路内の圧力分布とバイパス穴の穿設位置を示す配
置図、第3図はパイパス穴をバイパスする二次流
れの流れを示す模式図、第4図は従来のシユラウ
ドを有するタービンを示す外観図、第5図はその
平面図、第6図はその二次流れの流れを示す模式
図である。 1……シユラウド、2,2′……各タービン翼
、3……作動流体、3a……二次流れ、4……翼
通路、6……翼出口部、8……パイパス穴。
FIG. 1 shows the structural composition of an example of a turbine having a shroud with bypass holes according to the present invention, in which a is an external view, b is a plan view, and c is a side view. Fig. 2 is a layout diagram showing the pressure distribution in the blade passage between turbine blades and the drilling position of the bypass hole according to the present invention, Fig. 3 is a schematic diagram showing the secondary flow bypassing the bypass hole, and Fig. 4 is a schematic diagram showing the flow of the secondary flow bypassing the bypass hole. The figure is an external view showing a conventional turbine having a shroud, FIG. 5 is a plan view thereof, and FIG. 6 is a schematic diagram showing the flow of the secondary flow. 1... Shroud, 2, 2'... Each turbine blade, 3... Working fluid, 3a... Secondary flow, 4... Blade passage, 6... Blade outlet, 8... Bypass hole.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 隣接し合うタービン翼の腹面と背面との圧力差
によりその翼間に発生する作動流体の二次流れを
バイパスするシユラウドを有するタービンであつ
て、タービン翼を固定するシユラウドに翼通路内
及び翼出口部を連絡するバイパス穴を少なくとも
1つ以上穿設してなるパイパス穴付シユラウドを
有するタービン。
A turbine that has a shroud that bypasses the secondary flow of working fluid generated between adjacent turbine blades due to the pressure difference between the ventral surface and the back surface of the blades, and the shroud that fixes the turbine blades has a section inside the blade passage and a blade outlet. A turbine having a shroud with a bypass hole, which is formed by drilling at least one bypass hole connecting the parts.
JP4883888U 1988-04-13 1988-04-13 Pending JPH01152004U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4883888U JPH01152004U (en) 1988-04-13 1988-04-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4883888U JPH01152004U (en) 1988-04-13 1988-04-13

Publications (1)

Publication Number Publication Date
JPH01152004U true JPH01152004U (en) 1989-10-19

Family

ID=31274971

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4883888U Pending JPH01152004U (en) 1988-04-13 1988-04-13

Country Status (1)

Country Link
JP (1) JPH01152004U (en)

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