JPS6324301U - - Google Patents

Info

Publication number
JPS6324301U
JPS6324301U JP11827886U JP11827886U JPS6324301U JP S6324301 U JPS6324301 U JP S6324301U JP 11827886 U JP11827886 U JP 11827886U JP 11827886 U JP11827886 U JP 11827886U JP S6324301 U JPS6324301 U JP S6324301U
Authority
JP
Japan
Prior art keywords
parts
shroud
holes
blades
adjacent blades
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
JP11827886U
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 JP11827886U priority Critical patent/JPS6324301U/ja
Publication of JPS6324301U publication Critical patent/JPS6324301U/ja
Pending legal-status Critical Current

Links

Description

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

第1図から第5図は本考案に係わる実施例を示
す図で、第1図は本考案に係る一実施例を示す軸
流形翼の側断面図である。第2図、第3図は第1
図に図示のシユラウド部分の翼の挿入植込み方法
を示す水平断面図である。第4図、第5図は柱状
ピンの外形図である。第6図から第7図は従来例
を示す図で、第6図はシユラウド側面の摩擦ダン
ピングによる従来の方法を示す斜視図、第7図は
ダンピングワイヤによる従来方法を示す斜視図で
ある。 10,20…翼本体、11,21…シユラウド
部、12,22…ラツシングワイヤ部、13,2
3…翼根部、14,15,24,25…シユラウ
ド部の有限長の孔(盲孔)、16,17,26,
27…ラツシングワイヤ部の有限長の孔(盲孔)
、30,31…スプリング、40,41,42,
43…柱状ピン。
1 to 5 are diagrams showing an embodiment of the present invention, and FIG. 1 is a side sectional view of an axial airfoil showing an embodiment of the present invention. Figures 2 and 3 are
FIG. 4 is a horizontal cross-sectional view showing a method of inserting and implanting a wing in the shroud portion shown in the figure. FIGS. 4 and 5 are external views of the columnar pin. 6 to 7 are diagrams showing conventional examples. FIG. 6 is a perspective view showing a conventional method using friction damping on the side surface of a shroud, and FIG. 7 is a perspective view showing a conventional method using damping wires. 10, 20...Blade body, 11,21...Shroud part, 12,22...Lashing wire part, 13,2
3...Blade root part, 14,15,24,25...Limited length hole (blind hole) in shroud part, 16,17,26,
27...Limited length hole (blind hole) in the lashing wire part
, 30, 31... Spring, 40, 41, 42,
43...Pillar pin.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 相隣り合う翼のシユラウド部またはラツシング
ワイヤ部の対向面の両側にそれぞれ有限長の孔を
穿設すると共に、同一対の孔にスプリングによつ
て押圧される柱状ピンを挿入して相隣り合う上記
翼同志を上記柱状ピンによつて連結させたことを
特徴とする回転翼の制振構造。
Holes of finite length are drilled on both sides of the opposing surfaces of the shroud parts or lashing wire parts of adjacent blades, and columnar pins pressed by springs are inserted into the same pair of holes so that the shroud parts or latching wire parts of adjacent blades are connected. A vibration damping structure for a rotor blade, characterized in that the blades are connected to each other by the columnar pin.
JP11827886U 1986-07-31 1986-07-31 Pending JPS6324301U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11827886U JPS6324301U (en) 1986-07-31 1986-07-31

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11827886U JPS6324301U (en) 1986-07-31 1986-07-31

Publications (1)

Publication Number Publication Date
JPS6324301U true JPS6324301U (en) 1988-02-17

Family

ID=31004582

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11827886U Pending JPS6324301U (en) 1986-07-31 1986-07-31

Country Status (1)

Country Link
JP (1) JPS6324301U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH045402A (en) * 1990-04-20 1992-01-09 Mitsubishi Heavy Ind Ltd Integral shroud vane
JP2014114734A (en) * 2012-12-07 2014-06-26 Mitsubishi Heavy Ind Ltd Turbine blade and turbine
JP2015148284A (en) * 2014-02-06 2015-08-20 三菱日立パワーシステムズ株式会社 Liquid damper and rotary machine blade including the same

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH045402A (en) * 1990-04-20 1992-01-09 Mitsubishi Heavy Ind Ltd Integral shroud vane
JP2014114734A (en) * 2012-12-07 2014-06-26 Mitsubishi Heavy Ind Ltd Turbine blade and turbine
JP2015148284A (en) * 2014-02-06 2015-08-20 三菱日立パワーシステムズ株式会社 Liquid damper and rotary machine blade including the same

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