发明名称 |
ターボ機械 |
摘要 |
The turbomachine has stationary component and rotating component e.g. rotor (12) between which clearance (g1) is formed. The clearance has two values in stationary and steady-state operations of machine, respectively. The clearance has a value which traverses a curve having extreme value on account of different time variation of rotational speed and thermal expansion of components during transient operating phase between both operations. A self-adjusting device (20) has non-linear compensation mechanism that reduces or compensates extreme value during transient operating phase. |
申请公布号 |
JP6025398(B2) |
申请公布日期 |
2016.11.16 |
申请号 |
JP20120118739 |
申请日期 |
2012.05.24 |
申请人 |
ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングGeneral Electric Technology GmbH |
发明人 |
ヤロスラフ レシェク シュヴェドヴィチ;アレクセイ モザロフ;シュテファン イアミシュ |
分类号 |
F01D11/02;F01D11/08;F01D25/00;F02C7/00;F02C7/28 |
主分类号 |
F01D11/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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