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
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