CENTRIFUGAL COMPRESSOR

To provide a centrifugal compressor capable of achieving both reduction in moment of inertia of an impeller and a thrust load acting on the impeller, and suppression in reduction in a pressure ratio.SOLUTION: A centrifugal compressor 1 comprises a rotational shaft, an impeller, and a casing. The imp...

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Bibliographic Details
Main Authors NAKANE YOSHIYUKI, UMEYAMA AKIRA
Format Patent
LanguageEnglish
Japanese
Published 01.02.2022
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Summary:To provide a centrifugal compressor capable of achieving both reduction in moment of inertia of an impeller and a thrust load acting on the impeller, and suppression in reduction in a pressure ratio.SOLUTION: A centrifugal compressor 1 comprises a rotational shaft, an impeller, and a casing. The impeller has a hub 110 and a plurality of blades 120. The casing has an opposite surface 442 facing a back surface 118 of the hub 110, and a protrusion part 444 protruding from the opposite surface 442 toward the impeller. The hub 110 is formed with an accommodation space 110S for accommodating the protrusion part 444. The accommodation space 110S is provided with a through hole penetrating the hub 110 from the back surface 118 toward an outer peripheral surface 112. The through hole is opened so as to avoid the blade 120.SELECTED DRAWING: Figure 4 【課題】インペラの慣性モーメント及びインペラに作用するスラスト荷重の低減と、圧力比の低下の抑制と、の双方を達成可能な遠心圧縮機を提供すること。【解決手段】遠心圧縮機1は、回転軸と、インペラと、ケーシングと、を備える。インペラは、ハブ110と、複数のブレード120と、を有する。ケーシングは、ハブ110の背面118と対向する対向面442と、対向面442からインペラに向かって突出する突出部444と、を有する。ハブ110には、突出部444を収容する収容空間110Sが形成されている。収容空間110Sは、背面118から外周面112に向けてハブ110を貫通する貫通孔を備える。貫通孔は、ブレード120を避けて開口する。【選択図】図4
Bibliography:Application Number: JP20200123640