Invention Grant
US08376692B2 Turbo compressor in an axial type of construction 有权
涡轮压缩机采用轴向式结构

  • Patent Title: Turbo compressor in an axial type of construction
  • Patent Title (中): 涡轮压缩机采用轴向式结构
  • Application No.: US12301901
    Application Date: 2007-05-18
  • Publication No.: US08376692B2
    Publication Date: 2013-02-19
  • Inventor: Frank Stiehler
  • Applicant: Frank Stiehler
  • Applicant Address: DE Munich
  • Assignee: MTU Aero Engines GmbH
  • Current Assignee: MTU Aero Engines GmbH
  • Current Assignee Address: DE Munich
  • Agency: Crowell & Moring LLP
  • Priority: DE102006024085 20060523
  • International Application: PCT/DE2007/000916 WO 20070518
  • International Announcement: WO2007/134585 WO 20071129
  • Main IPC: F01D17/16
  • IPC: F01D17/16
Turbo compressor in an axial type of construction
Abstract:
A turbo compressor in an axial type of construction is disclosed. The turbo compressor has a bladed stator and a bladed rotor, and has a longitudinally split compressor casing and a guide blade ring with adjustable guide blades. The guide blades are pivotably mounted about radial axes radially within their aerofoil on an inner ring belonging to the stator. The inner ring is split, i.e., segmented, at at least two points of its circumference. Furthermore, the inner ring has for each guide blade at least one bearing bush which can be inserted radially into an opening from inside.
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