利索-全球专利检索

  1. Login
  2. Sign Up
Invention Application
US20120039710A1 INTERMEDIATE CASING OF AIRCRAFT TURBOMACHINE INCLUDING STRUCTURAL CONNECTING ARMS WHICH PERFORM SEPARATE MECHANICAL AND AERODYNAMIC FUNCTIONS 审中-公开
飞机涡轮机的中间模式，包括执行单独机械和空气动力功能的结构连接臂

  • Patent Title: INTERMEDIATE CASING OF AIRCRAFT TURBOMACHINE INCLUDING STRUCTURAL CONNECTING ARMS WHICH PERFORM SEPARATE MECHANICAL AND AERODYNAMIC FUNCTIONS
  • Patent Title (中): 飞机涡轮机的中间模式，包括执行单独机械和空气动力功能的结构连接臂
  • Application No.: US13265056
    Application Date: 2010-04-21
  • Publication No.: US20120039710A1
    Publication Date: 2012-02-16
  • Inventor: Frederic Marius Mathieu , Thierry Georges, Paul Papin
  • Applicant: Frederic Marius Mathieu , Thierry Georges, Paul Papin
  • Applicant Address: FR Paris
  • Assignee: Snecma
  • Current Assignee: Snecma
  • Current Assignee Address: FR Paris
  • Priority: FR0952626 20090422
  • International Application: PCT/EP2010/055262 WO 20100421
  • Main IPC: F01D25/28
  • IPC: F01D25/28 ;  B23P15/00
INTERMEDIATE CASING OF AIRCRAFT TURBOMACHINE INCLUDING STRUCTURAL CONNECTING ARMS WHICH PERFORM SEPARATE MECHANICAL AND AERODYNAMIC FUNCTIONS
Abstract:
A structural connecting arm for an intermediate casing of an aircraft turbomachine with a ducted fan, wherein the arm is configured to connect a hub and an outer ferrule of the casing, and including an aerodynamic outer surface manufactured such that the arm also forms an outlet guide vane. Multiple metal ties extend in the longitudinal direction of the arm, together with a shell made from composite material surrounding the ties and forming the aerodynamic outer surface.
Abstract(Chinese):

一种用于具有管道风扇的飞行器涡轮机的中间壳体的结构连接臂，其中所述臂被构造成连接所述壳体的轮毂和外部套圈，并且包括制造为使得所述臂还形成出口导向件的空气动力学外表面 叶片。 多个金属结合件在臂的纵向方向上延伸，以及由围绕连接件的复合材料制成的壳体并形成空气动力学外表面。

Information query
Global Dossier Espacenet
Patent Agency Ranking
0/0