中科微点-全球专利检索

  1. Login
  2. Sign Up
Invention Grant
US08770519B2 Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft 有权
飞机或航天器的结构部件和飞机或航天器的机身部件装置

Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft
Abstract:
In the case of a structural component of an aircraft or spacecraft comprising a fuselage portion connection region for connecting to an associated fuselage portion and having a thermal expansion coefficient which is approximately matched to the associated fuselage portion; an inner connection region for connecting to an associated installation element and having a thermal expansion coefficient which is approximately matched to the associated installation element; and a separation region for connecting the fuselage portion connection region and the inner connection region, at least one of the regions has a high heat conduction resistance.
Abstract(Chinese):

在飞行器或航天器的结构部件的情况下，其包括用于连接到相关联的机身部分并且具有与相关联的机身部分近似匹配的热膨胀系数的机身部分连接区域; 用于连接到相关联的安装元件并且具有与相关联的安装元件近似匹配的热膨胀系数的内部连接区域; 以及用于连接机身部连接区域和内部连接区域的分离区域，至少一个区域具有高的导热性。

Public/Granted literature
Information query
Espacenet
Patent Agency Ranking
0/0