发明授权
- 专利标题: Method for manufacturing outlet nozzles for rocket engines
- 专利标题(中): 制造火箭发动机出口喷嘴的方法
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申请号: US10872667申请日: 2004-06-21
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公开(公告)号: US06945032B2公开(公告)日: 2005-09-20
- 发明人: Jan Lundgren
- 申请人: Jan Lundgren
- 申请人地址: SE
- 专利权人: Volvo Aero Corporation
- 当前专利权人: Volvo Aero Corporation
- 当前专利权人地址: SE
- 代理机构: Lerner, David, Littenberg, Krumholz & Mentlik, LLP
- 优先权: SE9803387 19981002
- 主分类号: B23K26/00
- IPC分类号: B23K26/00 ; B23K26/20 ; B23K26/24 ; B23K26/28 ; F02K9/64 ; F02K9/97 ; F02K9/72
摘要:
A wall structure capable of withstanding high thermal load, including a wall structure with an inner wall, an outer wall positioned about the inner wall, and distancing elements located between the inner and outer walls. The distancing elements are joined to at least one of the inner and outer walls by means of laser welding and thereby establishing a plurality of cooling ducts between the inner and outer walls and a weld joint formed by the laser welding and having a cross-section taken through the wall structure that is substantially T-shaped and which displays a rounded shape towards an inside one of the plurality of cooling ducts.
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