发明授权
- 专利标题: Combustion chamber structure for a turbojet engine
- 专利标题(中): 涡轮喷气发动机的燃烧室结构
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申请号: US56884申请日: 1987-06-03
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公开(公告)号: US4805397A公开(公告)日: 1989-02-21
- 发明人: Gerard Y. G. Barbier , Gerard J. P. B. Laboure , Michel A. A. Desaulty , Francois Duchene , Pascal M. Truvillot
- 申请人: Gerard Y. G. Barbier , Gerard J. P. B. Laboure , Michel A. A. Desaulty , Francois Duchene , Pascal M. Truvillot
- 申请人地址: FRX Paris
- 专利权人: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- 当前专利权人: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- 当前专利权人地址: FRX Paris
- 优先权: FRX8608015 19860604
- 主分类号: F23R3/00
- IPC分类号: F23R3/00 ; F23R3/04 ; F02C7/20 ; F02C1/00
摘要:
A combustion chamber for a turbojet engine is disclosed which utilizes double walled construction. Hot walls are attached to adjacent cold walls solely by an orifice member which defines an orifice to supply primary of dilution air to the combustion chamber. The attachment allows relative radial movement of the hot walls with respect to the cold walls so as to accommodate the thermal expansion and contraction of the hot walls. The sleeves forming the walls also cooperate so as to provide an internal cooling film on the interior surface of the hot walls. Convection cooling may also be utilized between the walls to prevent structural damage due to high temperatures.
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