发明名称 |
Secondary air feed control for gas turbine burner flame tube - has jacketed tube with spherical surface in region with air ports with throttle ring |
摘要 |
The secondary air feed control consists of a throttle ring to surround a section of the flame tube coaxially by a casing tube, and a deflector which moves the ring to control the ports (9) round the casing tube. In the perforated section (8), the casing tube (5) has a spherical surface (7) on which the throttle ring (13) is pivoted via two journals (15) in the centre circumference of the tube section. The throttle ring has a spherical inside surface (14) to close the air ports. USE/ADVANTAGE - For gas turbine burner control, with simple design for preventing frictional motion of the throttle ring.
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申请公布号 |
DE4034711(C1) |
申请公布日期 |
1992.02.27 |
申请号 |
DE19904034711 |
申请日期 |
1990.11.01 |
申请人 |
DAIMLER-BENZ AKTIENGESELLSCHAFT, 7000 STUTTGART, DE |
发明人 |
MAYER, CHRISTIAN, DIPL.-ING. (FH), 7257 DITZINGEN, DE |
分类号 |
F23R3/26 |
主分类号 |
F23R3/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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