| 发明名称 |
Aircraft heater |
| 摘要 |
An aircraft heating system taps into a bleed air flowpath between a turbine engine and an external bleed air port on the aircraft. A system may be installed as a retrofit for heating the cabin of an aircraft already having a heating system for heating the cockpit.
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| 申请公布号 |
US6848652(B2) |
申请公布日期 |
2005.02.01 |
| 申请号 |
US20030376004 |
申请日期 |
2003.02.28 |
| 申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
PALIN HAROLD J.;BACKERT ROGER V.;JAMES CURTIS S.;SCHULTZ ANTHONY |
| 分类号 |
B64D13/08;(IPC1-7):B64D13/08 |
主分类号 |
B64D13/08 |
| 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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