发明名称 Thrust augmenter ejector combustion device
摘要 A combustion device for use with pressurized and zero pressure hot air balloons or other hot air appliances, which comprises in general, a coanda-type inlet nozzle, a diffuser, a flame-arrestor screen, and a fuel preheater means for supplying required fuel vapor at a desired pressure to the inlet nozzle. The combustion device may be used with any suitable fuel, but it is primarily applicable to propane. The combustion device is a fuel pressure driven-nozzle-mixer-diffuser-arrestor screen burner combustion device which generates a stream of heated air for the transfer of thermal energy to a load.
申请公布号 US4332547(A) 申请公布日期 1982.06.01
申请号 US19790080985 申请日期 1979.10.01
申请人 MACDONALD, JR., JAMES D. 发明人 MACDONALD, JR., JAMES D.
分类号 F23D11/40;F23D11/44;(IPC1-7):F23D11/44 主分类号 F23D11/40
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