发明名称 IN-SPACE TEMPERATURE CONTROL SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide an in-space temperature control system for controlling temperature in a space by using a combustion facility that uses solid fuel. ! SOLUTION: An in-space temperature control system includes a space which is to be controlled, a combustion facility for indirectly heating at least a part of the air in the space, a ventilation path for circulating air, a solid fuel supply facility for supplying solid fuel to the combustion facility, and a control part equipped with a timer. "In a case where an in-space temperature falls below a predetermined middle temperature range upper limit" (condition 1, on and after), a control signal for operating an air-suction fan and an air-exhaust fan at a speed higher than a speed based on desire is transmitted and a timer is triggered, In a case where the in-space temperature exceeds the middle temperature range upper limit within a predetermined wanted period otherwise exhaust temperature exceeds a predetermined solid fuel feeding reference tempe
申请公布号 JP2015004487(A) 申请公布日期 2015.01.08
申请号 JP20130130582 申请日期 2013.06.21
申请人 KIHARA SEISAKUSHO 发明人 NAKAMURA HIROYUKI ; SASAKI SHINGO
分类号 F23N5/00;F23B60/00;F23N3/08;F23N5/02 主分类号 F23N5/00
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