发明名称 MULTI-PULSE GAS GENERATOR AND OPERATION METHOD THEREOF
摘要 A multi-pulse gas generator includes a pressure vessel, an outer propellant arranged in the pressure vessel and which has a tubular shape, an intermediate propellant arranged inside the outer propellant and which has a tubular shape, an inner propellant arranged inside the intermediate propellant and which has a tubular shape, an internal structure arranged inside the inner propellant and fixed to the pressure vessel, a first barrier membrane arranged between the outer propellant and the intermediate propellant so as to isolate the outer propellant and the intermediate propellant from each other, and a second barrier membrane arranged between the intermediate propellant and the inner propellant so as to isolate the intermediate propellant and the inner propellant from each other. The outer propellant is supported on its outer surface by the pressure vessel. The inner propellant is supported on its inner surface by the internal structure.
申请公布号 US2015047316(A1) 申请公布日期 2015.02.19
申请号 US201414455037 申请日期 2014.08.08
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 MIHARA Chiyako;SUZUKI Tasuku;IEKI Katsunori
分类号 F02K9/28;F02K9/20;F02K9/12 主分类号 F02K9/28
代理机构 代理人
主权项 1. A multi-pulse gas generator comprising: a pressure vessel; an outer propellant disposed in the pressure vessel and having a tubular shape; an intermediate propellant disposed inside the outer propellant and having a tubular shape; an inner propellant disposed inside the intermediate propellant and having a tubular shape; an internal structure disposed inside the inner propellant and fixed to the pressure vessel; a first barrier membrane disposed between the outer propellant and the intermediate propellant so as to isolate the outer propellant and the intermediate propellant from each other; and a second barrier membrane disposed between the intermediate propellant and the inner propellant so as to isolate the intermediate propellant and the inner propellant from each other, wherein said outer propellant is supported on its outer surface by the pressure vessel, and wherein said inner propellant is supported on its inner surface by the internal structure.
地址 Tokyo JP