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    • 1. 发明授权
    • Heat exchanger for aircraft exhaust
    • 飞机排气换热器
    • US07857040B1
    • 2010-12-28
    • US11899202
    • 2007-09-05
    • Thomas J. Strohmayer
    • Thomas J. Strohmayer
    • F28D7/02F28F9/22
    • F28F9/22B64D33/04F28D1/047F28D7/005F28D21/0003F28F9/001F28F2275/06
    • A heat exchanger for use with exhaust pipes. A shroud inlet communicates with a rear chamber, which communicates with a front chamber via a center plate vent. The front chamber communicates with a shroud outlet. Ambient air entering the rear chamber is routed around at least one J-pipe in the rear chamber, and around a collector in the front chamber, thus being twice heated prior to exiting the heat exchanger through the shroud outlet. The double heating provided by this design increases the efficiency of the heat exchanger. The collector is attached to the center plate by means of a full-penetration fillet weld, and the J-pipes are attached to the center plate, a front plate, and a pipe assembly baffle by stitch welding external to the J-pipes, thus strengthening the integrity of the hermetic seal between exhaust gasses and ambient air passing through the heat exchanger.
    • 用于排气管的换热器。 护罩入口与后室连通,后室通过中心板通气口与前室连通。 前室与护罩出口连通。 进入后室的环境空气绕在后室中的至少一个J型管上,并且围绕前室中的收集器布置,因此在通过护罩出口离开热交换器之前被两次加热。 由该设计提供的双重加热增加了热交换器的效率。 收集器通过全角焊缝焊接在中心板上,J型管通过在J型管外面进行缝合焊接而连接到中心板,前板和管道组件挡板上,因此 加强废气和通过热交换器的环境空气之间的气密密封的完整性。