摘要：【中文】本发明提出一种基于屉式结构多种信号采编记录器，包括：存储模块、直流电压变换层、电源层、主控层、电压采集层、电荷采集层、温惯采集层、上盖和紧固件，紧固件将存储模块、直流电压变换层、电源层、主控层、电压采集层、电荷采集层、温惯采集层和上盖之间的相对位置固定并增加结构整体强度。本发明有益效果：将数据存储、直流电压变换、主控、电压采集、电荷采集和温惯采集单独分层，通过合理排布顺序，不仅可以有效减少电气干扰，提升数据准确性，而且可以根据实际需要停用部分分层，降低功耗，提升设备适用范围，同时屉式结构便于安装、拆卸和维护；通过上盖和紧固件，可以将各层限位紧固，更加安全可靠。 【EN】The invention provides a drawer-type structure-based multi-signal acquisition and coding recorder, which comprises: the storage module, the direct-current voltage conversion layer, the power supply layer, the main control layer, the voltage acquisition layer, the charge acquisition layer, the temperature inertia acquisition layer, the upper cover and the fastener fix the relative positions among the storage module, the direct-current voltage conversion layer, the power supply layer, the main control layer, the voltage acquisition layer, the charge acquisition layer, the temperature inertia acquisition layer and the upper cover and increase the overall strength of the structure. The invention has the beneficial effects that: the data storage, the direct-current voltage conversion, the master control, the voltage acquisition, the charge acquisition and the thermal inertia acquisition are independently layered, through reasonable arrangement sequence, not only can the electrical interference be effectively reduced and the data accuracy be improved, but also partial layering can be stopped according to actual needs, the power consumption is reduced, the application range of the equipment is improved, and meanwhile, the drawer type structure is convenient to install, disassemble and maintain; through upper cover and fastener, can be with the spacing fastening of each layer, safe and reliable more.

摘要：【中文】本发明为一种深空探测撞击过载测试及数据无线传输测量装置，属于深空探测技术领域；本发明包括两端为喇叭口设计的外壳体，外壳体的前端凹面内安装有第二过载传感器；外壳体内套装有内壳体及天线杯，内壳体内安装有第一过载传感器、采集控制模块、电池和天线模块；天线杯内安装有天线。电池与采集控制模块连接，采集控制模块与天线模块连接，天线模块与天线连接，第一过载传感器及第二过载传感器均与采集控制模块连接。本发明装置设计科学，结构简单，设备集成度高，其内外壳体多层设计可广泛应用到深空探测和高过载记录装置中，为后续深空探测探测器着落过载的测量打下坚实的基础。 【EN】The invention relates to a deep space exploration impact overload test and data wireless transmission measuring device, belonging to the technical field of deep space exploration; the invention comprises an outer shell with two ends designed as bell mouths, wherein a second overload sensor is arranged in a concave surface at the front end of the outer shell; an inner shell and an antenna cup are sleeved in the outer shell, and a first overload sensor, an acquisition control module, a battery and an antenna module are arranged in the inner shell; an antenna is arranged in the antenna cup. The battery is connected with the acquisition control module, the acquisition control module is connected with the antenna module, the antenna module is connected with the antenna, and the first overload sensor and the second overload sensor are both connected with the acquisition control module. The device has scientific design, simple structure and high equipment integration level, and the multilayer design of the inner shell and the outer shell can be widely applied to deep space detection and high overload recording devices to lay a solid foundation for the subsequent measurement of landing overload of the deep space detection detector.