首页> 外国专利> CONTROLLABLE ASSEMBLY FOR ACCURACY LANDING PARACHUTING AND ACCURACY LANDING PARACHUTING CONTROL METHOD

CONTROLLABLE ASSEMBLY FOR ACCURACY LANDING PARACHUTING AND ACCURACY LANDING PARACHUTING CONTROL METHOD

机译:精确着陆游标的可控制组件及精确着陆游标的控制方法

摘要

The invention relates to a controllable air transport assembly with a wing-type parachute, meant to be used in particular for the quick supply of troops with packaged military equipment or of zones difficlt to access in case of calamities, by parachuting from a transporting aircraft. According to the invention, the system comprises some wing-type parachutes (1 and 2), a stablilizing parachute and a main parachute, respectively, the control of the main parachute (2) being ensured by a control and guiding system (3), enabling the main parachute (2) to be hand controlled from the ground, by means of a transmitter (12) or automatically controlled, by using the data transmitted by a GPS receiver (5) which receives the data from the positioning satellites and transmits them serially to a microcontroller (7) which also receives radio signals transmitted after the reception thereof by a radio receiver (6), from a remote guiding transmitter (12), all data being processed by a computer program, loaded on the computer and converted into commands transmitted to an actuation unit (8) which transmits signals for the actuation of some servomechanisms (10 and 11) driving some chords. The claimed platform comprises two plates connected to each other, between which there is mounted a shock absorber with bellows provided with some calibrated air-discharge orifices, the platform of the shock absorber with container (4) being attached to the casing of the control and guiding system (3) by means of some launching devices.
机译:具有机翼降落伞的可控制的航空运输组件技术领域本发明涉及一种具有机翼降落伞的可控制的航空运输组件,该组件尤其用于通过运输机的跳伞来快速向部队提供打包的军事装备或在发生灾难时难以进入的区域。根据本发明,该系统包括一些机翼降落伞(1和2),稳定降落伞和主降落伞,通过控制和引导系统(3)来确保对主降落伞(2)的控制,使主降落伞(2)可以通过发射机(12)从地面手动控制,或者通过使用GPS接收机(5)传输的数据自动控制,该GPS接收机从定位卫星接收数据并进行传输串行连接到微控制器(7),该微控制器(7)在从无线电接收器(6)接收到无线电信号之后,还从远程引导发射机(12)接收无线电信号,所有数据都由计算机程序处理,加载到计算机上并转换为命令被发送到致动单元(8),该致动单元(8)发送用于致动驱动某些和弦的某些伺服机构(10和11)的信号。所要求保护的平台包括彼此连接的两个板,在两个板之间安装有具有波纹管的减震器,该波纹管具有一些校准的空气排放孔,具有容器(4)的减震器的平台附接到控制装置的壳体上。借助一些发射装置引导系统(3)。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号