POWERED AIRBAG FOR AEROPLANE'S VERTICAL FALL DURING AN ACCIDENT

    公开(公告)号:US20180009541A1

    公开(公告)日:2018-01-11

    申请号:US15513566

    申请日:2015-11-20

    申请人: Ngoc Quy Pham

    发明人: Ngoc Quy Pham

    IPC分类号: B64D25/00 B64C1/14

    摘要: The invention is about a powered airbag for planes in case of uncontrollable falling which makes the plane fall vertically with the head up. The invention includes the bonnet cover of the head 1, the hinges of the bonnet cover 17, the head cover of the plane 12, the structural frame of the head the plane 13, the container of gas-creating material 8, Valve to activate the airbag 9. There is a difference that the structural frame of the head of the plane 13 has a powered airbag 11, the flexible soft tube 10 which connects the powered airbag 11 to the frame of the head of the plane 13

    The engine operated by the buoyancy of water

    公开(公告)号:US20170306920A1

    公开(公告)日:2017-10-26

    申请号:US15509500

    申请日:2015-11-20

    IPC分类号: F03B17/04

    摘要: The invention relates to engine operated by the buoyancy of water, this engine is made up of water tank(16), the first device cluster (100) includes a shaft (1) and two gears (2a, 2b), at the teeth (24) there is a one-way air-supply valve (23), the second device cluster (200) includes a shaft (3) and two gears (4a, 4b). There is a difference that the third device clusters (300) includes two flanges (9a , 9b), a rectangular box (10) functioned to change the volume while coordinating activities with the structure of shaped rails (17) and (18), multiple third device clusters (300) are connected together by latches (15) forming a closed circle, the flanges (9a, 9b) of the closed circle are inserted fit the teeth (24) of the gears (2a, 2b) of the first device cluster (100) and mounted to fit the teeth (24) of the gears (4a, 4b) of the second device cluster (200).