发明名称 |
Method of making a flexprop |
摘要 |
A grenade device for use with and for ejection from an artillery shell is provided. The device includes a stabilizing propeller and a grenade body. The propeller has two opposite blades disposed on opposite sides of a rotation axis. Each blade has an upper tilted portion and a lower substantially flat portion and a connecting return bend tip portion. Each such portion has a leading edge and a trailing edge. Each upper tilted portion has a transverse angle of attack. The upper tilted portions have a common longitudinal upper projected axis. The lower flat portions also have a common longitudinal lower projected axis. The common longitudinal upper projected axis and the common longitudinal lower projected axis form a projected displacement angle therebetween. The propeller is made from a flexible metal or fabric ribbon. The blades are folded in a nested arrangement before descent. During descent, the blades unfold to their overall aerodynamic shape. The propeller has a windmill type of rotation during descent. The grenade body may have an alternator as part of an electronic fuze, which is connected to a shaft, that is connected to the propeller coaxially therewith along the rotation axis for energizing the alternator.
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申请公布号 |
US5111576(A) |
申请公布日期 |
1992.05.12 |
申请号 |
US19900520300 |
申请日期 |
1990.05.07 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY |
发明人 |
KUHNLE, WILLIAM G.;MURNANE, II, JAMES F. |
分类号 |
F42B10/58;F42C15/295 |
主分类号 |
F42B10/58 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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