JPS6239200U

JPS6239200U -

Info

Publication number: JPS6239200U
Application number: JP13211785U
Authority: JP
Priority date: 1985-08-29
Filing date: 1985-08-29
Publication date: 1987-03-09

Description

[Brief explanation of the drawing]

第１図は、この考案の一実施例を示す図、第２
図は、この考案によるピンが操舵翼から抜ける仕
組みを示す図、第３図は操舵翼が吹き流し翼とな
つている誘導飛翔体の構造の一例を示す図、第４
図は吹き流し翼となつている操舵翼が翼の回転軸
まわりに回転する状態を示す図、第５図は吹き流
し翼状態の操舵翼が母機にあたる状態を示す図で
あり、図中、１は誘導飛翔体の機体、２は操舵翼
、３はピン、４はスプリング、５はロツクピン、
６はワイヤ、７は操舵翼の回転軸、８は操舵駆動
系、９は母機、１０はパイロンである。なお、図
中同一符号は同一又は相当部分を示す。 Figure 1 is a diagram showing an embodiment of this invention;
The figure shows the mechanism by which the pin comes out of the steering blade according to this invention, Figure 3 shows an example of the structure of a guided flying object in which the steering blade is a windsock blade, and Figure 4
The figure shows the state in which the steering blade, which is a windsock blade, rotates around the axis of rotation of the blade, and Figure 5 shows the state in which the steering blade, which is a windsock blade, is in contact with the mother aircraft. The body of the flying object, 2 is the steering wing, 3 is the pin, 4 is the spring, 5 is the lock pin,
6 is a wire, 7 is a rotating shaft of a steering blade, 8 is a steering drive system, 9 is a mother plane, and 10 is a pylon. Note that the same reference numerals in the figures indicate the same or equivalent parts.

Claims

[Scope of utility model registration request]

In a guided flying object that is launched or dropped from an aircraft with the steering wing acting as a windswept wing, the steering wing has a pin hole on the bottom surface, and when the guided flying object is mounted on a mother aircraft, the pin hole of the steering wing is installed. When the inserted guided flying object is launched or dropped, the pin is pulled out of the pin hole of the steering wing and retracted into the aircraft body, and when the guided flying object is mounted on the mother aircraft, the pin is inserted into the pin hole of the steering wing. A guided flying object characterized by comprising a lock pin that is held and pulled out from the pin when launching or dropping, and configured so that the steering wing does not move when mounted on a mother aircraft by the pin and the lock pin.