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序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
101	Jet gas deflector angle altering device for missile	JP2236691	1991-02-15	JPH04260796A	1992-09-16	INOUE MASAO; WATANABE OSAMU
PURPOSE: To effectively feed jet gas rearward by varying a set angle of a deflector having an area necessary to deflect a jet gas. CONSTITUTION: A variable deflector 11 is provided on a section for directly receiving a jet gas of a jet gas deflector 2 provided in a jet gas deflecting mechanism 1, and a set angle of the deflector having an area necessary to deflect the gas is variably provided. COPYRIGHT: (C)1992,JPO&Japio
102	JPH0482587U -	JP12290890	1990-11-22	JPH0482587U	1992-07-17

103	JPS5514999B2 -	JP13446873	1973-12-03	JPS5514999B2	1980-04-19

104	Missile launching machine	JP2001241658	2001-08-09	JP2003056997A	2003-02-26	OUCHI MINORU
PROBLEM TO BE SOLVED: To obtain a missile launching machine in which a missile can be launched at a low launching angle and can be searched or observed from a high position ensuring an excellent visibility. SOLUTION: In a missile launching machine where a missile case 16 is fixed to a machine base 15 such that elevation/lowering and launching angle can be adjusted freely and a sighting unit 17 is fixed to the missile case 16 such that elevation/lowering and the angle can be adjusted freely, a missile can be launched while locating the missile case 16 at an upper position of a crew seat 13 when it is mounted on a vehicle 10 and thereby a missile can be launched at a low launching angle. Furthermore, the missile can be searched or visually confirmed from a high position ensuring an excellent visibility because the sighting unit 17 can be moved upward with respect to the missile case 16.
105	Launching device of missile	JP1541699	1999-01-25	JP2000213894A	2000-08-02	NISHIKIDO KOJI
PROBLEM TO BE SOLVED: To generate a chip-off moment in a target direction in a missile and to enable the missile to fly in the target direction by applying a load to the lower portion of the missile from the target direction by an initial path angle- changing device. SOLUTION: When a missile 5 is to be launched, first a launching direction is indicated by a launching control device 6 and a missile body 5 slides vertically on a rail 4 in a canister 3. When the missile body 5 departs from the rail 4, the departure is detected by a laser beam L for detecting the departure of a departure-detecting device 10, and an arm-driving device 13 in a launching direction is operated by the departure detection, thus applying the load of a hammer 11 to the lower portion of the missile body 5 and hence generating a chip-off moment in a target direction in the missile body 5 and changing the initial path angle of the missile body 5. By executing a series of operations, the missile body 5 is allowed to fly in the target direction being indicated by the launching control device 6.
106	Missile launcher	JP28780091	1991-11-01	JPH05126498A	1993-05-21	KODAMA MASARU; SUGIYAMA KATSUMASA
PURPOSE: To prevent the blow-up of sand, small stones and the like and reduce noise by a method wherein a jet gas deflecting board, consisting of a curved surface projected toward the downstream side of the flow of jet gas, is provided, in the title device launching a missile from a vehicle or the like. CONSTITUTION: A flow deflecting board 15, deflecting the flow of jet gas 2 of a missile 3, is attached to the rear end of a vehicle 7 through a hinge 5 so as to be rotatable about the hinge 5. The flow deflecting board 15 is provided with a curved surface formed so as to be projected toward the downstream side of the flow of the jet gas 2 of the missiles 3, loaded in two rows of fore- and-rear direction. According to this constitution, the jet gas 2 forms substantially horizontal flow 16 and will never be collided against the surface of the ground 10 whereby sand, small stones and the like will never be blown up. On the other hand, a sound absorbing material 29, consisting of glass fibers or the like, is bonded on the side of the flow deflecting board 15, against which the jet gas 2 is collided, whereby noise, generated by the collision of the jet gas 2 and the like, can be reduced. COPYRIGHT: (C)1993,JPO&Japio
107	Missile launcher	JP24332691	1991-09-24	JPH0579796A	1993-03-30	MURAOKA NOBUYUKI
PURPOSE:To stably fix a launcher firing base by providing a firing base supporter having a coupler including pins provided at the firing base, a pair of legs rotatably mounted at the ends of the pins of the coupler, and a foundation fixing bracket mounted by other pins at the other ends of the legs. CONSTITUTION:The missile launcher comprises a coupler 1a having pins so provided at a launcher firing base 9 as to perpendicularly cross a firing base propulsion force henerated by the deflection of a jet stream in the case of launching a missile, a pair of legs 1b rotatably mounted at the ends of the pins of the coupler, and a foundation fixing bracket 1c mounted by other pins at the other ends of the legs. A firing base supporter is mounted in response to a size between the firing base and a foundation after the firing base 9 is horizontally set by four jacks 2. Thus, fire base propulsion force generated at the time of launching the missile is supported by the four jacks to prevent the firing base from moving forward. Since the legs are obliquely provided, it can resist strongly against the propulsion force even by a small-sized apparatus.
108	Missile launcher system	JP24332591	1991-09-24	JPH0579795A	1993-03-30	MURAOKA NOBUYUKI; KOBAYASHI SUMIYUKI
PURPOSE:To perform launching preparation of a plurality of missiles by composing of a semi-trailer having a launching control function, a vehicle for a launcher, and a vehicle for supplementing a missile and placing a plurality of missiles and a launcher firing base function to be trailed by a vehicle. CONSTITUTION:A semi-trailer 9 placing missiles 3 is towed to be moved by a vehicle 6 for launching and having a missile launching controller 8. The vehicle 6 is separated from the semi-trailer 9, and a cable and a hydraulic hose 12 are connected. The vehicle 6 has a launcher 7, the controller 8 and a hydraulic pump 15, and has a launching control function. The trailer 9 has a launcher firing base function. The trailer 9 is fixed by an outrigger 13 by the pump 15, and the missile 3 is set vertically by a hydraulic cylinder 14. The missile can be launched by a signal from the controller 8. The trailer 9 in which the launching is finished can be replaced with a trailer 9A to be able to launch.
109	Jet deflecting device for flying body launcher	JP22805791	1991-09-09	JPH0571895A	1993-03-23	MURAOKA NOBUYUKI
PURPOSE:To operate a jet deflecting device installed to a firing vehicle of a flying body automatically, promptly and safely and hold the device during driving the firing vehicle in a stabilized manner. CONSTITUTION:The titled jet deflecting device comprises a jet deflecting board 4 mounted rotatively on the end of a firing vehicle 5, a drive cylinder 1 which rotates the jet deflecting board 4 installed to the firing vehicle 5 and a deflecting board support fitting 3 which couples the firing vehicle 5 which the jet deflecting board 4 removably.
110	Flying object launcher	JP19320591	1991-08-01	JPH0539998A	1993-02-19	KODAMA MASARU; SUGIYAMA KATSUMASA; NAKAMURA TETSUHITO
PURPOSE:To surely prevent a launcher tube, etc., from being damaged by back- flow of gas blast from a flying object on to a deflection plate by certainly deflecting the gas blast by the deflecting plate. CONSTITUTION:Launcher tubes 4 stand upright, and a deflection plate 13 is placed under the launcher tubes 4 at a specified angle to the launcher tubes 4. A block 14 is attached near the upper edge of line upper face of the deflection plate 13. The block 14 is attached along the whole width of the deflection plate 13 as seen from back. Within a range the block 14 can be attached, the higher the position of the block 14, the better, and it is preferable to attach it at a position a little (about 10cm) outside the position where the gas blast 2 directly strikes on the deflection plate 13. As the block 14 is attached on the deflection plate 13 to check the back-flow 12 of gas blast 2 that is generated on the deflection plate, the launcher tubes 4, etc., are certainly prevented from being thermally damaged.
111	Missile launching device	JP17141091	1991-07-11	JPH0518696A	1993-01-26	KODAMA MASARU; SUGIYAMA KATSUMASA
PURPOSE:To obtain a missile launching device, capable of deviating the flow of ejecting gas of a missile surely to the lateral direction so as not to wind up gravels, sand and the like on the surface of ground and preventing the circulation of ejected gas to prevent the damage of a launching tube, a vehicle and the like surely. CONSTITUTION:In a missile launching device equipped with a plurality of rows of launching tubes 4 launching missiles 3 vertically flow deflecting plates 1 guiding the ejected gas 2 of the missiles 3 respectively into predetermined directions are provided at the lower side of the launching tubes 4 of each rows. The flow deflecting plates are provided in respective rows for a plurality of rows of the missiles whereby the ejected gas of the missiles in respective rows can be deflected effectively into lateral directions whereby the damaging of the launching tubes, a vehicle and the like upon launching the missiles can be eliminated. On the other hand, the launching device can be compacted.
112	Flying body shooting apparatus	JP4223791	1991-02-15	JPH04356699A	1992-12-10	MURAOKA NOBUYUKI; WATANABE OSAMU
PURPOSE: To ensure the use of a title apparatus even in a narrow space without causing a danger of fires even in the narrow space such as those in a valley and a forest, etc., by increasing the degree of freedom of an installation place. CONSTITUTION: There are provided a jetting gas deflection plate 11 disposed backwardly of the shooting of a flying body for deflecting jetting gas 6 from the flying body, and a voltex generator 12 mounted at a location of the jetting gas deflection plate 11 through which the jetting gas passes for generating a turbulent flow. The jetting gas 6 deflected by the jetting gas deflection plate 11 is diffused by the voltex generator 12 to produce a turbulent flow and hereby uniformize the temperature and velocity distributions. COPYRIGHT: (C)1992,JPO&Japio
113	Missile charging device for launcher	JP6212391	1991-03-26	JPH04297795A	1992-10-21	MURAOKA NOBUYUKI; KOBAYASHI SUMIYUKI
PURPOSE: To perform an efficient and safe operation for loading a missile into a launcher and also perform an efficient and safe operation of unloading of a used protection cage from the launcher. CONSTITUTION: This device comprises an air pallet 6 for use in mounting a protection case 3 having a missile therein, an air pallet sliding device 17, a height adjusting out-trigger 11, a guide for preventing a lateral displacement of the air pallet and a protection cage fixing lock device. The air pallet 6 is floated by blowing pressurized air downwardly and it is characterized in that it is moved toward a launcher 4 under an operation of the sliding device 17. COPYRIGHT: (C)1992,JPO&Japio
114	Launcher for missile	JP5460491	1991-03-19	JPH04292798A	1992-10-16	GOUKI JIYUNICHI
PURPOSE: To prevent occurrence of sand dusts, jumping stones due to a jet, to prevent transmission of a reaction due to deflection of the jet to a launcher and to remove detrimental gas, smoke, etc., in the jet. CONSTITUTION: A bag 1 in contact with the ground surface, in which a jet of a missile is introduced, is installed at a downstream side of a launching cylinder 4 to prevent occurrence of sand dusts, jumping stones, etc., due to the jet, and a reaction due to deflection of the jet is received by the ground surface. A catalytic converter 2 for removing detrimental gas, smoke, etc., in the jet and/or a silencer 3 are provided at a downstream side of the bag 1. COPYRIGHT: (C)1992,JPO&Japio
115	JPH04115297U -	JP1994391	1991-03-29	JPH04115297U	1992-10-13

116	JPH01129595U -	JP2179588	1988-02-23	JPH01129595U	1989-09-04

117	JPS4988400A -	JP13446873	1973-12-03	JPS4988400A	1974-08-23

118	JPS4988399A -	JP13446773	1973-12-03	JPS4988399A	1974-08-23

119	MULTI-PURPOSE MISSILE LAUNCHER SYSTEM FOR A MILITARY LAND VEHICLE	PCT/US0209242	2002-03-25	WO02103276A3	2003-05-08	BOUDREAU DAVID R; BOVEE STAN; MATTESON PHILIP; GAEDKE BRUCE; BORGWARTH DENNIS
A multi-purpose missile launcher system 10 for a military land vehicle 12 that has the capability for direct targeting both short and medium range land targets, as well launching missiles against longer-range land targets or air targets using indirect targeting. The multi-purpose missile launcher system is deployed as part of a modular weapon system that mates with a modular bed of the military land vehicle 12.
120	MULTIPLE TUBE PNEUMATIC LAUNCHER	PCT/US2004009427	2004-03-29	WO2005001372A3	2005-08-11	MILLER STEPHEN W; FOX STEVEN J; FEILD DAVID M; BAUERNSCHUB RICHARD A; METTEE JUSTIN A
A launcher includes a plurality of launch tubes (110) for stowing and launching a plurality of air vehicles. A central air manifold (310) is operatively connected to an air storage tank (150); a first launch tube air manifold (320) is operatively connected to a first group of the launch tubes (110) and operatively connected to the central air manifold (310). The first launch air manifold (320) has a separate port corresponding to each launch tube (110) of the first group of launch tubes. A release valve mechanism (360) is removably mounted in one of the ports (355) of the first launch tube air manifold (320), the release valve mechanism (360) controlling the passage of launch air between the first launch tube air manifold (320) and the launch tube corresponding to the port (355) in which the release valve mechanism (360) is mounted. A plug (350) is removably mounted in each of the ports (355) not occupied by the release valve mechanism (360).

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