| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 81 | Jet gas deflecting plate for missile launcher | JP25356991 | 1991-10-01 | JPH0593597A | 1993-04-16 | MURAOKA NOBUYUKI; TODA KATSUAKI |
| PURPOSE:To contrive the reduction of weight and the improvement of heat resistant property by a method wherein the main body or the jet gas deflecting plate of a missile launcher, which deflects the direction of jet gas of a missile, is made of light metal material and heat resistant coating is applied on the surface of the main body. CONSTITUTION:A deflecting plate 3 is constituted of a main body 1, consisting of a light metal material, and heat resistant coating 2, applied on the surface of the main body 1. Mounting fittings 4 are provided on one end face of the main body 1. Anticorrosion aluminum alloy, for example, is used for the light metal material forming the main body 1 while epoxyamide material or RTV silicone, having heat insulating property, for example, is used for a material forming the heat resistant coating 2. In this case, the deflecting plate 3 is constituted of the main body 1 of light metal material and the heat resistant coating 2 applied on the surface of the main body 1 whereby the weight of the deflecting plate can be reduced and sufficient heat resistant property against the high- temperature jet gas of a missile, which is received by the deflecting plate 3, can be ensured. | ||||||
| 82 | Jet gas diffusion device for missile launcher | JP7868191 | 1991-02-15 | JPH0593595A | 1993-04-16 | INOUE MASAO; WATANABE OSAMU |
| PURPOSE:To permit the installation of a launcher in a canyon, forest and the like without spreading the danger of generating fire due to high-temperature jet gas to a wide range, in the jet gas diffusion device for the missile launcher, in which the diffusion of high-temperature and high-speed jet gas is promoted upon launching a missile. CONSTITUTION:A jet gas deflecting plate 21, deflecting the direction of jet gas 17 from a missile 13, is provided with a plurality of nozzles 22a-22h for injecting cooling water. High-pressure cooling water is injected concentratedly from the nozzles 22a-22h against the hot gas 7 to form a vortex generating device, formed of a plurality of water columns 23a-23h, in the jet gas 17. | ||||||
| 83 | Jet gas deflection plate of the flying object launchers | JP7314691 | 1991-09-11 | JPH0525194U | 1993-04-02 | 純之 小林; 勝昭 戸田; 信之 村岡 |
| (57)【要約】 【目的】 飛翔体発射機の噴流ガス偏向板を、耐熱性があり、かつ、軽量のものとする。 【構成】 飛翔体の噴流ガスを偏向させる飛翔体発射機の噴流ガス偏向板３を、偏向板本体１と同偏向板本体１
に取付けられた耐熱材料よりなる噴流受け部２とによって構成した。 |
||||||
| 84 | Flying body shooter | JP4223891 | 1991-02-15 | JPH04356700A | 1992-12-10 | MURAOKA NOBUYUKI; WATANABE OSAMU |
| PURPOSE: To ensure the use of the title shooter even in a narrow space, to install the shooter stably, to reduce the danger zone around the shooter and to lower the limit of installing the shooter by greatly reducing the force exerted on the shooter body by jetted gas to a low level at which the force is not a problem. CONSTITUTION: A jetted gas divider 11 for halving jetted gas 6 from a flying body is disposed in a place back of the flying body where the jetted gas 6 directly strikes the flying body, and each jetted gas flow halved by the divider 11 is deflected by deflection plates 12, 12a, 12b, 12c, 12d arranged into a substantially curved shape as a whole. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 85 | Deflecting device for jet stream gas generated upon launching missile | JP4352191 | 1991-03-08 | JPH04281198A | 1992-10-06 | MURAOKA NOBUYUKI; WATANABE OSAMU |
| PURPOSE: To reduce a force applied on a launcher by a method wherein the launching of the missile is permitted at a narrow place and jet stream gas, generated upon launching the missile, is deflected upwardly. CONSTITUTION: The title device is provided with a deflecting plate 2, deflecting jet stream gas 5, generated upon launching a missile and ejected downwardly into obliquely downward direction and deflecting it upward further, and a separator 3, arranged in the jet stream gas deflected upward and mixing the jet stream gas with ambient air through turbulent flow mixing. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 86 | Level setter for missile launcher | JP2236891 | 1991-02-15 | JPH04260798A | 1992-09-16 | INOUE MASAO; WATANABE OSAMU |
| PURPOSE: To safely and rapidly set a level by providing a hydraulic actuator deviation detector, and a body pitching/ rolling direction attitude angle detector, and controlling other hydraulic actuator with one hydraulic actuator as a reference according to the outputs of the detectors and a set level value. CONSTITUTION: A launcher 1 is installed on the ground inclined at a pitch angle θ and a roll angle ϕ to a horizontal plane, and a reference surface of the launcher is altered with a O point as a reference. That is, since the ground is inclined at the angle ϕ, a deviation (a) is added, and since the ground is inclined at the angle ϕ, a deviation (b) is added, and the reference surface of the launcher is set to a level equivalently to the horizontal plane. A reference hydraulic actuator is set by detecting the roll angle by an attitude angle detector 8, and a deviation command signal of other actuator is calculated. A controller 7 transmits a control signal based on a command value to a servo valve 4, and alters hydraulic pressure of a hydraulic pressure supply unit 5. This pressure is transmitted to the hydraulic actuator 2 to deviate its level. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 87 | Jet gas deflecting reaction cancelling device for missile | JP2236791 | 1991-02-15 | JPH04260797A | 1992-09-16 | OGAWA MOTOHIDE; WATANABE OSAMU |
| PURPOSE: To eliminate a supporting mechanism for receiving a force (FX) for pressing a launcher forward and to launch a missile from a narrow place by U-shape turning a jet gas of the missile to guide it upward (in a missile launching direction). CONSTITUTION: A U-turn type jet gas deflector 11 formed in a sectional shape for U-shape turning a jet gas is provided in a jet gas deflecting mechanism 6 of a self-traveling type ground launcher to guide the jet gas 2 of a missile 3 upward (in a missile launching direction). COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 88 | Supporting device for missile launching apparatus | JP2232091 | 1991-02-15 | JPH04260795A | 1992-09-16 | MURAOKA NOBUYUKI; WATANABE OSAMU |
| PURPOSE: To eliminate an increase in a weight of a structure by dispersing a load to be applied to a jet gas deflector even if the surface of the ground on which a selftraveling type ground launching apparatus is installed, is not horizontal. CONSTITUTION: Telescopic type supporting legs 1 are mounted on a bottom of a gas jet deflector 7 in a self-traveling type ground launching apparatus, telescoped by actuators 4 to close a gap between the surface of the ground and the deflector 7, the deflector 7 is supported, and a load to be applied to the deflector is dispersed together with jacks to be transmitted to the ground. COPYRIGHT: (C)1992,JPO&Japio | ||||||
| 89 | Blast shielding device in guided missile launchers | JP2004340915 | 2004-11-25 | JP4384968B2 | 2009-12-16 | 耕平 山本 |
| 90 | Blast shielding device for missile launcher | JP2004340915 | 2004-11-25 | JP2006153302A | 2006-06-15 | YAMAMOTO KOHEI |
| <P>PROBLEM TO BE SOLVED: To provide a blast shielding device using a blast shielding panel for shielding blast from the exhaust port of a missile launcher tube of a missile launcher without involving a transportation vehicle while reducing the influences of dust swirled by the blast on the side of the transportation vehicle. <P>SOLUTION: The blast shielding panel P is provided on the transportation vehicle V at the rear part of a launcher frame 4 on which the missile launcher tube 5 is mounted. The blast shielding panel P consists of a reversible frame P1 provided on the launcher frame 4 in an up-and-down reversible manner, a plurality of telescopic panel P2 individually provided on the reversible frame P1 in a telescopic manner, and a cover panel P3 for shielding the reversible frame P1. When the launcher frame 4 is raised up, the telescopic motion of the individual telescopic panels P2 are controlled so that their front ends are grounded. <P>COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
| 91 | Self-propelling missile launching apparatus | JP2002199552 | 2002-07-09 | JP2004044826A | 2004-02-12 | TANGE TOSHIAKI |
| PROBLEM TO BE SOLVED: To provide a self-propelling missile launching apparatus capable of preventing occurrence of torsion in setting a horizontal position on an irregular ground without increasing apparatus weight, improving service life of the apparatus, improving accuracy of the horizontal position setting, and improving launching accuracy of a missile. SOLUTION: The self-propelling missile launching apparatus has a launching mechanism on a vehicle. The launching mechanism has a lower frame mounted on a frame of the vehicle, and an upper frame that is mounted on the lower frame via a hinge, can be vertically turned around the hinge by a lifting device, and supports the missile. The missile launching apparatus has a jack for supporting and lifting the frames of the vehicle right and left on the front side and rear side of the vehicle. A plurality of tilt angle meters for detecting a tilt angle with respect to the horizontal plane of the launching mechanism are disposed in the longitudinal direction of the vehicle, and the jack is controlled based on the detected signals of the plurality of tilt angle meters. COPYRIGHT: (C)2004,JPO | ||||||
| 92 | Launcher for missile | JP8549692 | 1992-04-07 | JPH05288494A | 1993-11-02 | HAMADA TETSUYA |
| PURPOSE: To permit the obtaining of a large firing elevation upon launching a missile by a method wherein an air bag, propelling the missile, is attached to the inside of a launching tube for launching the missile while a gas generator, exploded by ignition and elongate the air bag, is provided in the air bag. CONSTITUTION: The launching device, arranged on a self-propelling vehicle and the like, is provided with an air bag 1, elongated into the launching direction of a missile 5 and propelling the missile 5 through a pressure receiving plate 3, in a launching tube 6 while a gas generator 2, exploded when ignited through an ignition controller 4 and inflating suddenly the gas in the air bag 1 to elongate the air bag 1, is provided in the air bag 1. The air bag 1 is formed of 'Kevlar(R)' woven cloth or the like coated with chloroprene rubber and is stored in the bottom part of the launching tube 6 under a condition that it is folded before launching. The missile 5 is launched by the air bag 1 inflated suddenly and after the missile is released from the launching tube 6, a booster is ignited and propulsion is continued by the booster. COPYRIGHT: (C)1993,JPO&Japio | ||||||
| 93 | Missile launcher | JP6718192 | 1992-03-25 | JPH05272891A | 1993-10-22 | Toru Kogure; 亨 木暮 |
| PURPOSE: To safely charge a missile in a launcher in a short time. CONSTITUTION: A float-and-sink type pulley block 2 which vertically slides and a floating and sinking unit 8 are provided in a trestle 6 in which a missile 5 is fixed and a launching angle is set. Pulleys, a missile lifting chain 3 and a chain winding unit 4 are provided in the block 2. COPYRIGHT: (C)1993,JPO&Japio | ||||||
| 94 | Missile launcher | JP25655391 | 1991-10-03 | JPH0593598A | 1993-04-16 | KODAMA MASARU; SUGIYAMA KATSUMASA |
| PURPOSE:To obtain a missile launcher equipped with a deflecting plate capable of preventing the noise of jet gas of a missile, the heat damage of a launching tube and the like due to the reverse flow of the jet gas, the winding-up of sand, gravels, grass, wood and the like due to the jet gas. CONSTITUTION:A missile launching device is provided with a flat plate 16 and a flow deflecting plate 15, provided with a mesh type material 17 mounted on the side of the flat plate, against which the jet gas 2 of the missile is collided. On the other hand, a plate having recessed and projected colliding surface of jet gas 2 is provided instead of the flat plate 16 and the colliding surface of the jet gas 2 of the flat or recessed and projected plate is slanted or resistant plates, flow guiding members and reverse flow preventing members are provided in the mesh type material. Further, a perforated plate, a multi-groove plate or the like is mounted on the jet gas colliding side of the mesh type material to protect the mesh type material. | ||||||
| 95 | Missile launcher | JP25356891 | 1991-10-01 | JPH0593596A | 1993-04-16 | MURAOKA NOBUYUKI; KOBAYASHI SUMIYUKI |
| PURPOSE:To permit the loading and/or unloading of a missile with reduced number of men in a stabilized condition by a method wherein the title device is provided with a gate crane having a parallelogram leg as well as two sets of hoists on the upper part of the same and pivotable back and forth, or a launching trestle, pivotable upward by a predetermined angle back and force about one end thereof. CONSTITUTION:A launcher 4 is provided with a gate crane 6, whose side surface forms a parallelogram, while the crane can be pivoted while forming a parallelogram. Further, the gate crane is provided with two sets of hoists 7 on the upper part of the gate. According to this constitution, 6 rounds of missiles, put on the arbitrary positions on the ground, can be loaded and/or unloaded in one time in stabilized condition. In this case, the hanging points of the missile 3 are two points whereby stabilized hanging condition can be obtained. On the other hand, the launching trestle 6, mounted on the launcher 4, is constituted so as to be rotatable within 180 deg. whereby 6 rounds of the missiles, positioned at arbitrary positions on the ground, can be loaded and/or unloaded in one time in stabilized condition. | ||||||
| 96 | Loading device for missile into launcher | JP9345891 | 1991-03-30 | JPH0593594A | 1993-04-16 | OGAWA MOTOHIDE; KOBAYASHI SUMIYUKI |
| PURPOSE:To carry out the loading work of a missile into a launcher and the unloading work of a used protection cage from the launcher efficiently and safely. CONSTITUTION:A missile loading device for a launcher is constituted of a fixed type boom 6, hanging a protection cage 3 receiving the missile, a horizontal regulating and retaining device 7, a hanging metal 8 and outriggers 9. The fixed type boom 6 lifts up the protection cage 3, receiving the missile, while preventing the swing of the protection cage 3 by the horizontal regulating and retaining device 7 to move the missile into the launcher 4. | ||||||
| 97 | Missile launching device | JP25148891 | 1991-09-30 | JPH0587494A | 1993-04-06 | KODAMA MASARU; SUGIYAMA KATSUMASA |
| PURPOSE:To prevent sand, gravles, grass and wood or the like from being swirled up with discharged gas of a missile in a missile launching machine and to reduce noise. CONSTITUTION:A flow deflecting device 14 for injection gas 2 of a missile is made into a duct shape, a sound absorbing material 15 is installed inside the duct and a vane 16 for guiding injection gas 2 is installed. An injection gas guiding straightener plate is disposed in parallel with the deflector plate while being spaced apart thereto. An injection gas guiding straightener plate extending in a lateral direction of the deflector plate and forming a certain angle with respect to the deflector plate is provided. The deflector plate is provided with a flap which can be moved around a hinge in a lateral direction of the deflector plate. A movable flap is arranged around a hinge in a lateral direction of the deflector plate. A column or rotary column with a sound absorbing material is disposed in a lateral direction of the deflector plate. | ||||||
| 98 | Jet deflecting device for flying body launcher | JP23615791 | 1991-09-17 | JPH0571896A | 1993-03-23 | MURAOKA NOBUYUKI; KOBAYASHI SUMIYUKI |
| PURPOSE:To make it possible to clear the height limitations imposed by the Road Traffic Act by lowering the height of a jet deflecting device of a flying body launcher during running time. CONSTITUTION:The titled jet deflecting device comprises a main body 1a pivoted to a launcher 11 mounted around a horizontal shaft of a firing vehicle rotatively by way of a horizontal shaft 7a and a front end section 4 pivoted to the main body 1a by way of a horizontal shaft 5. The both ends of the device are pivoted to a deflecting board 1 of a flying body jet which rotates between a rising position and a falling position, a front end section 4 and the launcher 11. The front end section 4 is stretched on the extension of the main body 1 at the falling position while at the rising position there is installed a link 3 which folds the front end section 4. | ||||||
| 99 | Vertical launcher | JP19934091 | 1991-08-08 | JPH0545093A | 1993-02-23 | KODAMA MASARU; FUKUMOTO KIICHI; SUGIYAMA KATSUMASA; NAKAMURA TETSUHITO |
| PURPOSE:To prevent generation of counter flow of ejection gas of a missile by installing an offset whose vehicle side is higher on the surface of a drift board located near the vehicle in a vertical launcher provided with the drift board slanting installed below a launching cylinder when launching a vehicle- mounted missile from a vehicle. CONSTITUTION:A vertical launcher of a vehicle-mounted missile launches a missile 3, rotating a launcher cylinder 4 around a hinge 5 of a vehicle 7 and keeping the cylinder in a vertical state. On the end of the vehicle is slantingly installed a drift board 14 whose one end is mounted with a hinge and whose other end is lowered below the launcher cylinder 4 when it is used. In this case, no attempt is made to flatten the surface of the drift board 14 but to install an offset 15 which is higher on the vehicle side, on the surface of the board near the vehicle 7, which forces the ejection gas 2 of a missile engine to collide with the surface of the drift board 14. When a counter flow 12 is partially generated, the counter flow 12 is checked at the offset 15 so as to protect the launcher cylinder 4 or the like from thermal damage. | ||||||
| 100 | High temperature-high speed jet gas diffusion accelerator | JP2236991 | 1991-02-15 | JPH04260799A | 1992-09-16 | OGAWA MOTOHIDE; WATANABE OSAMU |
| PURPOSE: To reduce temperature and speed of jet gas and to reduce a force for pressing a launcher forward to be generated by jet gas deflection rearward of the launcher by quickly making protruding temperature.speed distribution of high temperature.high speed jet gas to be ejected at the time of launching a missile uniform. CONSTITUTION: A vortex generator 2 for inducing strong turbulent flow mixture by accelerating generation of turbulent flow of jet gas 13, is provided on a jet gas deflector 1 for deflecting the high temperature.high speed jet gas 13 to be ejected at the time of launching a missile mounted in a launching cylinder 14 rearward of a launcher. Many nozzles 4 for ejecting coolant into the gas 13 only for a period for supplying high pressure coolant stored in an accumulator 6 to the generator 2 through a coolant supply tube 10, is provided. COPYRIGHT: (C)1992,JPO&Japio | ||||||
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