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1. 发明专利

JPH1150911A SOLID ROCKET AND ITS OSCILLATING COMBUSTION RESTRAINING METHOD 失效
公开(公告)号：JPH1150911A
公开(公告)日：1999-02-23
申请号：JP20936297
申请日：1997-08-04
申请人： NISSAN MOTOR
发明人： KUWABARA TAKUO
IPC分类号： F02K9/14
摘要： PROBLEM TO BE SOLVED: To realize restraint of oscillating combustion without influencing upon characteristics of combustion speed, etc., of a solid propellant by providing a solid particle producing mechanism to produce solid particles to function as an oscillating combustion restrainer on the upstream side of the solid propellant. SOLUTION: A solid rocket 11 is constituted by providing an insulation 13 on the inner surface of a cylindrical pressure container 12 and loading a solid propellant 14 in the inside of this insulation 13. A nozzle 15 is provided on the downstream side of the solid propellant 14, and an igniter 16 is provided on the upstream side of the solid propellant 14. The igniter 16 contains an oscillating combustion restrainer and ZrC powder to function not to inhibit turning to be smokeless or lean-smoke, and this igniter 16 is structured to doubly work as a solid particle producing mechanism 17. Consequently, on the solid rocket 11, ZrC solid particles are supplied from the solid particle producing mechanism 17 doubly to use by the igniter 16 while the solid propellant 14 is ignited by the igniter 16 and burns and thrust is generated as combustion gas is blown out from the nozzle 15.

2. 发明专利

JPH074660A COMBUSTION HEATER 失效
公开(公告)号：JPH074660A
公开(公告)日：1995-01-10
申请号：JP14624393
申请日：1993-06-17
申请人： HITACHI LTD , NISSAN MOTOR
发明人： YOSHINO TOMOYA , YOSHIDA MASAHIRO , ISHIGAMORI ISAO , HASHIMOTO TAKASHI , NINOMIYA KAZUYOSHI , KUWABARA TAKUO , KONO MINORU
IPC分类号： F02K7/10 , F23R3/00 , F23R3/28 , F23R3/42 , G01M15/00 , G01M15/14
摘要： PURPOSE:To provide a combustion heater which is capable of stably producing high temperature high pressure gas with uniform total temperature, and in which reduction of heat load of an internal cylinder with the aid of secondary air is satisfactory, and in which damage by a fire due to adhesion of a kept flame can reliably be prevented. CONSTITUTION:A conical internal cylinder 4 is provided at an upstream portion in an external cylinder constituting a combustion chamber, to which secondary air is directly uniformly blown out from a mixing air supply nozzle 2b. The combustion chamber is divided into a combustion region 5 and a secondary air passage 7 through the internal cylinder 4, and a mixing air passage outlet 7a is constructed such that flow velocity of mixing air is 0.8 times or more the flow velocity of combustion gas. Into the combustion region 5, a fuel and an oxydizing agent flow to produce the combustion gas. The oxydizing agent supplied to the secondary air passage 7 cools the internal cylinder 4 uniformly and is fed to a mixing region 6 from the mixing air pasasge outlet 7a. Hereby, the internal cylinder 4 is effectively uniformly cooled with the aid of the secondary air, and simultaneously the internal cylinder 4 is prevented from being burned owing to adhesion of a flame at the secondary air outlet.

3. 发明专利

JPH0586980A LIQUID RAM ROCKET 失效
公开(公告)号：JPH0586980A
公开(公告)日：1993-04-06
申请号：JP25150691
申请日：1991-09-30
申请人： JAPAN TECH RES & DEV INST , NISSAN MOTOR
发明人： KUBOTA NAMINOSUKE , WATANABE HISAYUKI , KONO MINORU , KUWABARA TAKUO
IPC分类号： F02K7/18 , F02K9/76 , F02K9/95
摘要： PURPOSE:To obviate an ignition device and to maintain combustion in an excellent state by providing a combustion gas generating means to generate combustion gas for both ignition and stabilization of flame of fuel-air mixture to feed it in a combustion chamber, in a device having a combustion chamber to burn fuel-air mixture of liquid fuel and air. CONSTITUTION:A liquid ram rocket 1 has a combustion chamber 3 charged with a booster propellant 2. A booster nozzle 4 and a ram rocket nozzle 5 are concentrically arranged to the rear end part of the combustion chamber 3 through a separating coupling 6. The front side of the combustion chamber 3 is filled with liquid fuel 11 and a fuel tank 12 the size of which is reduced through pressurization, a flow rate control device 13, and a fuel injection valve 14 are provided. In this case, a gas generating chamber 17 filled with solid fuel 16 serving as a combustion gas generating means is located on a machine shaft on the front side of the combustion chamber 3. The chamber 17 is provided with an ignition device 18 for solid fuel and a gas injection nozzle 19 for both ignition and stabilization of flame, and combustion gas is injected in the combustion chamber 3 through the nozzle 19 to both ignite fuel-air mixture and stabilize flame.

4. 发明专利

JPH04275992A GAS GENERATING AGENT 失效
公开(公告)号：JPH04275992A
公开(公告)日：1992-10-01
申请号：JP3621591
申请日：1991-03-01
申请人： JAPAN TECH RES & DEV INST , NISSAN MOTOR
发明人： KUBOTA NAMINOSUKE , MIYATA YUKIO , KUWABARA TAKUO , KONO MINORU , NAKAGAWA ICHIROU
IPC分类号： C06D5/00 , C06D5/06
摘要： PURPOSE:To increase specific propelling force by compounding a specified amt. of Ti powder of specified particle size into one or more kinds of metal fuels selected from B and magnalium. CONSTITUTION:A gas generator as a sustainer propellant for a solid ram rocket is prepared by compounding 1-5wt.% Ti powder of

5. 发明专利

JPH04204134A STOPPING METHOD OF WIND TUNNEL APPARATUS 失效
公开(公告)号：JPH04204134A
公开(公告)日：1992-07-24
申请号：JP33053090
申请日：1990-11-30
申请人： HITACHI LTD , NISSAN MOTOR
发明人： TAKAKUSAKI TSUNEHIKO , YOSHIDA MASAHIRO , ISHIGAMORI ISAO , HASHIMOTO TAKASHI , TSUBOUCHI KUNIYOSHI , NINOMIYA KAZUYOSHI , KUWABARA TAKUO , KONO MINORU
IPC分类号： G01M9/02
摘要： PURPOSE:To make it possible to restore pressure at the time of stop when a flow-path closing means is omitted by providing a vacuum brake valve, introducing air from a high-pressure gas feeding source through a gas heating part and a nozzle, and stopping a fluid jetting means at a specified time constant. CONSTITUTION:A vacuum brake valve 6 for introducing atmosphere into a low-pressure chamber 3 when an apparatus is stopped is provided. Air for restoring the pressure in the chamber 3 is introduced from a main flow-path pipe 7 from a high-pressure gas feeding system on the upstream side through a lean burning heater 1 and a nozzle 2. An ejector 5 of a fluid jetting means which sets the pressure in the chamber 3 at the constant low-pressure state is stopped at a certain time constant. These parts are associatively operated automatically. When the apparatus is stopped, the pressure in the chamber 3 and the air from the valve 6 and the high-pressure-gas feeding system are used together during the period from the stopping command of the ejector 5 to the complete stopping. Thus the apparatus can be smoothly stopped without the breakdown of the ejector 5.

6. 发明专利

JPH02163448A GAS GENERATOR FOR RAM ROCKET 失效
公开(公告)号：JPH02163448A
公开(公告)日：1990-06-22
申请号：JP31616388
申请日：1988-12-16
申请人： JAPAN TECH RES & DEV INST , NISSAN MOTOR
发明人： KUBOTA NAMINOSUKE , WATABE YASUSHI , NINOMIYA KAZUYOSHI , KUWABARA TAKUO , KONO MINORU
IPC分类号： F02K7/18
摘要： PURPOSE:To improve the durability of a sealing for a pintle and obtain a small- sized pintle driving source by installing a driving means which moves the pintle in reciprocation in the axial direction at the basic edge part of the pintle whose top edge projects to the center of the opened port part of a nozzle. CONSTITUTION:When the internal pressure of a tank 3 or the introduced air pressure varies, a gas generator 1 drives a servomotor 19 by an instruction signal supplied from a servoamplifier 27 according to a pressure signal B, and the position detection signal A of a pintle 12 by a potentiometer 26. The pintle 12 is shifted in the axial direction through a ball screw 18 and a nut holder 24, and the opening area of a nozzle 5 varies to adjust the flow rate for the combustible gas. Therefore, in a ram rocket, the combustion in a combustion chamber 4 and the thrust are stabilized by the gas generator 1. In the gas generator 1, only the top edge of the pintle 12 projects from a pintle case 6, and the structure in which the influence of the pressure of the gas stream is little is obtained, and the pintle 12 can be sufficiently driven by a small driving source.

7. 发明专利

JPH01110867A CARBON COMPOUND MATERIAL COMBUSTION DEVICE 失效
公开(公告)号：JPH01110867A
公开(公告)日：1989-04-27
申请号：JP26523987
申请日：1987-10-22
申请人： NAT AEROSPACE LAB , NISSAN MOTOR
发明人： MIYAJIMA HIROSHI , KOSAKA KATSUAKI , KUWABARA TAKUO
IPC分类号： F02K9/62
摘要： PURPOSE:To improve strength and durability of a combustion device by provid ing a silicon carbide coating layer in the internal surface of a carbon compound material while a chemical vapor deposition film of carbon in the external sur face of this carbon compound material. CONSTITUTION:A carbon compound material 23, serving as the main unit of a combustion device 11, respectively provides a silicon carbide coating layer 24 in the internal surface of the material 23 and a chemical vapor deposition film 25 of carbon in the external surface. Thus providing sufficient air-tightness in the carbon compound material 23, it surely inhibits high pressure gas from its transmission to the material while remarkably improves its corrosion resis tance. While by covering respectively the internal and external surfaces of the carbon compound material 23 with the fine and hard quality coating layer 24 and the chemical vapor deposition film 25, the carbon compound material 23 enables its existing surface flaw to be completely embedded as well as suffi ciently prevent the generation of a new surface. Further the carbon compound material 23 in its turn the combustor 11 remarkably improves its strength and durability. Here the silicon carbide coating layer 24 can be formed by diffusion, conversion, etc., in addition to coating of silicon carbide.

8. 发明专利

JPS57119147A Ram rocket 失效
标题翻译： RAM ROCKET
公开(公告)号：JPS57119147A
公开(公告)日：1982-07-24
申请号：JP579381
申请日：1981-01-16
申请人： Nissan Motor Co Ltd
发明人： KUWABARA TAKUO , KOSAKA KATSUAKI , NOTAKE SHINJI
IPC分类号： F02K7/18
CPC分类号： F02K7/18
摘要： PURPOSE:To obtain a prescribed thrust, by radially providing numerous through holes in a fuel liner fitted in a main fuel combustion chamber, to conduct a part of external air to completely burn fuel gas. CONSTITUTION:A plurality of grooves 20 are provided on the peripheral surface 8b of a cylindrical fuel liner 8 so that the grooves extend in the axial direction. The liner 8 is provided with numerous through holes 21 which extend radially and connect the grooves 20 to the inside 8a of the liner. Inflammable gas of high temperature, which is produced in a primary combustion chamber 3 by the combustion of a solid propellant 5, is supplied into a secondary combustion chamber 4 through the numerous holes 10a of an ejector 10. At the same time, compressed air is supplied into the secondary combustion chamber 4 through an air inlet port 7. A part of the air is blown into passages 22 and drastically mixed with the inflammable gas to ingnite it. As a result, combustion is uniformly progressed in the chamber 4.
摘要翻译：目的：为了获得规定的推力，通过在安装在主燃料燃烧室中的燃料衬套中径向提供许多通孔，以使一部分外部空气完全燃烧燃料气体。构成：在圆筒形燃料衬套8的周面8b上设置多个槽20，使得槽沿轴向延伸。衬套8设置有许多径向延伸的通孔21，其将槽20连接到衬套的内部8a。通过固体推进剂5的燃烧在一次燃烧室3中产生的高温易燃气体通过喷射器10的多个孔10a供给到二次燃烧室4.同时，压缩空气是通过空气入口7供应到二次燃烧室4中。一部分空气被吹入通道22中，并与易燃气体大量混合以使其熔化。结果，在室4中燃烧均匀地进行。

9. 发明专利

JP2000007479A TITANIUM/CARBON PTFE BASED MIXTURE FOR HEAT SOURCE AND GAS GENERATING AGENT AND HEAT GENERATING AGENT 失效
公开(公告)号：JP2000007479A
公开(公告)日：2000-01-11
申请号：JP16882598
申请日：1998-06-16
申请人： HOSOYA FIREWORKS , NISSAN MOTOR
发明人： TAKIZUKA MICHINORI , ONDA TOSHIO , KUWABARA TAKUO
IPC分类号： C06B43/00 , C06D5/00
摘要： PROBLEM TO BE SOLVED: To provide a Ti/C/PTFE based mixture suitable for a heat source material of a heat source-blending composition such as a gas generating agent generating a large quantity of a gas or a heat generating agent generating a large quantity of heat. SOLUTION: The Ti/C/PTFE composition consists essentially of 40-80 pts.wt. Ti, 20-60 pts.wt. C, 5-20 pts.wt. PTFE and 1-10 pts.wt. binder and is suitable for the heat source material of the heat source-blending composition such as the gas generating agent or the heat generating agent. The gas generating agent and the heat generating agent are obtained by blending the Ti/C/PTFE based mixture.

10. 发明专利

JPH11322483A IGNITER FOR SOLID ROCKET MOTOR 失效
公开(公告)号：JPH11322483A
公开(公告)日：1999-11-24
申请号：JP13886298
申请日：1998-05-20
申请人： HOSOYA FIREWORKS , NISSAN MOTOR
发明人： TAKIZUKA MICHINORI , ONDA TOSHIO , KUWABARA TAKUO
IPC分类号： C06B43/00 , C06D5/06
摘要： PROBLEM TO BE SOLVED: To increase the density and the calorific value per unit weight or gas amt. produced per unit time and to decrease the weight for required energy by constituting an igniter essentially comprising Ti and PTFE (polytetrafluoroethylene). SOLUTION: The igniter is produced by compounding about 40 to 80 pts.wt. Ti and about 20 to 60 pts.wt. PTFE as the main components and a binder, and forming into pellets. The binder is incorporated by about 1 to 20 pts.wt. The pellet is preferably formed into 0.1 to 20 mm size. The particle size of metal Ti used is preferably 20 to 80 μm. Or, a part of Ti may be substituted with Mg. The density of PTFE is preferably about 2.17 g/cm . The PTFE is used in a molding powder or fine powder state, and preferably about 5 to 200 μm in size when used as the source material.

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