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21. 发明专利

JPH1122555A ONE-LIQUID PROPULSION METHOD AND ONE-LIQUID PROPULSION DEVICE 失效
公开(公告)号：JPH1122555A
公开(公告)日：1999-01-26
申请号：JP17465397
申请日：1997-06-30
申请人： HOSOYA FIREWORKS , NISSAN MOTOR
发明人： TAKIZUKA MICHINORI , HATANO HIDEO , ONDA TOSHIO , KUWABARA TAKUO , NAKAGAWA ICHIROU
IPC分类号： F02K9/50 , F02K9/60
摘要： PROBLEM TO BE SOLVED: To provide a one-liquid propulsion device having the toxicity lower than that of conventional hydrazine and capable of obtaining the specific impulse not inferior to that of the conventional hydrazine. SOLUTION: This one-liquid propulsion device 1 is provided with a propellant storage section 5 storing a one-liquid propellant 5P made of a mixed liquid containing at least hydroxylammonium nitrate and fuel, a catalyst layer 7C decomposing a partial mixed liquid flowing in a catalyst layer side branch pipe 8C of the mixed liquid to generate high-temperature gas, an injector 7J injecting the remaining mixed liquid flowing in an injector side branch pipe 8J of the mixed liquid, and a combustion space 7B igniting and burning the injected mixed liquid with the high-temperature gas to obtain thrust via a nozzle section 7N.

22. 发明专利

JPH03244906A COAXIAL INJECTOR FOR BURNER 失效
公开(公告)号：JPH03244906A
公开(公告)日：1991-10-31
申请号：JP3823490
申请日：1990-02-21
申请人： HITACHI LTD , NISSAN MOTOR
发明人： YOKOYAMA TOSHIAKI , HASHIMOTO TAKASHI , TAKAKUSAKI TSUNEHIKO , YOSHIDA MASAHIRO , ISHIGAMORI ISAO , NINOMIYA KAZUYOSHI , KUWABARA TAKUO , KONO MINORU
IPC分类号： F23D14/22 , F23D11/24 , F23L1/00
摘要： PURPOSE:To enable an accurate setting of a combustion gas temperature to be attained by a method wherein a flow rate of fuel is set by an orifice arranged on an external injector device constituting a coaxial injector device. CONSTITUTION:Fuel is supplied from a passage 5 and injected into a combustion chamber 9 through an orifice 4 arranged on an injector device 2. Ignition is carried out with an igniter 8, oxidization agent is supplied through a passage 6, injected into a combustion chamber 9 through an injector device 3 and then a hit combustion gas can be attained. The fuel is metered by an orifice which is machined under a high precision manner and of which hole area and shape are well controlled and so an accuracy of flow rare is high. Accordingly, an accuracy of combustion gas temperature is high. A flow rate of the gas can be varied by varying an area of on orifice hole, and a temperature of the combustion gas can also be varied. Arranging a hole at a forget position on the orifice 4 cause the fuel to be uniformly injected.

23. 发明专利

JPS6115264B2 JPS6115264B2 - 失效
公开(公告)号：JPS6115264B2
公开(公告)日：1986-04-23
申请号：JP3849480
申请日：1980-03-25
申请人： Nissan Motor
发明人： KUWABARA TAKUO , NOTAKE SHINJI , KOSAKA KATSUAKI
IPC分类号： F02K7/18

24. 发明专利

JPH1149514A PRODUCTION OF CRYSTALLINE HYDROXYLAMMONIUM NITRATE 失效
公开(公告)号：JPH1149514A
公开(公告)日：1999-02-23
申请号：JP20800697
申请日：1997-08-01
申请人： HOSOYA FIREWORKS , NISSAN MOTOR
发明人： HATANO HIDEO , ONDA TOSHIO , KUWABARA TAKUO
IPC分类号： C01C1/18 , C06B31/28
摘要： PROBLEM TO BE SOLVED: To efficiently produce crystalline hydroxylammonium nitrate. SOLUTION: The aq. soln. of hydroxylammonium nitrate is concd. to >=80 wt.% concn. The non-dissolving liq. that does not dissolve the hydroxylammonium nitrate is added to the concd. aq. soln., the liq. compatible with water and the non-dissolving liq. is further added and they are cooled optionally under vigorous stirring, or the solvent acting as a bad solvent to the hydroxylammonium nitrate and compatible with water is added to the concd. aq. soln. and they are cooled optionally under vigorous stirring. The hydroxylammonium nitrate is separated by cooling and the objective crystalline hydroxylammonium nitrate is obtd.

25. 发明专利

JPH111386A SOLID PROPELLANT 失效
公开(公告)号：JPH111386A
公开(公告)日：1999-01-06
申请号：JP15549997
申请日：1997-06-12
申请人： HOSOYA FIREWORKS , NISSAN MOTOR
发明人： TAKIZUKA MICHINORI , HATANO HIDEO , ONDA TOSHIO , KUWABARA TAKUO
IPC分类号： F02K9/08 , C06D5/00
摘要： PROBLEM TO BE SOLVED: To obtain a solid propellant for generating the same degree of impelling force as that using ammonium perchlorate, not containing a component like ammonium perchlorate to cause pollution such as acidic rain, by mixing hydroxylammonium nitrate as an oxidizing agent component with a binder as a fuel component to constitute the propellant. SOLUTION: This propellant is constituted by mixing preferably 70-90 pts.wt. of hydroxylammonium with preferably 10-30 pts.wt. of a binder. Various kinds of hydrocarbon-based polymers or rubber-like materials can be used as the binder. For example, a polysulfide, a PVC, a polyurethane, a polyester, a terminal carboxyl group-containing polybutadiene, a glycidylazidated polymer may be cited as the binder. The propellant is further mixed with a metal such as Al. Mg, Be, B, Zr, etc. as a fuel component.

26. 发明专利

JPH084588A PROPULSION DEVICE 失效
公开(公告)号：JPH084588A
公开(公告)日：1996-01-09
申请号：JP13912494
申请日：1994-06-21
申请人： NISSAN MOTOR
发明人： MATSUO SHINJI , KUWABARA TAKUO , KONO MINORU
IPC分类号： F02K7/14 , F02K9/62
摘要： PURPOSE:To improve combustion efficiency and to simplify structure, in a propulsion device operated in a supersonic area. CONSTITUTION:In a propulsion device 1 operated in a supersonic area, solid fuel 3 is arranged along the inner surface of the interior of a burner 2 opened to the head part side and the tail part side and an injector 6 for fuel component surplus gas is arranged at the inner central part of the head part of the burner 2.

27. 发明专利

JPH03244905A COAXIAL INJECTOR FOR BURNER 失效
公开(公告)号：JPH03244905A
公开(公告)日：1991-10-31
申请号：JP3823390
申请日：1990-02-21
申请人： HITACHI LTD , NISSAN MOTOR
发明人： YOKOYAMA TOSHIAKI , HASHIMOTO TAKASHI , TAKAKUSAKI TSUNEHIKO , YOSHIDA MASAHIRO , ISHIGAMORI ISAO , NINOMIYA KAZUYOSHI , KUWABARA TAKUO , KONO MINORU
IPC分类号： F23D14/22 , F23D11/24 , F23L1/00
摘要： PURPOSE:To prevent adhering of a flame and to enable a burn loss of a burner to be prevented by a method wherein an outlet end of an inner injector device is projected out of an outlet end of an outer injector device. CONSTITUTION:Fuel is supplied from a passage 5 and injected into a combustion chamber 9 through an orifice 4 arranged on an injector 2. Ignition is carried out by an ignition device, oxidization agent is supplied from a passage 6, injected into the combustion chamber 9 through an injector 3 and then a hot combustion gas can be attained. Accordingly to the preferred embodiment, fuel injected from the injector device 2 is mixed with oxidization agent injected from the injector device 3, the outlet end 3a of the injector device is projected out of the outlet end 2a of the injector device, resulting in that a flame is hardly adhered to the outlet end and thus it has an effect that a burn loss can be prevented.

28. 发明专利

JPS5990747A BURNING TEST DEVICE OF ROCKET MOTOR 失效
公开(公告)号：JPS5990747A
公开(公告)日：1984-05-25
申请号：JP19968682
申请日：1982-11-16
申请人： NISSAN MOTOR
发明人： AOKI ICHIROU , KUWABARA TAKUO
IPC分类号： F02K9/96
摘要： PURPOSE:To obtain more accurate measured data in the burning characteristic test of a propellant by a structure wherein the outer periphery of a motor case is covered with heat insulating material and at the same time a means for holding a rocket motor at a predetermined temperture by cooling and heating is arranged onto said periphery. CONSTITUTION:A heating pipe 9 and a cooling pipe 10 are spirally wound around the outer peripheral part of a motor case 1. An outer peripheral cover 11 is positioned by fitting a shell part 11c to both of a front and a rear side plates 11a and 11b through brackets 12a and 12b between said side plates 11a and 11b. Furthermore, the heating pipe 9 and the cooling pipe 10 are connected to a boiler 9a, a control valve 9b and a cooler 10a and a control valve 10b, all of which are a part of a temperature control device. In addition, heat insulating material 13 is packed within the outer peripheral cover 11. Due to the structure as mentioned above, the temperature of the motor case 1 is held at a set state for performing a burning test of a propellant 14. Accordingly, more accurate data on the propellant 14 can be measured.

29. 发明专利

JPS56138449A RAMROCKET 失效
公开(公告)号：JPS56138449A
公开(公告)日：1981-10-29
申请号：JP4243080
申请日：1980-03-31
申请人： NISSAN MOTOR
发明人： KUWABARA TAKUO , KOSAKA KATSUAKI , NOTAKE SHINJI
IPC分类号： F02K7/18 , B64D27/16
摘要： PURPOSE:To prevent the blow-out by arranging an overexpansion nozzle axially at the position where the primary and secondary combustion chambers of a ram rocket will conduct thereby separating the combustion gas in the nozzle and forming the flame retaining region. CONSTITUTION:A primary combustion chamber 4 is formed at the rear of a fuel 8 while a secondary combustion chamber 5 is formed through an overexpansion nozzle 30 at the rear of said chamber 4. The nozzle 30 is formed such that an enlarging nozzle skirt 32 is provided in axial line from the nozzle skirt 23a of a barrier wall 23 while a flame retaining mesh 35 is arranged at the end of the exit. The combustion gas flow F is formed at the central portion of the nozzle 30 while it is separated at the outer-circumferential portion to form a flame retaining region H. The seed fire is formed by said region H and the member 35.

30. 发明专利

JPS56135735A RAM ROCKET 失效
公开(公告)号：JPS56135735A
公开(公告)日：1981-10-23
申请号：JP3849480
申请日：1980-03-25
申请人： NISSAN MOTOR
发明人： KUWABARA TAKUO , NOTAKE SHINJI , KOSAKA KATSUAKI
IPC分类号： F02K7/18
摘要： PURPOSE:To enhance the corrosion-resisting property of an injector and to stabilize the quantity of production of combustible gas and the properties of the gas by a method wherein a nozzle throat to which ceramic coating is applied is projected out in the injector provided between the primary and secondary combustion chambers of the ram rocket. CONSTITUTION:Inside the front part of the ram rocket 11 a solid propellant 18 is filled up and in the rear thereof the primary combustion chamber having an igniter 10 is formed. In the further rear thereof, the secondary combustion chamber 15 is formed through the intermediary of the injector 23 and the air for combustion is introduced by a diffuser 9. The injector 23 has a number of nozzle holes 22, 23 in the front and rear surfaces thereof and the nozzle throat 16 on the surface of which ceramic coating is applied from the direction of the outer periphery thereof is arranged in projection therein.

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