专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20180112628A1 Rocket Engine Ignition System 审中-公开
公开(公告)号：US20180112628A1
公开(公告)日：2018-04-26
申请号：US15572440
申请日：2016-05-09
申请人： ECAPS Aktiebolag
发明人： Kjell Anflo
IPC分类号： F02K9/95
CPC分类号： F02K9/95 , F02K9/52 , F02K9/68 , F05D2260/99
摘要： The present invention relates to an ignition system for a liquid propellant chemical rocket engine, which comprises a thermal-catalytic element (20) for initiating decomposition of the liquid propellant, and an electrical heater (30) for electrically preheating the thermal-catalytic element, wherein the thermal-catalytic element is thermally connected to the electrical heater, both of which are located in a flow path of the propellant, a rocket engine, and a preburner, respectively, comprising the ignition system, as well as a method of preheating a liquid propellant rocket engine using the system, and a spacecraft comprising such engine.

2. 发明申请

US20180298846A1 Liquid Propellant Chemical Rocket Engine Reactor Thermal Management System 审中-公开
公开(公告)号：US20180298846A1
公开(公告)日：2018-10-18
申请号：US15566362
申请日：2016-04-14
申请人： ECAPS Aktiebolag
发明人： Kjell Anflo , Benjamin Crow
IPC分类号： F02K9/68 , F02K9/42 , F02K9/52 , B64G1/40 , F02K9/58
摘要： The present invention relates to a liquid propellant chemical rocket engine reactor Thermal Management System (TMS), which system comprises a reactor comprising a thermally conductive reactor housing, a heat bed, and a catalyst bed, which system further comprises an injector configured to spray the propellant in the form of a cone towards a portion of the circumference of the inner surface of the reactor housing, and an electrical heater located on the outside or inside of the reactor housing for heating said portion of the inner surface of the reactor housing. The invention also relates to a rocket engine comprising the reactor Thermal Management System, a spacecraft comprising the engine, as well as to a method of decomposing a liquid propellant, which can be carried out using the inventive reactor Thermal Management System, wherein vaporization of the propellant is accomplished by bringing the propellant into close proximity to, or to imping on, a portion of the circumference of said inner reactor surface adjacent to the injector.

3. 发明专利

AT375960T 未知
公开(公告)号：AT375960T
公开(公告)日：2007-11-15
申请号：AT02726542
申请日：2002-05-23
申请人： ECAPS AKTIEBOLAG
发明人： ANFLO KJELL , AGRELL JOHAN , ERSSON ANDERS , JAERAS SVEN , BOUTONNET MAGALI , BRANDT JESPER , LYCKFELDT OLA
IPC分类号： C01F7/16 , B01J2/06 , B01J21/04 , B01J23/02 , B01J23/10 , B01J23/34 , B01J23/46 , B01J35/00 , B01J35/02 , B01J35/08 , B01J35/10 , B01J37/00 , B01J37/03 , C01F17/00 , C04B35/634 , C06D5/08

4. 发明申请

WO2016182496A1 ROCKET ENGINE IGNITION SYSTEM 审中-公开
标题翻译： ROCKET发动机点火系统
公开(公告)号：WO2016182496A1
公开(公告)日：2016-11-17
申请号：PCT/SE2016/050415
申请日：2016-05-09
申请人： ECAPS AKTIEBOLAG
发明人： ANFLO, Kjell
IPC分类号： F02K9/52 , F02K9/68
CPC分类号： F02K9/95 , F02K9/52 , F02K9/68 , F05D2260/99
摘要： The present invention relates to an ignition system for a liquid propellant chemical rocket engine, which comprises a thermal-catalytic element (20) for initiating decomposition of the liquid propellant, and an electrical heater (30) for electrically preheating the thermal-catalytic element, wherein the thermal-catalytic element is thermally connected to the electrical heater, both of which are located in a flow path of the propellant, a rocket engine, and a preburner, respectively, comprising the ignition system, as well as a method of preheating a liquid propellant rocket engine using the system, and a spacecraft comprising such engine.
摘要翻译：本发明涉及一种用于液体推进剂化学火箭发动机的点火系统，其包括用于引发液体推进剂分解的热催化元件（20）和用于电热预热热催化元件的电加热器（30）其中所述热催化元件热连接到所述电加热器，它们都分别位于包括所述点火系统的所述推进剂，火箭发动机和预燃机的流动路径中，以及预热方法使用该系统的液体推进剂火箭发动机，以及包括这种发动机的航天器。

5. 发明申请

WO2016186566A1 ROCKET ENGINE HEATER ASSEMBLY 审中-公开
标题翻译： ROCKET发动机加热器总成
公开(公告)号：WO2016186566A1
公开(公告)日：2016-11-24
申请号：PCT/SE2016/050467
申请日：2016-05-20
申请人： ECAPS AKTIEBOLAG
发明人： ANFLO, Kjell
IPC分类号： F02K9/42 , F02K9/68 , B23K1/00
CPC分类号： F02K9/42 , B23K1/0018 , B23K1/19 , B23K2201/001 , B23K2203/08 , B23K2203/26 , F02K9/68 , F05D2230/237
摘要： The present invention relates to an electrical heater assembly (1) for liquid propellant chemical rocket engines, and more particularly to such heater assembly comprising a heating cable (30) and a heater support (10), wherein the heater support exhibits a groove (17) in which the cable is accommodated, and wherein the heating cable is attached to the support by means of brazing (40) and/or by means of an enclosing member, as well as a liquid propellant chemical rocket engine provided with the heater assembly.
摘要翻译：本发明涉及一种用于液体推进剂化学火箭发动机的电加热器组件（1），更具体地涉及包括加热电缆（30）和加热器支架（10）的加热器组件，其中加热器支架呈现出一个凹槽（17 ），其中所述电缆被容纳在其中，并且其中所述加热电缆通过钎焊（40）和/或借助于封闭构件以及设置有所述加热器组件的液体推进剂化学火箭发动机附接到所述支撑件。

6. 发明申请

WO2016167700A1 LIQUID PROPELLANT CHEMICAL ROCKET ENGINE REACTOR THERMAL MANAGEMENT SYSTEM 审中-公开
标题翻译：液体推进剂化学发动机发动机反应器热管理系统
公开(公告)号：WO2016167700A1
公开(公告)日：2016-10-20
申请号：PCT/SE2016/000017
申请日：2016-04-14
申请人： ECAPS Aktiebolag
发明人： ANFLO, Kjell , CROW, Benjamin
IPC分类号： F02K9/42 , F23R3/30 , F23R3/40 , F23R7/00 , F02K9/52 , F02K9/68
CPC分类号： F02K9/42 , F02K9/425 , F02K9/52 , F02K9/68 , F05D2260/20 , F23R3/30 , F23R3/40 , F23R7/00
摘要： The present invention relates to a liquid propellant chemical rocket engine reactor Thermal Management System (TMS), which system comprises a reactor comprising a thermally conductive reactor housing, a heat bed, and a catalyst bed, which system further comprises an injector configured to spray the propellant in the form of a cone towards a portion of the circumference of the inner surface of the reactor housing, and an electrical heater located on the outside or inside of the reactor housing for heating said portion of the inner surface of the reactor housing. The invention also relates to a rocket engine comprising the reactor Thermal Management System, a spacecraft comprising the engine, as well as to a method of decomposing a liquid propellant, which can be carried out using the inventive reactor Thermal Management System, wherein vaporization of the propellant is accomplished by bringing the propellant into close proximity to, or to imping on, a portion of the circumference of said inner reactor surface adjacent to the injector.
摘要翻译：本发明涉及一种液体推进剂化学火箭发动机反应堆热管理系统（TMS），该系统包括一个包括导热反应器壳体，加热床和催化剂床的反应器，该系统还包括喷射器，推进剂呈锥体形式，朝向反应器壳体内表面的一部分周边;以及电加热器，位于反应器壳体的外侧或内部，用于加热反应堆外壳内表面的所述部分。本发明还涉及包括反应堆热管理系统，包括发动机的航天器以及可以使用本发明的反应器热管理系统进行分解的液体推进剂的方法的火箭发动机，其中蒸发推进剂通过使推进剂与所述内反应器表面的与喷射器相邻的一部分周边紧密接触或撞击而实现。

7. 发明申请

WO2013048315A3 METHOD AND ARRANGEMENT FOR CONVERSION OF CHEMICAL ENERGY FROM AQUEOUS, LIQUID, ADN-BASED MONOPROPELLANTS INTO MECHANICAL ENERGY 审中-公开
标题翻译：从水性，液态，基于ADN的单极化合物转化为机械能的化学能量的方法和装置
公开(公告)号：WO2013048315A3
公开(公告)日：2013-07-04
申请号：PCT/SE2012051017
申请日：2012-09-26
申请人： ECAPS AKTIEBOLAG
发明人： ANFLO KJELL , THORMAEHLEN PETER
IPC分类号： F23L7/00 , F23R7/00
CPC分类号： F23R7/00 , F23L7/002 , F23L2900/07008
摘要： The present invention generally relates to a method of converting chemical energy from aqueous,liquid, ADN-based monopropellantsinto mechanical energy and a corresponding arrangement comprising a reactor for combustion of aqueous,liquid,ADN-based monopropellants and a mechanical-energy converting device, and to a vehicle, vessel, missile, secondary power plant, EPU, APU and the like comprising such arrangement.
摘要翻译：本发明一般涉及将化学能从水性，液态，基于ADN的单推进剂转化为机械能的方法，以及包括用于燃烧含水，液体，基于ADN的单推进剂和机械能转换装置的反应器的相应装置，以及包括这种布置的车辆，船只，导弹，二次发电厂，EPU，APU等。

8. 发明申请

WO2013048315A2 METHOD AND ARRANGEMENT FOR CONVERSION OF CHEMICAL ENERGY FROM AQUEOUS, LIQUID, ADN-BASED MONOPROPELLANTS INTO MECHANICAL ENERGY 审中-公开
标题翻译：将含水，液体，基于ADN的单体化学能转化为机械能的方法和装置
公开(公告)号：WO2013048315A2
公开(公告)日：2013-04-04
申请号：PCT/SE2012/051017
申请日：2012-09-26
申请人： ECAPS AKTIEBOLAG
发明人： ANFLO, Kjell , THORMÄHLEN, Peter
CPC分类号： F23R7/00 , F23L7/002 , F23L2900/07008
摘要： The present invention generally relates to a method of converting chemical energy from aqueous,liquid, ADN-based monopropellantsinto mechanical energy and a corresponding arrangement comprising a reactor for combustion of aqueous,liquid,ADN-based monopropellants and a mechanical-energy converting device, and to a vehicle, vessel, missile, secondary power plant, EPU, APU and the like comprising such arrangement.
摘要翻译：本发明总体上涉及一种将来自水性液体ADN基单组元推进剂的化学能转化为机械能的方法，以及包括用于燃烧水基ADN基单组分推进剂的反应器的相应装置和机械能转换装置，并且涉及包括这种布置的车辆，船舶，导弹，二次发电厂，EPU，APU等等。

9. 发明授权

EP3004031B1 DUAL MODE CHEMICAL ROCKET ENGINE, AND DUAL MODE PROPULSION SYSTEM COMPRISING THE ROCKET ENGINE 有权
公开(公告)号：EP3004031B1
公开(公告)日：2020-01-01
申请号：EP14734946.8
申请日：2014-05-28
申请人： ECAPS Aktiebolag
发明人： ANFLO, Kjell , BERGMAN, Göran
IPC分类号： C06B47/00 , C06B47/02 , C06D5/08 , F02K9/42

10. 发明授权

EP2847452B1 IMPROVED REACTOR FOR AMMONIUM DINITRAMIDE-BASED LIQUID MONO-PROPELLANTS, AND THRUSTER INCLUDING THE REACTOR 有权
标题翻译：改进的基于硝酸铵的液体单体推进剂的反应器和包括反应器的推进器
公开(公告)号：EP2847452B1
公开(公告)日：2016-11-30
申请号：EP13727664.8
申请日：2013-05-07
申请人： ECAPS Aktiebolag
发明人： ANFLO, Kjell , THORMÄHLEN, Peter
IPC分类号： F02K9/42
CPC分类号： F02K9/68 , B01J23/38 , B01J23/40 , B01J37/0221 , F02K9/42 , F02K9/425 , F02K9/52 , F23R3/30 , F23R3/40 , F23R7/00

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式