公开(公告)号：EP2157306B1

公开(公告)日：2018-07-18

申请号：EP09168405.0

申请日：2009-08-21

申请人： Lockheed Martin Corporation (Maryland Corp.)

发明人： Boespflug, Matthew Patrick ,  Steenburgh, Dennis ,  Saddoughi, Seyed Gholami ,  Bennett, Grover Andrew

IPC分类号： F02K7/02 ,  F02K1/00 ,  F02K1/28 ,  F02K7/075 ,  F02C5/02 ,  F23R7/00

CPC分类号： F02C5/02 ,  F02K1/002 ,  F02K1/28 ,  F02K7/075 ,  F05D2240/40 ,  F05D2250/311 ,  F05D2260/16 ,  F05D2270/18 ,  F23R7/00 ,  Y02T50/671

摘要： Pulse detonation/deflagration apparatus (30, 30') for providing enhanced pressure wave operating frequency and/or magnitude, and methods of increasing the frequency or the magnitude of deflagration to detonation waves (37), are provided. A pulse detonation/deflagration apparatus (30, 30') can include a main/outer pulse detonation/deflgration actuator/engine (31) with multiple smaller internal combustion chambers or tubes (33) positioned inside the cavity of the main/outer actuator/engine (31) with each performing the function of individual pulse detonation/deflagration actuator/engines (31), The output pressure waves (37) created by the internal combustion chambers or tubes (33) can be utilized for propulsion or for controlling large scale flows, where needed.

公开(公告)号：EP2157306A3

公开(公告)日：2017-01-18

申请号：EP09168405.0

申请日：2009-08-21

申请人： Lockheed Martin Corporation (Maryland Corp.)

发明人： Boespflug, Matthew Patrick ,  Steenburgh, Dennis ,  Saddoughi, Seyed Gholami ,  Bennett, Grover Andrew

IPC分类号： F02K7/02 ,  F02K1/00 ,  F02K1/28 ,  F02K7/075 ,  F02C5/02 ,  F23R7/00

CPC分类号： F02C5/02 ,  F02K1/002 ,  F02K1/28 ,  F02K7/075 ,  F05D2240/40 ,  F05D2250/311 ,  F05D2260/16 ,  F05D2270/18 ,  F23R7/00 ,  Y02T50/671

摘要： Pulse detonation/deflagration apparatus (30, 30') for providing enhanced pressure wave operating frequency and/or magnitude, and methods of increasing the frequency or the magnitude of deflagration to detonation waves (37), are provided. A pulse detonation/deflagration apparatus (30, 30') can include a main/outer pulse detonation/deflgration actuator/engine (31) with multiple smaller internal combustion chambers or tubes (33) positioned inside the cavity of the main/outer actuator/engine (31) with each performing the function of individual pulse detonation/deflagration actuator/engines (31), The output pressure waves (37) created by the internal combustion chambers or tubes (33) can be utilized for propulsion or for controlling large scale flows, where needed.

摘要翻译： 提供脉冲爆震/用于提供增强的压力波的工作频率和/或幅度爆燃装置（30，30“），和增加的频率或爆燃到爆轰波（37）的大小的方法。 脉冲爆震/爆燃装置（30，30“）可包括主/外脉冲爆震/ deflgration致动器/主/外致动器的腔体内部定位的多个较小内部燃烧腔或燃烧管（33）的发动机（31）/ 发动机（31）与每个执行个别脉冲爆震/爆燃致动器/发动机（31）（37）由内部燃烧腔或燃烧管（33）创建的函数的输出压力波可以用于推进或用于控制大规模 流动时，在需要的地方。

公开(公告)号：EP2157306A2

公开(公告)日：2010-02-24

申请号：EP09168405.0

申请日：2009-08-21

申请人： Lockheed Martin Corporation (Maryland Corp.)

发明人： Boespflug, Matthew Patrick ,  Steenburgh, Dennis ,  Saddoughi, Seyed Gholami ,  Bennett, Grover Andrew

IPC分类号： F02K7/02

CPC分类号： F02C5/02 ,  F02K1/002 ,  F02K1/28 ,  F02K7/075 ,  F05D2240/40 ,  F05D2250/311 ,  F05D2260/16 ,  F05D2270/18 ,  F23R7/00 ,  Y02T50/671

摘要： Pulse detonation/deflagration apparatus (30, 30') for providing enhanced pressure wave operating frequency and/or magnitude, and methods of increasing the frequency or the magnitude of deflagration to detonation waves (37), are provided. A pulse detonation/deflagration apparatus (30, 30') can include a main/outer pulse detonation/deflgration actuator/engine (31) with multiple smaller internal combustion chambers or tubes (33) positioned inside the cavity of the main/outer actuator/engine (31) with each performing the function of individual pulse detonation/deflagration actuator/engines (31), The output pressure waves (37) created by the internal combustion chambers or tubes (33) can be utilized for propulsion or for controlling large scale flows, where needed.