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1. 发明授权

US5678857A Assembly and method for the moderation of inflator output 失效
标题翻译：充气机输出的装配和方法
公开(公告)号：US5678857A
公开(公告)日：1997-10-21
申请号：US606261
申请日：1996-02-23
申请人： Darrin L. Johnson , Linda M. Rink
发明人： Darrin L. Johnson , Linda M. Rink
IPC分类号： B60R21/201 , B60R21/217 , B60R21/26 , B60R21/261
CPC分类号： B60R21/2171 , B60R21/201 , B60R21/26 , B60R21/261
摘要： An inflatable restraint system assembly and method of operation are provided wherein a compliance chamber pressure vessel formed about the gas exit area of an inflator appropriately and desirably moderates the inflation gas output from the inflator into an associated inflatable device such as inflatable vehicle occupant restraint. The invention has particular utility for use in conjunction with high mass flow rate inflators.
摘要翻译：提供了一种充气式约束系统组件和操作方法，其中围绕充气机的气体出口区域形成的顺应性室压力容器适当地和适当地调节从充气机输出的膨胀气体到相关联的充气装置，例如充气车辆乘员约束。本发明特别适用于与高质量流量充气机结合使用。

2. 发明授权

US07703395B2 Inflator having an ignition nozzle 有权
标题翻译：具有点火嘴的充气器
公开(公告)号：US07703395B2
公开(公告)日：2010-04-27
申请号：US11055360
申请日：2005-02-10
申请人： Fred J. Cook , Halley O. Stevens , Darrin L. Johnson
发明人： Fred J. Cook , Halley O. Stevens , Darrin L. Johnson
IPC分类号： C06D5/00
CPC分类号： B60R21/2644 , B60R21/264
摘要： An inflator (10) includes a container (12) having a chamber (120). An exit opening (48) is provided in the container (12) and is connected to the chamber (120). A substance (122, 180) is stored in the chamber (120) and is responsive to heat for providing inflation fluid. An igniter (130) is associated with the container (12) and is actuatable to provide combustion products for heating the substance (122, 180). A nozzle (80) is interposed between the igniter (130) and the chamber (120). A passage (90) extends from the igniter (130) and through the nozzle (80). The passage (90) includes a divergent portion (110) for focusing a flow of combustion products from the igniter (130) into the chamber (120).
摘要翻译：充气机（10）包括具有室（120）的容器（12）。出口开口（48）设置在容器（12）中并连接到腔室（120）。物质（122,180）存储在腔室（120）中并且响应于热量以提供充气流体。点火器（130）与容器（12）相关联并且可致动以提供用于加热物质（122,180）的燃烧产物。喷嘴（80）介于点火器（130）和腔室（120）之间。通道（90）从点火器（130）延伸并且通过喷嘴（80）延伸。通道（90）包括用于将来自点火器（130）的燃烧产物流聚焦到腔室（120）中的发散部分（110）。

3. 发明授权

US5918901A Airbag module with pressure relief adaptive performance 失效
标题翻译：安全气囊模块具有减压自适应性能
公开(公告)号：US5918901A
公开(公告)日：1999-07-06
申请号：US802803
申请日：1997-02-18
申请人： Darrin L. Johnson , Bradley D. Harris , Donald R. Lauritzen
发明人： Darrin L. Johnson , Bradley D. Harris , Donald R. Lauritzen
IPC分类号： B60R21/20 , B60R21/217 , B60R21/276 , B60R21/30
CPC分类号： B60R21/276 , B60R2021/2177 , B60R2021/2765 , B60R21/2171
摘要： An airbag module providing adaptive performance. The module includes a housing defining an interior. At least an inflator is received within the housing, and preferably the folded, uninflated cushion, also. Various arrangements are provided to selectively block, or create, a vent extending through the housing. This vent, when open, permits the inflation gas provided by the inflator to exit the housing without entering the cushion. The vent may be initially open, and blocked by a sliding cover block, may be initially closed and opened by movement of a slide plug, or may be initially closed and opened by deformation of a portion of the housing. The venting of the inflation gas will at least slow the rate of inflation of the cushion, and may reduce the final pressure within the cushion. As such, the housing will be vented for less severe collisions, and will not be vented for more severe collisions.
摘要翻译：提供适应性能的安全气囊模块。模块包括限定内部的壳体。至少一个充气机被容纳在壳体内，并且优选地被收纳在折叠的未充气的垫子中。提供了各种布置以选择性地阻挡或产生延伸穿过壳体的通风口。该通气口在打开时允许由充气机提供的充气气体离开壳体而不进入垫子。通风口可以最初打开并被滑动盖块封闭，可以通过滑动塞的移动而被初始地关闭和打开，或者可以通过壳体的一部分的变形而被初始地关闭和打开。膨胀气体的排放将至少减缓衬垫的膨胀速率，并且可以减小衬垫内的最终压力。因此，房屋将被排放较少的严重碰撞，不会泄漏更严重的碰撞。

4. 发明授权

US5820160A Airbag inflator with venturi effect cooling and gas supplement 失效
标题翻译：气囊充气机，文丘里效应冷却和气体补充
公开(公告)号：US5820160A
公开(公告)日：1998-10-13
申请号：US609665
申请日：1996-03-01
申请人： Darrin L. Johnson , Brett Hussey , Linda M. Rink
发明人： Darrin L. Johnson , Brett Hussey , Linda M. Rink
IPC分类号： B60R21/30 , B60R21/32
CPC分类号： B60R21/30 , Y10T137/1647 , Y10T137/87587
摘要： An airbag inflator with venturi effect cooling and gas supplement. The inflator includes a housing having a quantity of gas-producing fuel therein, and possibly a stored gas also, along with appropriate igniters. These materials are stored within a gas production chamber of the housing. The gas leaving this chamber travels through the housing to an exit port on the housing. Intermediate the gas production chamber and the housing exit port is a venturi section of the housing. This section reduces the pressure of the gas, and thus the pressure at the interior end of draw vents opening onto the venturi section. The vents therefore draw outside air into the housing to mix with the gas. This cools the gas to the desired temperature, and also supplements the gas exiting the housing. As such, the need for a heat sink to cool the gas is reduced or eliminated. Furthermore, since the cushion is inflated with a mixture of gas and air, the amount of gas typically needed is reduced by the amount of added air. This permits the amount of fuel to be reduced, thus reducing cost and weight.
摘要翻译：安全气囊充气机，文丘里效应冷却和气体补充。充气机包括其中具有一定量的产生气体的壳体，以及可能的储存气体以及合适的点火器。这些材料储存在壳体的气体生产室内。离开该室的气体通过壳体行进到壳体上的出口。气体生成室和外壳出口的中间是壳体的文氏管部分。该部分减小了气体的压力，因此在通向文丘里管部分的通气孔内端的压力。因此，通风口将外部空气吸入外壳以与气体混合。这将气体冷却至所需温度，并补充离开外壳的气体。因此，降低或消除了需要散热器来冷却气体。此外，由于气垫和气体的混合使气垫膨胀，所以通常需要的气体量减少了空气量。这允许减少燃料量，从而降低成本和重量。

5. 发明授权

US5719351A Anti-rupture method for liquid propellant gas inflator 失效
标题翻译：液体推进剂气体充气机的抗破裂方法
公开(公告)号：US5719351A
公开(公告)日：1998-02-17
申请号：US770382
申请日：1996-12-03
申请人： Darrin L. Johnson , Bradley D. Harris
发明人： Darrin L. Johnson , Bradley D. Harris
IPC分类号： B60R21/26 , B60R21/264 , B60R21/268 , B60R21/272 , B60R21/276
CPC分类号： B60R21/264 , B60R21/276
摘要： An inflator of a vehicle safety restraint system includes a housing having a reservoir of liquid propellant. A combustion chamber is disposed in the housing in communication with the liquid propellant reservoir. A regenerative piston is movably disposed within the housing for separating the liquid propellant reservoir and the combustion chamber. The piston head includes a plurality of injection ports for delivering the liquid propellant to the combustion chamber in a controlled manner. A pressure relieving bore, normally sealed by the piston stem, is disposed in the housing for relieving pressure in the liquid propellant reservoir. Decomposition or combustion within the propellant storage reservoir will move the piston to open the pressure relief bore which depressurizes the liquid propellant and prevents rupture and fragmentation of the inflator.
摘要翻译：车辆安全限制系统的充气机包括具有液体推进剂储存器的壳体。燃烧室设置在与液体推进剂储存器连通的壳体中。再生活塞可移动地设置在壳体内，用于分离液体推进剂储存器和燃烧室。活塞头包括多个注射口，用于以受控的方式将液体推进剂输送到燃烧室。通常由活塞杆密封的减压孔设置在壳体中以减轻液体推进剂储存器中的压力。推进剂储存容器内的分解或燃烧将使活塞移动以打开压力释放孔，该压力释放孔减压液体推进剂并防止充气机的破裂和碎裂。

6. 发明授权

US5564738A Overflow channeling reaction canister assembly 失效
标题翻译：溢流引导反应罐组件
公开(公告)号：US5564738A
公开(公告)日：1996-10-15
申请号：US512591
申请日：1995-08-10
申请人： Darrin L. Johnson
发明人： Darrin L. Johnson
IPC分类号： B60R21/20 , B60R21/217 , B60R21/26 , B60R21/276
CPC分类号： B60R21/2171 , B60R21/276
摘要： A reaction canister assembly for use in an inflatable airbag module system comprises a reaction canister housing having at least one open side and an inflator chamber. An inflator is disposed in the inflator chamber and includes a plurality of perforations or ports for passing excess gas generated within the inflator into the canister housing. At least one endplate partially closes the open side of the canister to leave an excess gas outlet passage at the open side of the housing. At least one overflow channel extends along a length of the housing for filtering and cooling the excess gas generated by the inflator. The excess gas passes through the ports of the inflator into the overflow channels and is discharged through the excess gas outlet passage at the open side of the housing.
摘要翻译：用于可充气安全气囊模块系统的反应罐组件包括具有至少一个开口侧和充气器室的反应罐壳体。充气机设置在充气机室中，并且包括多个穿孔或端口，用于将在充气机内产生的多余的气体传送到罐壳体中。至少一个端板部分地封闭罐的开口侧，以在壳体的开放侧留下多余的气体出口通道。至少一个溢流通道沿壳体的长度延伸，用于过滤和冷却由充气机产生的过量气体。过量气体通过充气机的端口进入溢流通道，并通过外壳开口侧的多余气体出口通道排出。

7. 发明授权

US06237950B1 Staged air bag inflator 失效
标题翻译：分级气囊充气机
公开(公告)号：US06237950B1
公开(公告)日：2001-05-29
申请号：US09360920
申请日：1999-07-26
申请人： Fred J. Cook , Barry F. Shaffer , Darrin L. Johnson , Edward F. Randell
发明人： Fred J. Cook , Barry F. Shaffer , Darrin L. Johnson , Edward F. Randell
IPC分类号： B60R2126
CPC分类号： B60R21/272 , B60R21/264 , B60R2021/26094
摘要： An apparatus (10) for inflating an inflatable vehicle occupant protection device (32) comprises a container (20) defining a gas storage chamber (14), and inflation fluid (66) under pressure in the gas storage chamber. An opening (40, 42) in the container (20) enables fluid flow from the gas storage chamber (14) to the inflatable device (32). A rupturable burst disk (60, 62) extends across the opening (40, 42). An assembly (80) in the gas storage chamber (14) is provided for producing combustion products for heating and pressurizing the inflation fluid (66). The assembly (80) includes a housing (82) and a separator (100) in the housing defining first and second chambers (112, 114). A first pyrotechnic charge (122) in the first chamber (112) has a first burn rate. The housing (82) has first fluid outlets (96) for enabling flow of combustion products from the first chamber (112) to the gas storage chamber (14). A second pyrotechnic charge (124) in the second chamber (114) has a second burn rate less than the first burn rate. The housing (82) has second fluid outlets (98) for enabling flow of combustion products from the second chamber (114) to the gas storage chamber (14).
摘要翻译：一种用于对充气车辆乘员保护装置（32）进行充气的装置（10）包括限定气体储存室（14）的容器（20）和在气体储存室内的压力下的充气流体（66）。容器（20）中的开口（40,42）使流体能够从气体储存室（14）流向充气装置（32）。可破裂的突发盘（60,62）跨越开口（40,42）延伸。设置在气体储存室（14）中的组件（80），用于产生用于加热和加压充气流体（66）的燃烧产物。组件（80）包括壳体（82）和壳体中的分隔件（100），其限定第一和第二腔室（112,114）。第一室（112）中的第一烟火装置（122）具有第一燃烧速率。壳体（82）具有用于使燃烧产物从第一室（112）流到气体储存室（14）的第一流体出口（96）。在第二室（114）中的第二烟火装置（124）具有小于第一燃烧速率的第二燃烧率。壳体（82）具有第二流体出口（98），用于使燃烧产物从第二室（114）流到气体储存室（14）。

8. 发明授权

US06176249B1 Inflator 有权
标题翻译：气筒
公开(公告)号：US06176249B1
公开(公告)日：2001-01-23
申请号：US09371777
申请日：1999-08-10
申请人： Ahmad K. Al-Amin , Jerome W. Emery , Guy M. Jackman , Darrin L. Johnson , Scott R. Peavy , Barry F. Shaffer
发明人： Ahmad K. Al-Amin , Jerome W. Emery , Guy M. Jackman , Darrin L. Johnson , Scott R. Peavy , Barry F. Shaffer
IPC分类号： F16K1740
CPC分类号： B60R21/268 , F16K13/06 , Y10T137/1647 , Y10T137/1692 , Y10T137/1774
摘要： An inflator (10) for providing inflation fluid to inflate an inflatable vehicle occupant protection device includes a pressure vessel (12) defining a chamber (30) for inflation fluid. The pressure vessel (12) has a passage (40) through which inflation fluid flows from the chamber (30). A burst disk (52) blocks fluid flow through the passage (40). A member (80) is disposed adjacent to and on one side of the burst disk (52) prior to the inflation fluid entering the pressure vessel (12). The burst disk (52) deforms toward the one side due to the pressure of the inflation fluid when the inflation fluid is disposed in the chamber (30). The member (80) limits deformation of the burst disk (52) by contacting the burst disk. An actuatable igniter assembly (66), when actuated, moves the member toward the burst disk (52) to rupture the burst disk and enable the inflation fluid to flow from the chamber (30) through the passage (40).
摘要翻译：用于提供充气流体以使充气车辆乘员保护装置充气的充气器（10）包括限定用于充气流体的腔室（30）的压力容器（12）。压力容器（12）具有通道（40），充气流体通过该通道从腔室（30）流出。爆破盘（52）阻挡通过通道（40）的流体流。在膨胀流体进入压力容器（12）之前，构件（80）设置在爆破盘（52）的邻近并在其一侧。当膨胀流体设置在室（30）中时，由于膨胀流体的压力，爆破盘（52）向一侧变形。构件（80）通过接触突发盘来限制突发盘（52）的变形。可致动点火器组件（66）在被致动时将构件移向爆破盘（52）以使破裂盘破裂并使膨胀流体能够从腔室（30）流过通道（40）。

9. 发明授权

US5851030A Regenerative monopropellant airbag inflator 失效
标题翻译：再生式单组分推进气囊充气机
公开(公告)号：US5851030A
公开(公告)日：1998-12-22
申请号：US759995
申请日：1996-12-03
申请人： Darrin L. Johnson , Bradley D. Harris , Donald R. Lauritzen
发明人： Darrin L. Johnson , Bradley D. Harris , Donald R. Lauritzen
IPC分类号： B60R21/26 , B60R21/264 , C06D5/00 , B60R21/28
CPC分类号： B60R21/264 , C06D5/00
摘要： A regenerative monopropellant inflator having improved initiation of the regenerative cycle and improve operating efficiency. The inflator may direct the flow of the monopropellant into a localized volume to create a "hot spot" to increase combustion. This serves to ensure that the regenerative cycle is initiated. Various arrangements are provided to increase the residence time of the combusting monopropellant within the inflator, to ensure complete combustion of the monopropellant, and thus increased efficiency. These arrangements include inducing a helical gas flow to increase the length of the path traveled by the gas. Various barriers may also be placed within the gas flow to force direction changes, which reduce the velocity of the gas.
摘要翻译：一种再生式单组元推进式充气机，其具有改善的再生循环的启动并提高运行效率。充气机可以将单组元推进剂的流动引导到局部容积以产生“热点”以增加燃烧。这用于确保再生循环启动。提供了各种布置以增加燃烧单组分推进剂在充气机内的停留时间，以确保单组分推进剂的完全燃烧，从而提高效率。这些布置包括引起螺旋形气流以增加由气体行进的路径的长度。气体流中也可以设置各种障碍物，以迫使方向改变，从而降低气体的速度。

10. 发明授权

US5768885A Regenerative piston liquid propellant rocket motor 失效
标题翻译：再生活塞液体推进剂火箭发动机
公开(公告)号：US5768885A
公开(公告)日：1998-06-23
申请号：US760011
申请日：1996-12-03
申请人： Darrin L. Johnson , Donald R. Lauritzen
发明人： Darrin L. Johnson , Donald R. Lauritzen
IPC分类号： F02K9/50 , F02K9/44
CPC分类号： F02K9/50
摘要： A regenerative liquid propellant rocket motor including a body having an integrally formed central tube. A primary combustion chamber is disposed in the body. A secondary combustion chamber is formed by the central tube of the body. A reservoir of liquid propellant is disposed in the body. A regenerative piston is slidably disposed in the body for delivering the liquid propellant to the primary and secondary combustion chambers. The piston includes a plurality of injection ports for injecting the liquid propellant. An ignitor is disposed in the body for initiating combustion of the liquid propellant. A nozzle is formed at a free end of the central tube for producing thrust, wherein upon ignition of the ignitor combustion occurs in the primary combustion chamber driving the piston into the liquid propellant reservoir and the liquid propellant is injected into the primary combustion chamber to produce combustion products which are channeled into the secondary combustion chamber and expanded through the nozzle.
摘要翻译：一种再生液体推进剂火箭发动机，其包括具有一体形成的中心管的主体。主燃烧室设置在主体中。二次燃烧室由主体的中心管形成。液体推进剂储存器设置在体内。再生活塞可滑动地设置在主体中，用于将液体推进剂输送到初级和次级燃烧室。活塞包括用于喷射液体推进剂的多个喷射口。点燃器设置在身体中用于引发液体推进剂的燃烧。在中心管的自由端处形成喷嘴以产生推力，其中当点火器燃烧发生在主燃烧室中时，将活塞驱动到液体推进剂储存器中，并且液体推进剂被注入到主燃烧室中以产生燃烧产物被引导到二次燃烧室中并通过喷嘴膨胀。

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