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1. 发明授权

US07806035B2 Safety vent device 有权
标题翻译：安全排气装置
公开(公告)号：US07806035B2
公开(公告)日：2010-10-05
申请号：US12137671
申请日：2008-06-12
申请人： Garry R. Kaiser , Colby W. Ross , Tracy L. Graham , Mark L. Sloan
发明人： Garry R. Kaiser , Colby W. Ross , Tracy L. Graham , Mark L. Sloan
IPC分类号： E21B43/116
CPC分类号： E21B43/119
摘要： A perforating gun system having a relief system for relieving high pressure during unexpected high temperature or situations that may produce rupture of the gun body. The relief system may be responsive either to high temperatures as well as high pressures. In the high temperature situation, the relief system has a fuseable link that melts thereby allowing movement of a piston to open vent communication between the inside of a gun body in the ambient conditions. Similarly, a pressure device includes a piston responsive to pressure that moves under high pressure within the gun body thereby exposing a port enabling communication between the inside of the gun body and the ambient conditions.
摘要翻译：一种穿孔枪系统，其具有用于在意外高温下释放高压的释放系统或可能产生枪体破裂的情况。释放系统可以响应于高温以及高压。在高温情况下，释放系统具有熔化的连接件，从而允许活塞在环境条件下在枪体的内部之间开放通气连通。类似地，压力装置包括响应于在枪体内高压下移动的压力的活塞，从而暴露出能够使枪体内部和周围环境之间进行连通的端口。

2. 发明申请

US20080307951A1 SAFETY VENT DEVICE 有权
标题翻译：安全通风装置
公开(公告)号：US20080307951A1
公开(公告)日：2008-12-18
申请号：US12137671
申请日：2008-06-12
申请人： Garry R. Kaiser , Colby W. Ross , Tracy L. Graham , Mark L. Sloan
发明人： Garry R. Kaiser , Colby W. Ross , Tracy L. Graham , Mark L. Sloan
IPC分类号： E21B43/117
CPC分类号： E21B43/119
摘要： A perforating gun system having a relief system for relieving high pressure during unexpected high temperature or situations that may produce rupture of the gun body. The relief system may be responsive either to high temperatures as well as high pressures. In the high temperature situation, the relief system has a fuseable link that melts thereby allowing movement of a piston to open vent communication between the inside of a gun body in the ambient conditions. Similarly, a pressure device includes a piston responsive to pressure that moves under high pressure within the gun body thereby exposing a port enabling communication between the inside of the gun body and the ambient conditions.
摘要翻译：一种穿孔枪系统，其具有用于在意外高温下释放高压的释放系统或可能产生枪体破裂的情况。释放系统可以响应于高温以及高压。在高温情况下，释放系统具有熔化的连接件，从而允许活塞在环境条件下在枪体的内部之间开放通气连通。类似地，压力装置包括响应于在枪体内在高压下移动的压力的活塞，从而暴露出能够使枪身内部和周围环境之间进行连通的端口。

3. 发明授权

US5222359A Nozzle system and method for supersonic jet engine 失效
标题翻译：用于超音速喷气发动机的喷嘴系统和方法
公开(公告)号：US5222359A
公开(公告)日：1993-06-29
申请号：US722944
申请日：1991-06-28
申请人： Garry W. Klees , Gary L. Lidstone , Mark L. Sloan
发明人： Garry W. Klees , Gary L. Lidstone , Mark L. Sloan
IPC分类号： F02C7/04 , F02K1/38 , F02K3/075
CPC分类号： F02C7/04 , F02K1/386 , F02K3/075 , B64D2033/026 , F05D2220/80
摘要： A supersonic jet engine for improved noise abatement and thrust augmentation. There is an intake section, an engine, a mixing section, an exhaust section, and a secondary air passageway. Ambient air is directed into the engine and into the secondary air passageway. Exhaust from the engine and the secondary air are directed into primary and secondary segments to mix in a stream direction as supersonic flow. Selectively controllable primary bypass passageways are provided at the primary passageway segments and are operated to bypass the primary flow through the primary segments at times when greater primary flow area is required.
摘要翻译：一种超音速喷气发动机，用于改善噪声消除和推力增大。有进气段，发动机，混合段，排气段和二次空气通道。环境空气被引导到发动机中并进入二次空气通道。来自发动机和二次空气的排气被引导到一级和二级段，以在流动方向上作为超音速流动混合。在主通道段处设置选择性可控的主旁通通路，并且在需要更大的主流动区域的时候，操作以旁通通过主段的主流。

4. 发明授权

US5129227A Low speed engine for supersonic and hypersonic vehicles 失效
标题翻译：用于超级和超级车辆的低速发动机
公开(公告)号：US5129227A
公开(公告)日：1992-07-14
申请号：US683350
申请日：1991-04-10
申请人： Garry W. Klees , Mark L. Sloan , Russel L. Thornock
发明人： Garry W. Klees , Mark L. Sloan , Russel L. Thornock
IPC分类号： F02K7/12
CPC分类号： F02K7/12 , Y02T50/671
摘要： A jet engine for use in a hypersonic aircraft. A fuel rich injectant is injected into the mixing zone of a duct at a substantial downstream angle to form an ejector. The temperature of the injectant is sufficiently low that spontaneous combustion of the injectant is delayed until the injectant reaches the combustion zone of the duct. In order to prevent combustion from propagating upstream from the combustion zone, the equivalence ratio of the mixture of injectant and ambient air flowing along the wall of the duct is maintained at a relatively high value, and the velocity profile of the flow along the wall of the duct is maintained at a relatively high value.

5. 发明授权

US06679327B2 Internal oriented perforating system and method 有权
标题翻译：内部定向穿孔系统及方法
公开(公告)号：US06679327B2
公开(公告)日：2004-01-20
申请号：US10021799
申请日：2001-11-30
申请人： Mark L. Sloan , Erick R. Rantala
发明人： Mark L. Sloan , Erick R. Rantala
IPC分类号： E21B43119
CPC分类号： E21B43/119
摘要： One embodiment of the present invention discloses a system and method for orienting perforating guns inside of slanted or deviated wellbores. The invention involves adding a weight inside of the guns to gravitate the gun to a specified orientation. The weight is situated on the outer circumference of the gun tube and within the inner diameter of the gun body. The invention is capable of orienting the gun in any radial position without affecting the shot performance of any of the shaped charges.
摘要翻译：本发明的一个实施例公开了一种用于将穿孔枪定向在倾斜或偏斜的井筒内的系统和方法。本发明涉及在枪内添加一个重物，以将喷枪推向指定的方位。重量位于枪管的外圆周上并且位于枪体的内径内。本发明能够将枪定向在任何径向位置，而不影响任何成形装料的喷射性能。

6. 发明授权

US4507552A Method and apparatus for determining flow characteristics within a well 失效
标题翻译：用于确定井内流量特性的方法和装置
公开(公告)号：US4507552A
公开(公告)日：1985-03-26
申请号：US410276
申请日：1982-08-23
申请人： Raymond E. Roesner , Mark L. Sloan
发明人： Raymond E. Roesner , Mark L. Sloan
IPC分类号： E21B47/10 , G01V5/00
CPC分类号： E21B47/1015
摘要： In the representative embodiments of the new and improved methods and apparatus disclosed herein, a well logging instrument includes an elongated body member having a funnel configuration fluid collector mounted thereon. An aperture in the body member, proximate the apex of the collector, allows discharge of the fluid through a passage in the body member, past a pair of radiation detectors, thereafter returning into the well. A tracer ejector valve assembly is mounted proximate the apex of the funnel and the aperture therein for selectively injecting a quantity of radioactive tracer element into the fluid flow. The tracer element is detected by the pair of detectors with the signals provided therefrom used to determine flow characteristics of the fluids within the well.
摘要翻译：在本文公开的新的和改进的方法和装置的代表性实施例中，测井仪器包括细长的主体构件，其具有安装在其上的漏斗形流体收集器。身体构件中的靠近收集器顶点的孔允许流体通过身体构件中的通道排出，经过一对辐射检测器，然后返回到井中。示踪剂排出阀组件安装在漏斗的顶点附近，并且其中的孔用于选择性地将一定量的放射性示踪元件注入到流体流中。示踪元件由一对检测器检测，其中提供的信号用于确定井内的流体的流动特性。

7. 发明授权

US07757767B2 Through tubing gun lock 失效
标题翻译：通过管枪锁
公开(公告)号：US07757767B2
公开(公告)日：2010-07-20
申请号：US12043542
申请日：2008-03-06
申请人： Freeman L. Hill , Randy L. Evans , Mark L. Sloan
发明人： Freeman L. Hill , Randy L. Evans , Mark L. Sloan
IPC分类号： E21B23/00
CPC分类号： E21B43/119 , E21B23/01
摘要： A lock for a perforating gun system comprising, a housing, a cylinder formed in the housing, a piston assembly disposed within the cylinder, and anchoring arms coupled with the piston assembly. Detonation of the shaped charges of an associated perforating gun produces a pressure surge which is communicated to a surface of the piston assembly. Appropriate movement of the piston assembly outwardly rotates the anchoring arms into anchoring engagement with an associated tubular. Thus the pressure from the detonation event will anchor a perforating system within its associated tubular.
摘要翻译：一种用于射孔枪系统的锁，包括壳体，形成在壳体中的气缸，设置在气缸内的活塞组件以及与活塞组件联接的锚定臂。相关联的射孔枪的成形电荷的爆震产生压力浪涌，其被传递到活塞组件的表面。活塞组件的适当运动将锚定臂向外转动成与相关联的管状物的固定接合。因此，来自引爆事件的压力将将穿孔系统锚定在其相关管状体内。

8. 发明授权

US07210524B2 Perforating gun quick connection system 有权
标题翻译：穿孔枪快速连接系统
公开(公告)号：US07210524B2
公开(公告)日：2007-05-01
申请号：US10703114
申请日：2003-11-06
申请人： Mark L. Sloan , Randy C. Schutte
发明人： Mark L. Sloan , Randy C. Schutte
IPC分类号： E21B43/119
CPC分类号： E21B43/119 , E21B17/046 , F16L37/0985 , Y10T403/1641
摘要： A connection system to be used in conjunction with a perforating gun comprising a top sub formed to receive one end of a gun body of a perforating gun, a circumferential groove disposed on the outer surface of the gun body, and a collet secured to the top sub. The collet has at least one finger that engages the groove. Engaging the groove with the at least one finger of the collect connects the gun body to the top sub. A cover sleeve is included that retains the finger in connective engagement with the groove.
摘要翻译：一种与射孔枪结合使用的连接系统，包括形成为接收射孔枪的枪体的一端的顶部子弹，设置在枪体的外表面上的周向槽，以及固定到顶部的夹头子夹头具有至少一个接合凹槽的指状物。将凹槽与收集器的至少一个手指接合将枪体连接到顶部副。包括保持手指与凹槽连接的盖套筒。

9. 发明授权

US5779169A Aircraft engine inlet hot gas and foreign object ingestion reduction and pitch control system 失效
标题翻译：飞机引擎入口热气和异物摄入减少和俯仰控制系统
公开(公告)号：US5779169A
公开(公告)日：1998-07-14
申请号：US573047
申请日：1995-12-15
申请人： Mark L. Sloan
发明人： Mark L. Sloan
IPC分类号： B64C15/14 , B64C29/00 , B64D33/02 , F02K1/00 , F02K3/02
CPC分类号： F02K1/002 , B64C15/14 , B64C29/0066 , B64D33/02 , F02K3/025 , B64D2033/026
摘要： An aircraft for vertical or short take off and landing operations having two main lift nozzles, both positioned at or near the aircraft center of gravity utilizes one or more jet screen nozzles, arranged in a variety of shapes and combinations, discharging bypass air from a position forward of the center of gravity, and a variable pitch nozzle discharging engine exhaust gas mixed with bypass air from a position aft of the center of gravity, to achieve pitch control while airborne in vertical take off or landing mode. The jet screen nozzle also prevents or reduces ingestion of mixed hot exhaust gas and bypass air discharged through the main lift nozzles. The jet screen nozzle further prevents or reduces ingestion of foreign object debris disturbed by the vertical lift discharge flowing from the main lift nozzles. Lift improvement devices are deployed during short or vertical takeoff and landing operations to act as air dams to cause main lift nozzle discharge striking the ground and returning to the aircraft as a fountain flow and flowing against the lower surface of the aircraft, to separate from the aircraft surface and return toward the ground. This enhances lift effect on the aircraft while avoiding further hot exhaust gas flow along the aircraft skin surface and eventually into the aircraft engine inlet. A control system modulates the jet screen nozzle and aft pitch control nozzle, along with the cruise nozzle, main lift nozzles and other control nozzles so that total engine discharge flow area remains substantially constant through a range of pitch control and other maneuvering commands.
摘要翻译：一种用于垂直或短时起飞和着陆作业的飞机，其具有两个位于飞机重心处或附近的主要提升喷嘴，其使用一个或多个喷射筛喷嘴，其布置成各种形状和组合，从旁边排出旁路空气重心的前方，以及从重心位置排出与旁路空气混合的发动机废气的可变节距喷嘴，在垂直起飞或着陆模式下实现俯仰控制。喷射式喷嘴还防止或减少了通过主提升喷嘴排出的混合热废气和旁路空气的摄取。喷丝机喷嘴进一步防止或减少由从主升力喷嘴流出的垂直提升排放物而扰乱的异物碎屑摄取。升降机设备在短时或垂直起飞和着陆作业期间部署，作为空气坝，使主升力喷头排放到地面并作为喷泉流返回飞机，并流向飞机的下表面，与飞机的下表面分离飞机表面并返回地面。这增强了对飞行器的提升效果，同时避免了沿着飞机皮肤表面的进一步的热废气流并且最终进入飞机发动机入口。控制系统连同巡航喷嘴，主提升喷嘴和其他控制喷嘴一起调节喷射屏幕喷嘴和后桨距控制喷嘴，使得总发动机排气流动面积通过一系列俯仰控制和其他操纵命令保持基本恒定。

10. 发明申请

US20100243323A1 PRESSURE COMPENSATION FOR A PERFORATING GUN 有权
标题翻译：执行枪的压力补偿
公开(公告)号：US20100243323A1
公开(公告)日：2010-09-30
申请号：US12732943
申请日：2010-03-26
申请人： Jason W. McCann , Mark L. Sloan
发明人： Jason W. McCann , Mark L. Sloan
IPC分类号： E21B43/117
CPC分类号： E21B43/1195
摘要： A perforating system having a perforating gun with a pressurizable gun body. The gun body can be pressurized prior to deployment in a wellbore, or while in the wellbore. Pressurizing the gun body can include adding fluid into the gun body, such as a pressurized gas, a liquid, or combustion products. A seal diaphragm can be used to transfer wellbore pressure into the gun body.
摘要翻译：一种穿孔系统，具有带有可加压枪体的射孔枪。在主体部署在井眼之前，或者在井眼中，枪体可以被加压。加压枪体可以包括将流体添加到枪体中，例如加压气体，液体或燃烧产物。可以使用密封隔膜将井眼压力转移到枪体中。

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