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1. 发明授权

US07571680B1 Ordnance canister with collapsible fuel-storing structure that after descent and impact atomizes and forcefully disperses fuel 失效
标题翻译：具有可折叠燃料储存结构的弹性罐，在下降和冲击后雾化并强制分散燃料
公开(公告)号：US07571680B1
公开(公告)日：2009-08-11
申请号：US11515699
申请日：2006-09-05
申请人： Samuel Barran Tafoya
发明人： Samuel Barran Tafoya
IPC分类号： F42B10/00
CPC分类号： F42B12/52 , F42B10/06
摘要： A fuel-storing ordnance canister for release from military aircraft that does not explode upon impact, its collapsible accordion-like structure instead forcefully dispersing atomized fuel in an upwardly direction in the impact zone after descent for dispersal in, around, and beyond the impact zone. When the fuel from multiple canisters is released into a drop zone and later ignited by a dropped or ground-based incendiary device, all life in the dispersal area is eliminated. Tail fins assure nose-down flight and provide handles for easy canister handling and loading onto airplanes. The configuration of a pop-open tail plug allows for its partial release upon canister collapse to create a spray nozzle that atomizes the fuel stored in the canister as it is being dispersed. The most preferred application is by the U.S. Military to eliminate terrorists hiding in caves, hidden ordnance, and other areas previously resistant to air-released ordnance.
摘要翻译：用于从军用飞机上释放的储存燃料的弹药筒，其不会在冲击时爆炸，其可折叠的类风琴式结构反而在下降之后强力地将雾化燃料分散在冲击区域中，以将其分散在冲击区域内部，之外和之外。当来自多个罐的燃料被释放到下降区域中并且随后被落地或地基燃烧装置点燃时，消除了分散区域中的所有寿命。尾翼确保了下降的飞行，并提供手柄，便于罐子处理和装载到飞机上。弹开式尾塞的构造允许其在罐崩溃时的部分释放以产生喷雾喷嘴，其在储存在罐中的燃料在其被分散时雾化。最优选的应用是由美国军方消除躲在洞穴，隐藏的武器以及其他以前抵抗空中弹药的地区的恐怖分子。

2. 发明授权

US07618005B1 Stealth bomber, transporter, air-to-air fueling tanker, and space plane 失效
标题翻译：隐形轰炸机，运输机，空对空加油车和太空飞机
公开(公告)号：US07618005B1
公开(公告)日：2009-11-17
申请号：US11789718
申请日：2007-04-25
申请人： Samuel Barran Tafoya
发明人： Samuel Barran Tafoya
IPC分类号： B64C1/10
CPC分类号： B64C1/064 , B64C1/065 , B64C2039/105 , Y02T50/12
摘要： A stealth transporter aircraft having a rhomboid airframe with a dihedral bottom surface and a top surface designed as an airfoil. The rhomboid cross-sectional configuration of the airframe gives it increased lift, stealth characteristics, and enhanced load bearing capacity. The aircraft does not have conventional wing structure and its dihedral bottom surface allows it to make wheels-up emergency landings on water and hard runway surfaces with greater pilot survivability. A rigid central tubular area extending nearly the full length of the airframe is configured for passengers, luggage, munitions, and/or equipment and provides a backbone for the aircraft. The aircraft further has rear engines, a large fuel carrying capability, and may also undergo primarily interior modifications for function as a space plane or air-to-air fueling tanker. A vortex spoiler on the side edges of the airframe is also preferred, which eliminates trails while in high altitude flight.
摘要翻译：隐形运输机具有具有二面底面的菱形机身和设计为翼型的顶面。机身的菱形横截面结构提高了提升，隐形特性和增强的承载能力。飞机没有传统的机翼结构，其二面底面允许其在水和硬的跑道表面上轮起紧急着陆，具有更大的飞行员生存能力。延伸几乎整个机身长度的刚性中央管状区域被配置为乘客，行李箱，弹药和/或设备，并为飞行器提供骨干。飞机还具有后发动机，具有大的燃料承载能力，并且还可以主要进行内部修改以用作空间飞机或空对空加油车。在机身侧边缘的涡流扰流器也是优选的，这在高空飞行中消除了小径。

3. 发明授权

US07168523B1 Mechanic's step with stirrup 失效
标题翻译：机械师的步骤与马镫
公开(公告)号：US07168523B1
公开(公告)日：2007-01-30
申请号：US11374606
申请日：2006-03-14
申请人： Craig A. Tafoya , Mary E Tafoya , Samuel Barran Tafoya
发明人： Craig A. Tafoya , Mary E Tafoya , Samuel Barran Tafoya
IPC分类号： B60R3/00
CPC分类号： B60R3/007
摘要： A suspended step assembly that is attachable over the tire of a motor vehicle and which can support a mechanic working in the engine compartment. It has a frame that can be broken down into sub-parts for compact storage in a motor vehicle, is easy and fast to assemble and disassemble, is adjustable to differing tire widths, has an upper configuration that securely hooks over the top of the tire, has a strong and simple closed-loop tubular structure that resists parallelogram deforming while under load, has a step that is secured into a fixed position on the frame without fasteners, and has a bottom stirrup under its step. Applications may include, but are not limited to, use by mechanics to more easily and efficiently perform engine work, and use by those needing to clean or otherwise have access to the upper portions of high-profile vehicles.
摘要翻译：一种可悬挂在机动车辆的轮胎上并且可以支撑在发动机舱中工作的机械师的悬挂台阶组件。它具有可以分解成子部件以便在机动车辆中紧凑存储的框架，容易且快速的组装和拆卸，可调整到不同的轮胎宽度，具有牢固地钩在轮胎顶部上方的上部构造具有坚固且简单的闭环管状结构，其在负载下抵抗平行四边形变形，具有在没有紧固件的情况下固定在框架上的固定位置的台阶，并且在其台阶下具有底部箍筋。应用可以包括但不限于由机械师更容易和有效地执行发动机工作，以及需要清洁或以其他方式进入高调车辆的上部的那些使用。

4. 发明授权

US07164211B1 Vehicle assisted power generator 失效
标题翻译：车载发电机
公开(公告)号：US07164211B1
公开(公告)日：2007-01-16
申请号：US11374589
申请日：2006-03-14
申请人： Craig A. Tafoya , Mary E Tafoya , Samuel Barran Tafoya
发明人： Craig A. Tafoya , Mary E Tafoya , Samuel Barran Tafoya
IPC分类号： B61L3/12 , H02K41/00
CPC分类号： H02K35/06 , H02K7/1869
摘要： A system and method whereby power pods having multiple permanent magnets or coils of wire with a very low voltage charge create a multiple magnetic fields within frequently traveled roadways and other surfaces so that voltage is created when vehicles carrying ferrous metal pass over it. The most efficient areas for electrical generation are the downhill sides of bridges, hills, and mountain grades, although the power pods may be used on substantially flat surfaces if not too closely spaced together to drain inertia from passing vehicles. An added benefit on inclined surfaces, the magnetic field would have a speed-reducing effect on the vehicles. Enhancement of electrical generation via the present invention system could be achieved by installing a permanent magnet on vehicular and railroad traffic. Applications may include, but are not limited to, highways and railroads.
摘要翻译：具有多个永久磁铁或具有非常低电压电荷的线圈的电源盒的系统和方法在经常行进的道路和其它表面中产生多个磁场，使得当携带有色金属的车辆通过时产生电压。发电最有效的区域是桥梁，山丘和山坡的下坡，尽管如果不太紧密地分开，动力舱可以用在基本上平坦的表面上，以排除过往车辆的惯性。对于倾斜表面还有一个好处，磁场将对车辆产生减速效果。通过在车辆和铁路交通上安装永磁体可以实现通过本发明系统增强发电。应用可以包括但不限于公路和铁路。

5. 发明授权

US06981902B1 Marine reaction thruster 失效
标题翻译：海洋反应推进器
公开(公告)号：US06981902B1
公开(公告)日：2006-01-03
申请号：US10700027
申请日：2003-11-03
申请人： Samuel Barran Tafoya , Hans Guenter Broemel
发明人： Samuel Barran Tafoya , Hans Guenter Broemel
IPC分类号： B63H11/103
CPC分类号： B63H11/08 , B63H11/103 , B63H2011/084
摘要： A propulsion system designed to propel submarine and surface vessels by discharging fluid rearwardly with a reaction of increased force that is approximately twenty percent greater than that possible with conventional propeller systems. Its conical/tapered housing is mounted to the inside bottom surface and transom of a marine vessel hull whereby a keyhole-shaped inlet opening directs a large volume of seawater into the housing's wider end. Seawater then flows across several increasingly smaller propellers positioned within the housing. A reverse and steering assembly with a movable gate can be optionally aligned with the discharge end of the housing to control the direction of marine vessel movement. Size is not a limiting factor for the present invention and its operation is virtually silent. Also, its inlet opening is always below the water level so priming is never needed and no transmission is required. Recreational, commercial, and military applications are contemplated.
摘要翻译：推进系统旨在通过向后排出液体来推动潜艇和水面船只，反应是增加的力，比常规螺旋桨系统可能的大约大20％。其锥形/锥形壳体安装在船体船体的内部底部表面和横梁上，由此锁眼形入口将大量海水引导到壳体的较宽端部。然后海水穿过位于壳体内的几个越来越小的螺旋桨。具有可移动门的反向和转向组件可以可选地与壳体的排出端对准以控制船舶运动的方向。尺寸不是本发明的限制因素，其操作实际上是无声的。此外，其入口开口始终低于水位，因此不需要启动，并且不需要传输。预期休闲，商业和军事应用。

6. 发明授权

US07207286B2 Tri-point hydro sled 失效
标题翻译：三点水车
公开(公告)号：US07207286B2
公开(公告)日：2007-04-24
申请号：US11127998
申请日：2005-05-12
申请人： Samuel Barran Tafoya
发明人： Samuel Barran Tafoya
IPC分类号： B63B1/32
CPC分类号： B63B1/20 , B63B2001/201 , B63B2001/202 , B63B2001/203 , B63H11/08
摘要： A marine vessel that planes over the water in a straight ahead mode and has a V-shaped bow configuration, two lateral rails, a water jet intake aft of the bow, and a water jet discharge through the transom above the water line. The vessel's tri-point contact with the water at high speeds permits sled-like movement with minimal wet area under the hull along the center aft of the water jet intake. It moves fast through the water, is stable, moves smoothly and silently through the water, makes little wake, and makes hard turns without loss of velocity. At idle and slow speed it is low in the water, while at high speed it rides high on the water with only the bow and rear rails in contact with the water. Vessel size and scale are not limiting factors. Applications include, but are not limited to, military, recreational, and sporting uses.
摘要翻译：一艘海洋船舶，以直线前进的方式在水面上飞行，并具有V形弓形结构，两个横向轨道，船尾后部的水射流进气口以及通过水管线上方的横梁排出的水射流。船舶与水的高速三点接触允许滑架状运动，船体沿着水射流入口的中心后方，具有最小的湿润面积。它快速移动通过水面，稳定，平稳无声地移动通过水中，几乎没有唤醒，并且在不损失速度的情况下进行硬转弯。在空闲和缓慢的速度下，它在水中低，而在高速时，它只能在水和水中接触到弓和后轨。船只尺寸和尺寸不是限制因素。应用包括但不限于军事，娱乐和体育用途。

7. 发明授权

US06983604B1 Thermodynamic pressure generator 失效
标题翻译：热力学压力发生器
公开(公告)号：US06983604B1
公开(公告)日：2006-01-10
申请号：US10903801
申请日：2004-07-30
申请人： Samuel Barran Tafoya
发明人： Samuel Barran Tafoya
IPC分类号： F02C5/02 , F02C3/14
CPC分类号： F02C5/02 , F01D15/02 , F02C3/16 , F02C5/12
摘要： A thermodynamic pressure generator having an oscillating valve that allows premixed fuel to enter a combustion chamber in turbulence, until it comes into contact with an annular spoiler, which converts a portion of the fuel into a Karmon vortex ring for delayed ignition. A continuous spark then ignites the remaining fuel with rapid pressure rise that kills the vortex. The fuel in the vortex goes from laminar to turbulence, adding fuel to the already burning charge, super charging it and permitting total ignition. Thus, present invention exhaust contains no polluting by-products and only sensible heat is released into the environment. Exhaust gases are released radially through turbine vanes having a shape that permits a relatively low rotational speed, with sufficient peripheral speed to create torque of considerable degree. Applications include, but are not limited to, land transportation vehicles, propeller-driven airplanes, and marine vessels.
摘要翻译：一种具有摆动阀的热力学压力发生器，该摆动阀允许预混合燃料在湍流中进入燃烧室，直到其与环形扰流板接触，该环形扰流器将燃料的一部分转换成卡门涡流环用于延迟点火。连续的火花然后以快速的压力上升点燃剩余的燃料，从而杀死涡流。涡流中的燃料从层流到湍流，将燃料添加到已经燃烧的电荷中，超级充电并允许总点火。因此，本发明废气不含污染副产物，只有显热被释放到环境中。废气通过涡轮叶片径向释放，该涡轮叶片具有允许相对较低转速的形状，具有足够的圆周速度以产生相当程度的扭矩。应用包括但不限于陆路运输车辆，螺旋桨驱动的飞机和船舶。

8. 发明授权

US06935980B1 Infinitely variable geared transmission 失效
标题翻译：无级变速齿轮传动
公开(公告)号：US06935980B1
公开(公告)日：2005-08-30
申请号：US10930389
申请日：2004-08-31
申请人： Craig Allen Tafoya , Samuel Barran Tafoya
发明人： Craig Allen Tafoya , Samuel Barran Tafoya
IPC分类号： B63H23/06 , B63H23/26 , F16H37/08 , F16H47/08 , F16H48/06
CPC分类号： F16H47/085 , B63H23/06 , B63H23/26 , B63H2023/0275 , B63H2023/0283 , F16H37/0833
摘要： A compact transmission that is infinitely variable and load sensitive. It incorporates a standard hydrodynamic torque converter, however, this converter does not use a lock-up device. Instead engaged gears progressively change ratio output without shifting, thus eliminating the momentary power loss between shifts. It requires no special tooling and can be made from readily available over-the-counter parts. Thus, it is less expensive to manufacture than the transmissions and gearboxes currently used in modern vehicular and marine applications.
摘要翻译：紧凑型传动，无级可变，负载敏感。它集成了一个标准的液力变矩器，但是，该转换器不使用锁定装置。替代的啮合齿轮逐渐变化比率输出而不移动，从而消除了换档之间的瞬时功率损耗。它不需要特殊的工具，可以由现成的非处方零件制成。因此，与目前在现代车辆和船舶应用中使用的变速箱和变速箱相比，制造成本更低。

9. 发明授权

US06699087B1 High-volume, no-drag sea chest with purge capability 失效
标题翻译：大容量，无阻力的海胸具有清除能力
公开(公告)号：US06699087B1
公开(公告)日：2004-03-02
申请号：US10394907
申请日：2003-03-21
申请人： Samuel Barran Tafoya , Hans Guenter Broemel
发明人： Samuel Barran Tafoya , Hans Guenter Broemel
IPC分类号： B63H2110
CPC分类号： B63B13/00 , B63B2013/005 , B63H21/383 , F01P11/06 , F01P2011/065 , F01P2050/02
摘要： A sea chest that can provide a large volume of water substantially without drag or cavitation for cooling the inboard engines of a marine vessel. The keyhole shape through the bottom surface of the sea chest is critical to its function and causes eddys to form at its outside edges, as well as water to flow into the sea chest at the center of these edges. The present invention sea chest also has an orifice through which a quick burst of air or water can be sent to clean debris clogs and eliminate the need for manual cleaning. Present invention size and mounting location are determined by its application. Although not limited thereto, use of the present invention is generally contemplated for large and high-speed marine vessels. However the present invention can also provide benefit to smaller marine vessels, including those as small in length as twenty feet.
摘要翻译：可以提供基本上没有阻力或气蚀的大量水的海底来冷却海洋船只的内侧发动机。通过海底底部的锁眼形状对其功能至关重要，导致其外缘形成eddys，以及水流入这些边缘中心的海底。本发明的海底还具有孔口，通过该孔口可以发送快速爆发的空气或水以清洁碎屑堵塞并且消除对手动清洁的需要。本发明的尺寸和安装位置由其应用确定。尽管不限于此，但是大体上和高速海洋容器通常考虑使用本发明。然而，本发明还可以为较小的海洋容器提供益处，包括长度小于二十英尺的那些。

10. 发明授权

US07581699B1 Stealth attack fighter bomber 失效
标题翻译：隐形攻击战斗机轰炸机
公开(公告)号：US07581699B1
公开(公告)日：2009-09-01
申请号：US11732250
申请日：2007-04-03
申请人： Samuel Barran Tafoya
发明人： Samuel Barran Tafoya
IPC分类号： B64C1/00
CPC分类号： B64C1/0009 , B64C3/10 , B64C3/16 , B64C2039/105 , B64D7/00
摘要： A fighter bomber aircraft having a rhomboid airframe with a dihedral bottom surface and a top surface designed as an airfoil. The rhomboid cross-sectional configuration gives it increased lift, stealth characteristics, and enhanced load-bearing capacity. It also has two central tubes stacked on top of one another and extending front-to-rear, with the upper tube extending part way through the airframe and preferably housing a pilot, guns forward from and in line with the pilot, a gear/equipment compartment behind the pilot, and fuel tanks positioned behind the gear/equipment compartment. The lower tube extends substantially throughout the airframe and preferably houses the air-intake for the engine, radar, nose gear, bombs, and rear engine. The aircraft has no conventional wing structure and its dihedral bottom surface allows it to make wheels-up emergency landings on water and hard runway surfaces. In addition, rockets can be optionally mounted on the top of the lift area.
摘要翻译：一架具有菱形机身的战斗轰炸机，具有双面底面，顶面设计为翼型。菱形横截面结构提高了提升，隐形特性和增强的承载能力。它还具有彼此顶部彼此堆叠并且前后延伸的两个中央管，其中上管部分地延伸穿过机身并且优选地容纳导向器，从飞行员向前并与之对齐，齿轮/设备飞行员后面的舱室和位于齿轮/设备舱后面的油箱。下管基本上延伸穿过机身，并且优选地容纳用于发动机，雷达，前置齿轮，炸弹和后发动机的进气口。飞机没有传统的机翼结构，其二面底面允许其在水和硬的跑道表面上轮起紧急着陆。此外，火箭可以可选地安装在电梯区域的顶部。

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