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1.发明申请公开(公告)号：US20130146715A1
公开(公告)日：2013-06-13
申请号：US13324537
申请日：2011-12-13
IPC分类号： B64C23/06
CPC分类号： B64C21/10 , B64C23/069 , Y02T50/164 , Y02T50/166
摘要： An airfoil tip vortex mitigation arrangement comprising one or more flow directors configured and positioned to re-direct freestream air over a low pressure surface of an airfoil in such a way as to displace and weaken a main tip vortex generated at a tip of the airfoil.
摘要翻译： 翼型顶端涡流减轻装置，包括一个或多个流动导向器，其构造和定位成在翼型的低压表面上重新引导自由流空气，以便移位和减弱在翼型的尖端处产生的主尖端涡流。
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公开(公告)号：US09795812B2
公开(公告)日：2017-10-24
申请号：US13214532
申请日：2011-08-22
申请人： Eric F. Charlton
发明人： Eric F. Charlton
摘要： A method and apparatus for delivering fire retardant to a ground fire from an aircraft. The apparatus includes a dispenser casing that dispenses fire retardant after the casing has been released from an aircraft. The apparatus includes a dispenser fuse that actuates the dispenser casing to dispense the fire retardant in response to one or more predetermined conditions.
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公开(公告)号：US20130048317A1
公开(公告)日：2013-02-28
申请号：US13214532
申请日：2011-08-22
申请人： Eric F. Charlton
发明人： Eric F. Charlton
摘要： A method and apparatus for delivering fire retardant to a ground fire from an aircraft. The apparatus includes a dispenser casing that dispenses fire retardant after the casing has been released from an aircraft. The apparatus includes a dispenser fuse that actuates the dispenser casing to dispense the fire retardant in response to one or more predetermined conditions.
摘要翻译： 一种用于将火焰从飞机运送到地面火上的方法和装置。 该装置包括分配器壳体，其在壳体从飞行器释放之后分配阻燃剂。 该装置包括分配器保险丝，其致动分配器壳体以响应于一个或多个预定条件分配阻燃剂。
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4.发明授权System, method and apparatus for windblast reduction during release or ejection from aircraft 有权飞机释放或喷射期间减少风力的系统，方法和装置公开(公告)号：US08033504B2
公开(公告)日：2011-10-11
申请号：US12145558
申请日：2008-06-25
申请人： Mike I. Jones , Glenn W. Baird , Eric F. Charlton
发明人： Mike I. Jones , Glenn W. Baird , Eric F. Charlton
摘要： The invention reduces the impact of flowfield forces on objects launched from high speed aircraft during flight. For example, the invention provides a solution for overcoming ejection windblast injuries to pilots and increases the probability of injury-free or low-injury ejection. The gas flow is used to rapidly create a very short duration protective “bubble” in the incoming air flow ahead of the ejecting pilot. The bubble reduces the local flow velocity and aerodynamic forces on the pilot during the injury-critical time period of ejection. The invention also is suitable for reducing the intensity of flowfield forces that act on released military aircraft ordnance, such as bombs and missiles.
摘要翻译： 本发明减少了飞行中的力场对飞行中从高速飞机发射的物体的影响。 例如，本发明提供了一种解决方案，用于克服对飞行员造成的喷射伤害，并增加无伤害或低伤害弹射的可能性。 气流用于在喷射导向器之前的进入空气流中快速创建非常短的保护“气泡”。 在喷射的伤害关键时间段期间，气泡减少了飞行员上的局部流速和空气动力。 本发明也适用于减少对释放的军用飞机弹药（如炸弹和导弹）起作用的流场力的强度。
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5.发明授权Minimally intrusive wingtip vortex wake mitigation using inside-mold-line surface modifications 有权使用内模线表面修饰的微小侵入式翼尖涡流苏醒公开(公告)号：US08960609B2
公开(公告)日：2015-02-24
申请号：US13326592
申请日：2011-12-15
申请人： Perry Wooden , Ruble E. Moor , Eric F. Charlton , Daniel N. Miller , Edwin L. Blosch , Jeffrey J. Azevedo
发明人： Perry Wooden , Ruble E. Moor , Eric F. Charlton , Daniel N. Miller , Edwin L. Blosch , Jeffrey J. Azevedo
IPC分类号： B64C23/06
CPC分类号： B64C21/02 , B64C23/065 , B64C2003/143 , B64C2230/20 , Y02T50/164 , Y02T50/166
摘要： An airfoil tip vortex mitigation device comprising an intake port disposed in a first surface of an airfoil and an exit port in fluid communication with the intake port and disposed in a second surface of the airfoil where air pressure is less than at the first surface when the airfoil is producing lift. The channel and exit port are positioned and configured to direct diverted air in such a way as to weaken an airfoil tip vortex that's produced by the airfoil when the airfoil is producing lift.
摘要翻译： 一种翼型端涡流缓解装置，包括设置在翼型件的第一表面中的进气口和与进气口流体连通的出口，并且设置在翼型件的第二表面中，其中当空气压力小于第一表面时， 机翼正在生产电梯。 通道和出口定位和构造成引导转向的空气，以便当翼型件产生升力时削弱由翼型件产生的翼型顶端涡流。
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6.发明申请公开(公告)号：US20130153711A1
公开(公告)日：2013-06-20
申请号：US13326592
申请日：2011-12-15
申请人： Perry Wooden , Ruble E. Moor , Eric F. Charlton , Daniel N. Miller , Edwin L. Blosch , Jeffrey J. Azevedo
发明人： Perry Wooden , Ruble E. Moor , Eric F. Charlton , Daniel N. Miller , Edwin L. Blosch , Jeffrey J. Azevedo
IPC分类号： B64C23/06
CPC分类号： B64C21/02 , B64C23/065 , B64C2003/143 , B64C2230/20 , Y02T50/164 , Y02T50/166
摘要： An airfoil tip vortex mitigation device comprising an intake port disposed in a first surface of an airfoil and an exit port in fluid communication with the intake port and disposed in a second surface of the airfoil where air pressure is less than at the first surface when the airfoil is producing lift. The channel and exit port are positioned and configured to direct diverted air in such a way as to weaken an airfoil tip vortex that's produced by the airfoil when the airfoil is producing lift.
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公开(公告)号：US09896192B2
公开(公告)日：2018-02-20
申请号：US13324537
申请日：2011-12-13
CPC分类号： B64C21/10 , B64C23/069 , Y02T50/164 , Y02T50/166
摘要： An airfoil tip vortex mitigation arrangement comprising one or more flow directors configured and positioned to re-direct freestream air over a low pressure surface of an airfoil in such a way as to displace and weaken a main tip vortex generated at a tip of the airfoil.
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8.发明申请SYSTEM, METHOD AND APPARATUS FOR WINDBLAST REDUCTION DURING RELEASE OR EJECTION FROM AIRCRAFT 有权飞机释放或排放期间降低风量的系统，方法和装置公开(公告)号：US20090321570A1
公开(公告)日：2009-12-31
申请号：US12145558
申请日：2008-06-25
申请人： Mike I. Jones , Glenn W. Baird , Eric F. Charlton
发明人： Mike I. Jones , Glenn W. Baird , Eric F. Charlton
IPC分类号： B64D25/115 , B64D1/12
摘要： The invention reduces the impact of flowfield forces on objects launched from high speed aircraft during flight. For example, the invention provides a solution for overcoming ejection windblast injuries to pilots and increases the probability of injury-free or low-injury ejection. The gas flow is used to rapidly create a very short duration protective “bubble” in the incoming air flow ahead of the ejecting pilot. The bubble reduces the local flow velocity and aerodynamic forces on the pilot during the injury-critical time period of ejection. The invention also is suitable for reducing the intensity of flowfield forces that act on released military aircraft ordnance, such as bombs and missiles.
摘要翻译： 本发明减少了飞行中的力场对飞行中从高速飞机发射的物体的影响。 例如，本发明提供了一种解决方案，用于克服对飞行员造成的喷射伤害，并增加无伤害或低伤害弹射的可能性。 气流用于在喷射导向器之前的进入空气流中快速创建非常短的保护“气泡”。 在喷射的伤害关键时间段期间，气泡减少了飞行员上的局部流速和空气动力。 本发明也适用于减少对释放的军用飞机弹药（如炸弹和导弹）起作用的流场力的强度。
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