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1. 发明申请

US20090206195A1 ROTATING AIR CARGO DELIVERY SYSTEM AND METHOD OF CONSTRUCTION 有权
标题翻译：旋转空运货物运输系统及其施工方法
公开(公告)号：US20090206195A1
公开(公告)日：2009-08-20
申请号：US11613595
申请日：2006-12-20
申请人： JOSEPH M. COLICH , EDWARD BAROCELA , JAMES LIS
发明人： JOSEPH M. COLICH , EDWARD BAROCELA , JAMES LIS
IPC分类号： B64C27/32 , B64D1/14 , B64C27/50 , B64C13/16 , B23P15/02
CPC分类号： B64D1/08 , B64D19/02 , Y10T29/49337
摘要： A system and method of constructing a system for delivering cargo by airdrop are provided. In short, the system uses rotor blades to slow the descent of cargo dropped from an aircraft. In one example of one embodiment, a frame is secured to a cargo pallet and at least one rotor blade is secured to the frame. The rotor blade is secured to the frame in a position such that it causes the cargo pallet and the frame to rotate in air when dropped from an elevation. In another embodiment, the rotor blade may be extendable and extend during flight.
摘要翻译：提供了一种构建用于通过空投运送货物的系统和方法。简而言之，该系统使用转子叶片来减缓从飞机掉落的货物的下降。在一个实施例的一个示例中，框架被固定到货物托盘，并且至少一个转子叶片固定到框架。转子叶片固定在框架上，使其在从高度下降时使得货物托盘和框架在空气中旋转。在另一个实施例中，转子叶片可以是可延伸的并在飞行期间延伸。

2. 发明申请

US20050258306A1 Delta-winged hybrid airship 有权
标题翻译：三角翼混合飞艇
公开(公告)号：US20050258306A1
公开(公告)日：2005-11-24
申请号：US10853299
申请日：2004-05-24
申请人： Edward Barocela , Patrick Cassidy
发明人： Edward Barocela , Patrick Cassidy
IPC分类号： B64B1/20 , B64C39/10 , B64D27/24
CPC分类号： B64C39/10 , B64B2201/00 , B64D27/24 , B64D2211/00 , Y02T50/55 , Y02T50/64 , Y10S244/901
摘要： In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system may have the shape of a delta-wing. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The delta-wing shape can provide a surface area large enough to accommodate very large circular or elliptical transmission devices. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft at an operational altitude of at least about 85,000 ft for months or even years. The hybrid airship may function as an airborne military communications relay platform.
摘要翻译：一方面，包括外壳，多个氦气填充的气体包络和全电动推进系统的混合式飞艇可以具有三角翼的形状。在一些实施例中，混合式飞艇可以单独使用浮力提升机来启动，而空气动力提升可由全电动推进系统提供。在一个方面，光伏阵列和高能量密度功率存储系统可以组合起来，为推进系统提供动力，使推进系统再生。三角翼形状可以提供足够大的表面积以适应非常大的圆形或椭圆形传输装置。通过不断地对蓄电系统充电，根据一些实施例的混合式飞艇可以在至少约85,000英尺的操作高度上保持高度数月甚至数年。混合型飞艇可以作为空中军事通信中继平台。

3. 发明申请

US20050211827A1 High speed missile wing and associated method 审中-公开
标题翻译：高速导弹翼及相关方法
公开(公告)号：US20050211827A1
公开(公告)日：2005-09-29
申请号：US10811735
申请日：2004-03-29
申请人： Edward Barocela
发明人： Edward Barocela
IPC分类号： B64C3/38 , F42B15/10
CPC分类号： F42B15/10 , F42B15/105
摘要： A high speed missile and an associated system and method are provided. The missile includes a fuselage member, and an engine carried by the fuselage member and capable of thrusting the missile to transonic speed during flight. A wing actuator is also carried by the fuselage member, and a wing member is pivotally movable by the wing actuator. Advantageously, the wing member may pivot from a fore-aft position aligned along the fuselage member to various sweep angles, and the wing actuator is capable of pivoting the wing member to a predetermined sweep angle.
摘要翻译：提供了一种高速导弹及相关的系统和方法。导弹包括一个机身成员和一个由机身所承载的引擎，能够在飞行过程中将导弹推向跨音速。机翼致动器也由机身构件承载，翼构件可由翼致动器枢转运动。有利地，翼构件可以从沿着机身构件对准的前后位置枢转到各种扫掠角度，并且翼致动器能够将翼构件枢转到预定的扫掠角度。

4. 发明授权

US07137592B2 High-aspect ratio hybrid airship 有权
标题翻译：高宽比混合飞艇
公开(公告)号：US07137592B2
公开(公告)日：2006-11-21
申请号：US10853300
申请日：2004-05-24
申请人： Edward Barocela , Patrick F. Cassidy
发明人： Edward Barocela , Patrick F. Cassidy
IPC分类号： B64B1/06 , B64C1/00
CPC分类号： B64B1/24 , B64B1/06 , B64B2201/00 , B64D2211/00 , Y02T50/55 , Y10S244/90
摘要： In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system can have a high-aspect ratio wing shape. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The high-aspect ratio wing shape provides low drag, and can allow the hybrid airship to fly at an altitude of at least about 100,000 ft. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft for months or even years. The hybrid airship may function as a military intelligence, surveillance, and reconnaissance and communications relay platform.
摘要翻译：一方面，包括外壳，多个氦气填充的气体包络和全电动推进系统的混合式飞艇可以具有高纵横比的翼形。在一些实施例中，混合式飞艇可以单独使用浮力提升机来启动，而空气动力提升可由全电动推进系统提供。在一个方面，光伏阵列和高能量密度功率存储系统可以组合起来，为推进系统提供动力，使推进系统再生。高纵横比翼形提供了低阻力，并且可以允许混合飞艇在至少约100,000英尺的高度飞行。通过不断地对蓄电系统充电，根据一些实施例的混合式飞艇可以保持高空数月甚至几年。混合型飞艇可以作为军事情报，监视，侦察和通信中继平台。

5. 发明授权

US07014142B2 Low-drag rotor/wing flap 有权
标题翻译：低牵引转子/翼片
公开(公告)号：US07014142B2
公开(公告)日：2006-03-21
申请号：US10770764
申请日：2004-02-03
申请人： Edward Barocela , Charles N. Vaporean
发明人： Edward Barocela , Charles N. Vaporean
IPC分类号： B64C27/22
CPC分类号： B64C3/50 , B64C27/18 , B64C27/24 , B64C39/12 , Y02T50/14
摘要： Rotor/wing aircraft having a low-drag flap are disclosed. In one embodiment, a rotor/wing aircraft includes an elongated blade having a body portion and a flap portion. The body portion has first and second edges and includes a non-symmetric portion proximate the second edge. The flap portion is moveably coupled to the body portion proximate the second edge and is moveable between a rotary flight position and a forward flight position. In the rotary flight position, the flap portion is proximate at least part of the non-symmetric portion to form a second symmetric portion proximate the second edge. In the forward flight position, the flap portion extends away from the non-symmetric portion to form a tapered portion proximate the second edge.
摘要翻译：公开了具有低阻力翼片的转子/翼型飞机。在一个实施例中，转子/翼飞机包括具有主体部分和翼片部分的细长叶片。主体部分具有第一和第二边缘并且包括靠近第二边缘的非对称部分。翼片部分可移动地联接到靠近第二边缘的主体部分，并且可在旋转飞行位置和向前飞行位置之间移动。在旋转飞行位置，翼片部分靠近非对称部分的至少一部分，以形成靠近第二边缘的第二对称部分。在向前飞行位置，翼片部分远离非对称部分延伸以在第二边缘附近形成锥形部分。

6. 发明申请

US20050269441A1 High-aspect ratio hybrid airship 有权
标题翻译：高宽比混合飞艇
公开(公告)号：US20050269441A1
公开(公告)日：2005-12-08
申请号：US10853300
申请日：2004-05-24
申请人： Edward Barocela , Patrick Cassidy
发明人： Edward Barocela , Patrick Cassidy
IPC分类号： B64B1/06 , B64B1/24 , B64D27/24 , B64B1/00
CPC分类号： B64B1/24 , B64B1/06 , B64B2201/00 , B64D2211/00 , Y02T50/55 , Y10S244/90
摘要： In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system can have a high-aspect ratio wing shape. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The high-aspect ratio wing shape provides low drag, and can allow the hybrid airship to fly at an altitude of at least about 100,000 ft. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft for months or even years. The hybrid airship may function as a military intelligence, surveillance, and reconnaissance and communications relay platform.
摘要翻译：一方面，包括外壳，多个氦气填充的气体包络和全电动推进系统的混合式飞艇可以具有高纵横比的翼形。在一些实施例中，混合式飞艇可以单独使用浮力提升机来启动，而空气动力提升可由全电动推进系统提供。在一个方面，光伏阵列和高能量密度功率存储系统可以组合起来，为推进系统提供动力，使推进系统再生。高纵横比翼形提供了低阻力，并且可以允许混合飞艇在至少约100,000英尺的高度飞行。通过不断地对蓄电系统充电，根据一些实施例的混合式飞艇可以保持高空数月甚至几年。混合型飞艇可以作为军事情报，监视，侦察和通信中继平台。

7. 发明授权

US07578479B1 Rotating air cargo delivery system and method of construction 有权
标题翻译：旋转空运货物运输系统及施工方法
公开(公告)号：US07578479B1
公开(公告)日：2009-08-25
申请号：US11613595
申请日：2006-12-20
申请人： Joseph M. Colich , Edward Barocela , James Lis
发明人： Joseph M. Colich , Edward Barocela , James Lis
IPC分类号： B64D1/12
CPC分类号： B64D1/08 , B64D19/02 , Y10T29/49337
摘要： A system and method of constructing a system for delivering cargo by airdrop are provided. In short, the system uses rotor blades to slow the descent of cargo dropped from an aircraft. In one example of one embodiment, a frame is secured to a cargo pallet and at least one rotor blade is secured to the frame. The rotor blade is secured to the frame in a position such that it causes the cargo pallet and the frame to rotate in air when dropped from an elevation. In another embodiment, the rotor blade may be extendable and extend during flight.
摘要翻译：提供了一种构建用于通过空投运送货物的系统和方法。简而言之，该系统使用转子叶片来减缓从飞机掉落的货物的下降。在一个实施例的一个示例中，框架被固定到货物托盘，并且至少一个转子叶片固定到框架。转子叶片固定在框架上，使其在从高度下降时使得货物托盘和框架在空气中旋转。在另一个实施例中，转子叶片可以是可延伸的并在飞行期间延伸。

8. 发明授权

US07093789B2 Delta-winged hybrid airship 有权
标题翻译：三角翼混合飞艇
公开(公告)号：US07093789B2
公开(公告)日：2006-08-22
申请号：US10853299
申请日：2004-05-24
申请人： Edward Barocela , Patrick F. Cassidy
发明人： Edward Barocela , Patrick F. Cassidy
IPC分类号： B64B1/06
CPC分类号： B64C39/10 , B64B2201/00 , B64D27/24 , B64D2211/00 , Y02T50/55 , Y02T50/64 , Y10S244/901
摘要： In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system may have the shape of a delta-wing. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The delta-wing shape can provide a surface area large enough to accommodate very large circular or elliptical transmission devices. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft at an operational altitude of at least about 85,000 ft for months or even years. The hybrid airship may function as an airborne military communications relay platform.
摘要翻译：一方面，包括外壳，多个氦气填充的气体包络和全电动推进系统的混合式飞艇可以具有三角翼的形状。在一些实施例中，混合式飞艇可以单独使用浮力提升机来启动，而空气动力提升可由全电动推进系统提供。在一个方面，光伏阵列和高能量密度功率存储系统可以组合起来，为推进系统提供动力，使推进系统再生。三角翼形状可以提供足够大的表面积以适应非常大的圆形或椭圆形传输装置。通过不断地对蓄电系统充电，根据一些实施例的混合式飞艇可以在至少约85,000英尺的操作高度上保持高度数月甚至数年。混合型飞艇可以作为空中军事通信中继平台。

9. 发明申请

US20050224633A1 LOW-DRAG ROTOR/WING FLAP 有权
标题翻译： LOW-DRAG转子/翼片
公开(公告)号：US20050224633A1
公开(公告)日：2005-10-13
申请号：US10770764
申请日：2004-02-03
申请人： Edward Barocela , Charles Vaporean
发明人： Edward Barocela , Charles Vaporean
IPC分类号： B64C3/50 , B64C27/18 , B64C27/22 , B64C27/24 , B64C39/12
CPC分类号： B64C3/50 , B64C27/18 , B64C27/24 , B64C39/12 , Y02T50/14
摘要： Rotor/wing aircraft having a low-drag flap are disclosed. In one embodiment, a rotor/wing aircraft includes an elongated blade having a body portion and a flap portion. The body portion has first and second edges and includes a non-symmetric portion proximate the second edge. The flap portion is moveably coupled to the body portion proximate the second edge and is moveable between a rotary flight position and a forward flight position. In the rotary flight position, the flap portion is proximate at least part of the non-symmetric portion to form a second symmetric portion proximate the second edge. In the forward flight position, the flap portion extends away from the non-symmetric portion to form a tapered portion proximate the second edge.
摘要翻译：公开了具有低阻力翼片的转子/翼型飞机。在一个实施例中，转子/翼飞机包括具有主体部分和翼片部分的细长叶片。主体部分具有第一和第二边缘并且包括靠近第二边缘的非对称部分。翼片部分可移动地联接到靠近第二边缘的主体部分，并且可在旋转飞行位置和向前飞行位置之间移动。在旋转飞行位置，翼片部分靠近非对称部分的至少一部分，以形成靠近第二边缘的第二对称部分。在向前飞行位置，翼片部分远离非对称部分延伸以在第二边缘附近形成锥形部分。

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