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1. 发明公开

EP1755945A2 LIFT AUGMENTATION SYSTEM 审中-公开
标题翻译：升降增补系统
公开(公告)号：EP1755945A2
公开(公告)日：2007-02-28
申请号：EP05733909.5
申请日：2005-04-07
申请人： Lee, John, R.
发明人： LEE, John, R. , LEE, Craig , EASTLAKE, Charles , LADESIC, James, G. , MAHR, Peter , PIERPONT, Peter, S. , ANDERSON, Richard, P.
IPC分类号： B64C3/54
CPC分类号： B64C3/54 , B64C3/56 , B64C3/58 , B64C11/001 , B64C23/072 , B64C39/04 , Y02T50/164
摘要： This invention relates generally to a lift augmentation system for an airframe. More particularly, the invention concerns the combination of extendable/retractable wing tips with an airframe for lift augmentation as well as wings that can pivot into a deployed position. Flexible surface elements may be rolled for storage and unrolled for deployment with at least one being on the suction surface of the wing and at least one being on the pressure surface of the wing.
摘要翻译：本发明总体上涉及用于机身的升力增大系统。更具体地说，本发明涉及可伸展/可伸缩翼梢与用于升力增强的机身的组合以及可枢转到展开位置的翼。柔性表面元件可以被卷起来存储和展开展开，其中至少一个位于机翼的吸力表面上并且至少一个位于机翼的压力表面上。

2. 发明授权

EP0973676B8 EXTENDABLE/RETRACTABLE AIRFOIL ASSEMBLY FOR FIXED WING AIRCRAFT 失效
标题翻译：用于固定翼飞机的可伸缩/可伸缩翼型组件
公开(公告)号：EP0973676B8
公开(公告)日：2005-08-24
申请号：EP98919740.5
申请日：1998-04-08
申请人： Lee, John, R.
发明人： Wagner, Fred A. III
IPC分类号： B64C3/54
CPC分类号： B64C3/54 , Y02T50/14
摘要： A retractable airfoil assembly (20) augments the wing surface area (28) of an aircraft (22) enabling it to fly without stalling at reduced speeds during takeoff and landing. The airfoil assembly includes flexible sails (42, 44) and a furling mast (24) for extending and retracting the sails. The furling mast includes a furling drum mounted for clockwise and counterclockwise rotation on a static tube (50). The flexible sail assembly also includes guide tracks (80) located along a leading edge (101) or tailing edge (40) of the wings. The tracks guide the flexible sails during extension and retraction. A drive cable (26) extends and retracts the sails (42, 44) along the guide tracks and maintains tension in the sails while they are extended.
摘要翻译：可缩回的翼型组件（20）增大了飞机（22）的机翼表面区域（28），使其能够在起飞和着陆期间以降低的速度飞行而不会失速。翼型组件包括用于延伸和收回帆的柔性帆（42,44）和收拢桅杆（24）。收拢的桅杆包括一个安装在静态管（50）上顺时针和逆时针旋转的收卷鼓。柔性帆组件还包括沿着机翼的前缘（101）或后缘（40）定位的导轨（80）。轨道在延伸和收回期间引导柔性帆。驱动缆索（26）沿着导轨延伸和缩回帆（42,44），并在帆延伸时保持帆中的张力。

3. 发明公开

EP0656139A1 AN INTERACTIVE COMPUTER AIDED NATURAL LEARNING METHOD AND APPARATUS 失效
标题翻译：一种交互式计算机辅助自然学习方法和装置
公开(公告)号：EP0656139A1
公开(公告)日：1995-06-07
申请号：EP93905890.0
申请日：1993-02-11
申请人： LEE, John, R.
发明人： LEE, John, R. , ALVENDIA, John
IPC分类号： G06Q50 , G09B3 , G09B5 , G09B7
CPC分类号： G09B5/065 , G09B5/14 , G09B7/04 , Y10S706/927
摘要： An educational method and system for executing the method, to improve the efficiency of individual learning by monitoring the student's progress and pacing the course material to the student's ability to comprehend and learn. This method and system also reduces the teacher's administrative and paperwork burden. Interactive multimedia technology is combined with unique courseware development to provide a flexible teaching tool and student monitoring system.
摘要翻译：一种执行该方法的教育方法和系统，通过监视学生的进度并将课程材料投放到学生的理解和学习能力来提高个人学习的效率。这种方法和系统也减少了教师的行政和文书工作负担。交互式多媒体技术与独特的课件开发相结合，提供灵活的教学工具和学生监控系统。

4. 发明授权

EP0656139B1 AN INTERACTIVE COMPUTER AIDED NATURAL LEARNING METHOD AND APPARATUS 失效
标题翻译：一种交互式计算机辅助自然学习方法和装置
公开(公告)号：EP0656139B1
公开(公告)日：1999-05-12
申请号：EP93905890.5
申请日：1993-02-11
申请人： LEE, John, R.
发明人： LEE, John, R. , ALVENDIA, John
IPC分类号： G09B3/00 , G09B5/14 , G09B7/04
CPC分类号： G09B5/065 , G09B5/14 , G09B7/04 , Y10S706/927

5. 发明公开

EP0656139A4 AN INTERACTIVE COMPUTER AIDED NATURAL LEARNING METHOD AND APPARATUS. 失效
标题翻译：交互式计算机部门自然学习过程和设备。
公开(公告)号：EP0656139A4
公开(公告)日：1995-11-22
申请号：EP93905890
申请日：1993-02-11
申请人： LEE JOHN R
发明人： LEE JOHN R , ALVENDIA JOHN
IPC分类号： G06Q50/00 , G09B3/00 , G09B5/06 , G09B5/14 , G09B7/04
CPC分类号： G09B5/065 , G09B5/14 , G09B7/04 , Y10S706/927

6. 发明公开

EP1487697A2 VARIABLE AREA WING AIRCRAFT AND METHOD 审中-公开
标题翻译：与可变表面和方法WINGS PLANE
公开(公告)号：EP1487697A2
公开(公告)日：2004-12-22
申请号：EP03716286.4
申请日：2003-03-06
申请人： Lee, John R.
发明人： Lee, John R.
IPC分类号： B64C3/38
CPC分类号： B64C3/54 , Y02T50/14
摘要： An STOL aircraft structure has a variable-attitude, variable-area wing in addition to a traditional airfoil. The variable wing has an angle of attack that varies from 0° to a predetermined angle far in excess of the stall angle. The variable wing area can be adjusted from 0% to 100% by a roller furling arrangement. The aircraft structure operates during takeoff by deploying the variable wing with an attitude exceeding the stall angle, applying thrust to the aircraft so that the variable wing generates reaction lift and the aircraft attains a predetermined altitude, and stowing the variable wing so that the traditional airfoil is the primary lifting surface. Those steps are reversed for landing.

7. 发明专利

IL178431D0 LIFT AUGMENTATION SYSTEM 未知
公开(公告)号：IL178431D0
公开(公告)日：2007-05-15
申请号：IL17843106
申请日：2006-10-03
申请人： LEE JOHN R
IPC分类号： B64C3/54 , B64C3/56 , B64C3/58 , B64C11/00 , B64C23/06 , B64C39/04

8. 发明专利

DE69830717T2 未知
公开(公告)号：DE69830717T2
公开(公告)日：2006-06-01
申请号：DE69830717
申请日：1998-04-08
申请人： LEE JOHN R
发明人： WAGNER III
IPC分类号： B64C3/54
摘要： A retractable airfoil assembly (20) augments the wing surface area (28) of an aircraft (22) enabling it to fly without stalling at reduced speeds during takeoff and landing. The airfoil assembly includes flexible sails (42, 44) and a furling mast (24) for extending and retracting the sails. The furling mast includes a furling drum mounted for clockwise and counterclockwise rotation on a static tube (50). The flexible sail assembly also includes guide tracks (80) located along a leading edge (101) or tailing edge (40) of the wings. The tracks guide the flexible sails during extension and retraction. A drive cable (26) extends and retracts the sails (42, 44) along the guide tracks and maintains tension in the sails while they are extended.

9. 发明专利

AU2003219998A1 VARIABLE AREA WING AIRCRAFT AND METHOD 未知
公开(公告)号：AU2003219998A1
公开(公告)日：2003-09-22
申请号：AU2003219998
申请日：2003-03-06
申请人： LEE JOHN R
发明人： LEE JOHN R
IPC分类号： B64C3/54

10. 发明专利

ES2131108T3 未知
公开(公告)号：ES2131108T3
公开(公告)日：1999-07-16
申请号：ES93905890
申请日：1993-02-11
申请人： LEE JOHN R
发明人： LEE JOHN R , ALVENDIA JOHN
IPC分类号： G06Q50/00 , G09B3/00 , G09B5/06 , G09B5/14 , G09B7/04

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