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1. 发明授权

US08870125B2 Trailing edge split flap with pneumatic actuation 有权
标题翻译：具有气动启动功能的后缘分离式皮瓣
公开(公告)号：US08870125B2
公开(公告)日：2014-10-28
申请号：US13187634
申请日：2011-07-21
申请人： Michael A. Balzer , Gregory M. Santini , Michael K. Klein
发明人： Michael A. Balzer , Gregory M. Santini , Michael K. Klein
IPC分类号： B64C3/50 , B64C9/16
CPC分类号： B64C9/16 , B64C3/46 , Y02T50/14 , Y02T50/32 , Y02T50/44
摘要： A system for pneumatically actuating a split flap hingedly mounted near or at a trailing edge of an airfoil. The system includes a bladder system disposed between the split flap and the upper surface of the airfoil. The split flap is a small-chord (usually 1-3% of total wing chord) long-span lower panel which separates from the airfoil trailing edge by means of a hinge or a flexible lower skin. Deployment of the split flap is actuated pneumatically by the inflatable bladder system. The split flap may exist at a fixed wing trailing edge, a moving flap trailing edge, or an empennage trailing edge. The pneumatic bladder provides distributed force to extend and retract the split flap. This pneumatic approach eliminates extra drag, reduces cost and weight, and lessens flutter concerns.
摘要翻译：一种用于气动地致动分开的翼片的系统，其铰接地安装在翼型件的后缘附近或其后缘。该系统包括设置在分裂翼片和翼型件的上表面之间的气囊系统。襟翼是一个小和弦（通常是总翼弦的1-3％）长跨度下面板，通过铰链或柔性下皮肤与翼型后缘分离。通过可充气膀胱系统气动地驱动分裂瓣的部署。分裂瓣可以存在于固定的翼缘后缘，移动的翼片后缘或尾翼的后缘。气动气囊提供分布的力以延伸和缩回分裂瓣。这种气动方式消除了额外的阻力，降低了成本和重量，并减轻了颤抖的担忧。

2. 发明授权

US08844879B2 Wing variable camber trailing edge tip 有权
标题翻译：翼可变外倾末端
公开(公告)号：US08844879B2
公开(公告)日：2014-09-30
申请号：US13323524
申请日：2011-12-12
申请人： Gregory M. Santini
发明人： Gregory M. Santini
IPC分类号： B64C3/44
CPC分类号： B64C3/48 , B64C2003/147 , B64C2003/445 , Y02T50/12 , Y02T50/14
摘要： A flexible tip for integration in a wing trailing edge employs a wing structure rear spar. A flexible upper skin is attached at a forward boundary to the spar and a rigid lower skin is interconnected to the flexible upper skin at a rigid tail piece. At least one actuation link is attached to the rigid tail piece and has a hinge at a forward edge of the rigid lower skin. At least one positioning slider is attached to the hinge which is movable from a neutral position to a first extended position urging the hinge aft for rotation of the rigid lower skin upward and flexing of the flexible upper skin in an upward camber and to a second retracted position urging the hinge forward for rotation of the rigid lower skin downward and flexing of the flexible upper skin in a downward camber.
摘要翻译：用于集成在翼缘后缘中的柔性尖端采用翼结构后翼梁。弹性上皮附着在翼梁的前部边界处，并且刚性的下部皮肤以刚性的尾部片连接到柔性上皮肤。至少一个致动连杆附接到刚性尾部件并且在刚性下部皮肤的前边缘处具有铰链。至少一个定位滑块附接到铰链，该铰链可从中立位置移动到第一延伸位置，以推动铰链后部，以使刚性下部皮肤向上旋转，并且柔性上皮肤在向上弯曲中弯曲并且第二缩回向前推动铰链以使刚性下部皮肤向下旋转并使柔性上皮在向下弯曲中弯曲。

3. 发明申请

US20130146717A1 WING VARIABLE CAMBER TRAILING EDGE TIP 有权
公开(公告)号：US20130146717A1
公开(公告)日：2013-06-13
申请号：US13323524
申请日：2011-12-12
申请人： Gregory M. Santini
发明人： Gregory M. Santini
IPC分类号： B64C3/44
CPC分类号： B64C3/48 , B64C2003/147 , B64C2003/445 , Y02T50/12 , Y02T50/14
摘要： A flexible tip for integration in a wing trailing edge employs a wing structure rear spar. A flexible upper skin is attached at a forward boundary to the spar and a rigid lower skin is interconnected to the flexible upper skin at a rigid tail piece. At least one actuation link is attached to the rigid tail piece and has a hinge at a forward edge of the rigid lower skin. At least one positioning slider is attached to the hinge which is movable from a neutral position to a first extended position urging the hinge aft for rotation of the rigid lower skin upward and flexing of the flexible upper skin in an upward camber and to a second retracted position urging the hinge forward for rotation of the rigid lower skin downward and flexing of the flexible upper skin in a downward camber.
摘要翻译：用于集成在翼缘后缘中的柔性尖端采用翼结构后翼梁。弹性上皮附着在翼梁的前部边界处，并且刚性的下部皮肤以刚性的尾部片连接到柔性上皮肤。至少一个致动连杆附接到刚性尾部件并且在刚性下部皮肤的前边缘处具有铰链。至少一个定位滑块附接到铰链，该铰链可从中立位置移动到第一延伸位置，以推动铰链后部，以使刚性下部皮肤向上旋转，并且柔性上皮肤在向上弯曲中弯曲并且第二缩回向前推动铰链以使刚性下部皮肤向下旋转并使柔性上皮在向下弯曲中弯曲。

4. 发明申请

US20130020444A1 Trailing Edge Split Flap with Pneumatic Actuation 有权
标题翻译：带气动启动的后缘分流板
公开(公告)号：US20130020444A1
公开(公告)日：2013-01-24
申请号：US13187634
申请日：2011-07-21
申请人： Michael A. Balzer , Gregory M. Santini , Michael K. Klein
发明人： Michael A. Balzer , Gregory M. Santini , Michael K. Klein
IPC分类号： B64C3/50 , B64C13/36
CPC分类号： B64C9/16 , B64C3/46 , Y02T50/14 , Y02T50/32 , Y02T50/44
摘要： A system for pneumatically actuating a split flap hingedly mounted near or at a trailing edge of an airfoil. The system includes a bladder system disposed between the split flap and the upper surface of the airfoil. The split flap is a small-chord (usually 1-3% of total wing chord) long-span lower panel which separates from the airfoil trailing edge by means of a hinge or a flexible lower skin. Deployment of the split flap is actuated pneumatically by the inflatable bladder system. The split flap may exist at a fixed wing trailing edge, a moving flap trailing edge, or an empennage trailing edge. The pneumatic bladder provides distributed force to extend and retract the split flap. This pneumatic approach eliminates extra drag, reduces cost and weight, and lessens flutter concerns.
摘要翻译：一种用于气动地致动分开的翼片的系统，其铰接地安装在翼型件的后缘附近或其后缘。该系统包括设置在分裂翼片和翼型件的上表面之间的气囊系统。襟翼是一个小和弦（通常是总翼弦的1-3％）长跨度下面板，通过铰链或柔性下皮肤与翼型后缘分离。通过可充气膀胱系统气动地驱动分裂瓣的部署。分裂瓣可以存在于固定的翼缘后缘，移动的翼片后缘或尾翼的后缘。气动气囊提供分布的力以延伸和缩回分裂瓣。这种气动方式消除了额外的阻力，降低了成本和重量，并减轻了颤抖的担忧。

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