科技爱好与博览

　　

　　

　　

　　摘要

　　A leading edge (50) for an aircraft has a hard durometer elastomer tip (52).领先优势（ 50岁）的飞机有一个弹性硬durometer小费（ 52岁） 。 An elastomer panel (54) has a first end attached to the hard durometer elastomer tip (52) and has a plurality of reinforcing members capable of freely sliding inside the elastomer panel (54).一种弹性体面板（ 54岁）已经结束的第一个连接到硬盘durometer弹性小费（ 52岁） ，并有一个多元化的加强成员能够自由滑动内的弹性体面板（ 54 ） 。 A rigid block (58) is attached to a second end of the elastomer panel (54) and is attached to a structure (62) of the aircraft.僵硬的区块（ 58岁）是连接到第二个结束的弹性体面板（ 54岁）和附加到结构（ 62岁）的飞机。

　　Patent number : 6213433 专利号码： 6213433

　　Filing date : Mar 14, 2000 申报日期： 2000年3月14日

　　Issue date : Apr 10, 2001 发行日期： 01年四月10号

　　Inventors : Cynthia Ann Gruensfelder, Lawrence O. Brase, Jr. 发明人 ：蚕安Gruensfelder ，劳伦斯岛Brase ，小

　　Assignee : The Boeing Company 受让人 ：波音公司

　　1 。 An edge for a portion of an aircraft comprising:一种边缘的部分飞机，包括：

　　a hard durometer elastomer tip having first and second ends;硬弹性冰山durometer了第一和第二个目的;

　　a first elastomer panel having a first end attached to the first end of the hard durometer elastomer tip, a second end and a plurality of reinforcing members capable of freely sliding inside the first elastomer panel;第一小组有弹性的第一个连接到年底前结束的弹性硬durometer小费，第二个结束和一个多元化的加强成员能够自由滑动内第一橡胶板;

　　a second elastomer panel having a first end attached to the second end of the hard durometer elastomer tip and a second end;第二小组有弹性的第一个连接到年底的第二次结束的弹性硬durometer小费和第二个目的;

　　a first rigid block attached to the second end of the first elastomer panel and the portion of the aircraft;第一个刚性块重视第二次结束的第一小组和弹性体部分的飞机;

　　a second rigid block attached to the second end of the second elastomer panel and the portion of the aircraft; and第二个刚性块重视第二次结束的第二小组和弹性体的部分飞机和

　　a system within said portion of the aircraft for controllably altering the shape of the portion; and一个系统内说，部分飞机controllably改变形状的部分;和

　　wherein the portion has no gaps or crevices regardless of the shape which it is caused to assume.其中一部分没有漏洞或裂缝，不论形状它造成承担。

　　2. 2 。 The leading edge of claim 1, further including a blunting actuator connected to the hard durometer elastomer tip.前沿索赔1 ，进一步钝化，包括驱动器连接到硬盘durometer弹性小费。

　　3. 3 。 The leading edge of claim 1, further including a skeletal structure pivotally connected to the structure of the aircraft and supporting the blunting actuator.前沿索赔1 ，进一步包括骨骼结构至关重要连接结构的飞机，并支持钝化器。

　　4. 4 。 The leading edge of claim 3, further including a rotary actuator attached to the skeletal structure.前沿索赔3 ，进一步包括一个旋转驱动器连接到骨骼结构。

　　5. 5 。 The leading edge of claim 1, wherein the plurality of reinforcing members are permanently attached to the hard durometer elastomer tip.前沿索赔1 ，其中多数是加强成员永久性地附着在弹性硬durometer小费。

　　6. 6 。 The leading edge of claim 5, wherein the plurality of reinforcing members slide freely through the rigid block.前沿索赔5 ，其中多数成员加强自由滑动通过刚性块。

　　7. 7 。 The leading edge of claim 1, further including a second elastomer panel having a first end attached to a second side of the hard durometer elastomer tip and a second end attached to a second rigid block, the second rigid block attached to the structure of the aircraft.前沿索赔1 ，进一步包括第二小组有弹性的第一个连接到年底的第二方面的努力durometer弹性小费和第二个结束重视第二刚性块，第二个刚性块重视结构的飞机。

　　8. 8 。 The leading edge of claim 7, further including an actuator having a first end attached to the first elastomer panel and a second end attached to the second elastomer panel.前沿索赔7 ，进一步包括了驱动器的第一个结束重视弹性小组第一和第二个结束重视弹性的第二小组。

　　9. 9 。 An anti-icing edge for an aircraft comprising;抗冰边缘的飞机组成的;

　　a hard durometer elastomer tip having a first edge and a second edge;硬弹性冰山durometer了第一个优势，第二个边缘;

　　a first reinforced elastomer panel having a first edge attached to the first edge of the hard durometer elastomer tip;第一个小组加强了弹性体的第一个边缘重视第一边缘的弹性硬durometer小费;

　　a first rigid block attached to a structure of the aircraft, the first rigid block connected to a second edge of the first reinforced elastomer panel;第一个刚性块重视结构的飞机，第一个刚性块连接到第二个边缘的钢筋弹性第一小组;

　　a second reinforced elastomer panel having a first edge attached to the second edge of the hard durometer elastomer tip;第二个小组加强了弹性体的第一个边缘重视第二边缘的弹性硬durometer小费;

　　a second rigid block attached to the structure of the aircraft, the second rigid block connected to a second edge of the second reinforced elastomer panel; and第二个刚性块重视结构的飞机，第二块刚性连接到第二个边缘的第二个强化橡胶板;和

　　an actuator connected between the first reinforced elastomer panel and the second reinforced elastomer panel, the actuator operable for deflecting the first and second reinforced elastomer panels; and一个驱动器之间的连接钢筋弹性体的第一小组和第二小组增强弹性，可操作性的驱动器的偏转第一次和第二次强化橡胶板;和

　　wherein deflection of the first and second reinforced elastomer panels is adapted to crack an ice formation on at least one of the first and second reinforced elastomer panels to facilitate the removal of the ice formation therefrom.其中偏转第一次和第二次强化橡胶板适合冰裂缝的形成至少有第一次和第二次强化橡胶板，以方便清理冰由此形成。

　　10. 10 。 The anti-icing edge of claim 9, wherein the first reinforced elastomer panel includes a plurality of reinforcing members capable of sliding freely inside the first reinforced elastomer panel.抗冰边缘的索赔9日，其中第一钢筋弹性面板包含一个多元化的加强成员能够自由滑动内的钢筋弹性第一小组。

　　11. 11 。 The anti-icing edge of claim 9, wherein a plurality of reinforcing members are attached to the hard durometer elastomer tip.抗冰边缘的索赔9日，其中多数成员是相辅相成的重视硬durometer弹性小费。

　　12. 12 。 The anti-icing edge of claim 9, wherein the first reinforced elastomer panel includes a center rigid block attached to the actuator.抗冰边缘的索赔9日，其中第一钢筋弹性面板包含一个中心刚性块连接到驱动器。

　　13. 13 。 The anti-icing edge of claim 9, wherein the actuator has a retracted position and an extended position.抗冰边缘的索赔9 ，其中动了收回的立场和扩展的立场。

　　14. 14 。 The anti-icing edge of claim 13, wherein the first reinforced elastomer panel and the second reinforced elastomer panel have a gapless smooth curvilinear shape when the actuator is in the extended position.抗冰边缘的索赔13 ，其中第一个钢筋弹性小组和第二小组加强弹性的无缝平滑曲线形状时，驱动器是在延长的立场。

　　15. 15 。 The anti-icing edge of claim 9, further including a blunting actuator connected to the hard durometer elastomer tip.抗冰边缘的索赔9 ，进一步钝化，包括驱动器连接到硬盘durometer弹性小费。

　　16. 16 。 The anti-icing edge of claim 15, further including a skeletal structure pivotally attached to the structure of the aircraft, the skeletal structure holding the blunting actuator.抗冰边缘的索赔15 ，进一步包括骨骼结构至关重要重视结构的飞机，骨骼结构举行钝化器。

　　17. 17 。 A leading edge for an aircraft having a structure, the leading edge comprising:领先优势的飞机有一个结构，前沿包括：

　　a hard durometer elastomer tip having a first edge and a second edge;硬弹性冰山durometer了第一个优势，第二个边缘;

　　a first elastomer sheet having a first edge and a second edge, the first edge of the first elastomer sheet connected to the first edge of the hard durometer elastomer tip, the second edge of the first elastomer sheet connected to the structure, the first elastomer sheet connected to the hard durometer elastomer tip and the structure in a continuous manner without gaps, crevices, and discontinuities that cause turbulence and drag;第一个表有弹性的第一个优势，第二个优势，第一边缘的资产负债表第一弹性连接到第一个边缘的弹性硬durometer小费，第二边缘的资产负债表第一弹性连接结构，第一橡胶板连接到硬盘durometer小费和弹性体的结构连续无间隙的方式，裂缝，以及不连贯，造成动荡和阻力;

　　a plurality of first reinforcing members sliding freely inside the first elastomer sheet, the plurality of first reinforcing members having a first end attached to the hard durometer elastomer tip;多元化的成员首先加强内部自由滑动的第一橡胶板，多元化的成员首先加强了第一个结束重视弹性硬durometer小费;

　　a first rigid block attached to the structure of the aircraft, the first rigid block connected to a second edge of the first elastomer sheet and the plurality of first reinforcing members sliding freely inside the first rigid block;第一个刚性块重视结构的飞机，第一刚性块连接到第二个边缘的资产负债表第一弹性和多元化的成员首先加强内部自由滑动的第一刚性块;

　　a second elastomer sheet having a first edge and a second edge, the first edge of the second elastomer sheet connected to the second edge of the hard durometer elastomer tip, the second edge of the second elastomer sheet connected to the structure, the second elastomer sheet connected to the hard durometer elastomer tip and the structure in a continuous manner without gaps, crevices and discontinuities that cause turbulence and drag;第二个橡胶板有一个优势，第二个优势，第一边缘的第二个橡胶板连接到第二个边缘的弹性硬durometer小费，第二边缘的第二个橡胶板连接的结构，第二橡胶板连接到硬盘durometer小费和弹性体的结构连续无间隙的方式，裂缝和不连续性，造成动荡和阻力;

　　a plurality of second reinforcing members sliding freely inside the second elastomer sheet, the plurality or second reinforcing members having a first end attached to the hard durometer elastomer tip;多元化的第二个强化成员内部自由滑动的第二橡胶板，多元化或第二加强成员有一个结束重视弹性硬durometer小费;

　　a second rigid block attached to the structure of the aircraft, the second rigid block connected to a second edge of the second elastomer sheet and the plurality of second reinforcing members sliding freely inside the second rigid block;第二个刚性块重视结构的飞机，第二块刚性连接到第二个边缘的第二个橡胶资产负债表和多元化的第二个强化成员内部自由滑动的第二刚性块;

　　a skeletal structure pivotally attached to a structure of the aircraft; 1骨骼结构至关重要重视结构的飞机;

　　a blunting actuator attached to the skeletal structure and connected to the hard durometer tip; and 1钝化驱动器连接到骨骼结构和连接到硬盘durometer小费;和

　　a rotary actuator connected to the skeletal structure.旋转驱动器连接到骨骼结构。

　　18. 18 。 The leading edge of claim 17, further including an anti-icing actuator connected between the first elastomer sheet and the second elastomer sheet.前沿索赔17 ，进一步包括防冰器之间的连接弹性板第一和第二橡胶资产负债表。

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