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公开(公告)号：US06655633B1
公开(公告)日：2003-12-02
申请号：US09489041
申请日：2000-01-21
IPC分类号： B64C320
CPC分类号： B29D24/004 , B29C53/60 , B29C53/821 , B29C53/822 , B29C70/32 , B29L2031/3076 , B64C1/06 , B64C2001/0072 , Y02T50/43
摘要： Integrally stiffened and formed, load carrying structures comprising a plurality of elongated thin-walled tubes placed co-extensively in a complementary side-by-side fashion which together form a hollow structure having a desired external contour. Integral skins forming the external and internal surfaces of the structure cooperatively therewith. The structure can be formed with an underlying internal support member spanning the interior of the load carrying structure, thereby connecting opposite sides of the structure together. Also, each of the tubes are wound with fibers in controlled orientations generally paralleling the direction of the loads applied to the tubes to optimize the strength to weight ratio of the tubes.
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公开(公告)号：US06419188B1
公开(公告)日：2002-07-16
申请号：US09621317
申请日：2000-07-20
IPC分类号： B64D2502
CPC分类号： B64D43/00
摘要： The present invention includes an instrument panel that is adapted to stand over the lap of a pilot within a cockpit of an aircraft to make more efficient use of the limited space within the cockpit. The panel houses at least a portion of the instruments that are installed in the cockpit to fly the aircraft. More efficiently use of the space within the cockpit reduces the size and weight of the cockpit. Moreover, reducing the weight of the cockpit allows the cockpit with the canopy to be ejected from the aircraft rather than just the pilot seat. The cockpit enclosed by the canopy ejects the pilot faster and protects the pilot during and after the ejection. The ejection is faster because there is no need to remove the canopy before ejecting the seat. The pilot is further protected because the canopy protects the pilot from wind impact and harsh atmospheric conditions at high altitude.
摘要翻译： 本发明包括一种仪表板，其适于在飞机的驾驶舱内的飞行员的膝盖上站立，以更有效地利用驾驶舱内的有限空间。 该小组容纳至少一部分安装在驾驶舱中用于飞行飞机的仪器。 更有效地利用驾驶舱内的空间减少了驾驶舱的大小和重量。 此外，减轻驾驶舱的重量允许驾驶舱与机盖弹出而不是飞行员座椅。 由顶盖包围的驾驶舱更快地弹出飞行员，并在弹出期间和之后保护飞行员。 喷射更快，因为在弹出座椅之前不需要移除顶盖。 飞行员得到进一步的保护，因为机盖可以保护飞行员免受高风暴的大风和大气条件的影响。
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公开(公告)号：US07063763B2
公开(公告)日：2006-06-20
申请号：US10366606
申请日：2003-02-13
CPC分类号： B29D24/004 , B29C53/60 , B29C53/821 , B29C53/822 , B29C70/32 , B29L2031/3076 , B64C1/06 , B64C2001/0072 , Y02T50/43
摘要： Integrally stiffened and formed, load carrying structures comprising a plurality of elongated thin-walled tubes placed co-extensively in a complementary side-by-side fashion which together form a hollow structure having a desired external contour. Integral skins forming the external and internal surfaces of the structure cooperatively therewith. The structure can be formed with an underlying internal support member spanning the interior of the load carrying structure, thereby connecting opposite sides of the structure together. Also, each of the tubes are wound with fibers in controlled orientations generally paralleling the direction of the loads applied to the tubes to optimize the strength to weight ratio of the tubes.
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