
US Patent No: 5,094,412
Number of patents in Portfolio can not be more than 2000
Flaperon system for tilt rotor wings
Stats
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Mar 10, 1992
Issued date -
Oct 13, 1989
filing date -
07/417,811
serial no -
Expired
status
Importance
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Abstract
The present invention provides an aircraft wing (10) having a main portion (20) with a trailing edge (20b) and a movable flaperon (22) hingedly secured at the trailing edge. A movable flaperon seal (40) is hingedly attached at its leading edge to the trailing edge of the main portion of the wing. Interconnecting structure is provided between the main portion of the wing and the flaperon seal. Such structure is operable to pivot the seal flap such that the opening between the trailing edge of the main wing portion (20b) and the leading edge of said movable flap (22a) on the upper surface is selectively closed by the movable flap at predetermined angular positions of the movable flap.
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First Claim
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International Classification(s)
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- [Patents Count]
Cited Art
| Patent Info | (Count) | # Cites | Year |
|---|---|---|---|
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| 4,248,395 Airplane wing trailing-edge flap-mounting mechanism | 24 | 1978 | |
| 4,360,176 Wing leading edge slat | 42 | 1979 | |
| 4,471,927 Trailing edge flap assembly | 46 | 1981 | |
| 4,605,187 Wing flap mechanism | 27 | 1984 | |
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| 4,498,646 Wing for short take-off and landing aircraft | 39 | 1982 | |
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| 4,566,657 Span loaded flying wing control | 18 | 1980 | |
| 2009/0132,648 CONTENT DELIVERY AND GLOBAL TRAFFIC MANAGEMENT NETWORK SYSTEM | 2009 | ||