Aircraft wing structure profiled suspension pylon
According to the invention, the suspension pylon ( 3 ) comprises a fairing for reducing the local loss in lift ( 8 ) and its maximum-width section ( 7 ) is located at the front of the concave and set-back rear part ( 4 R) of the pressure face ( 4 ) of the wing structure ( 1 ). The fairing for reduci...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | According to the invention, the suspension pylon (
3
) comprises a fairing for reducing the local loss in lift (
8
) and its maximum-width section (
7
) is located at the front of the concave and set-back rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
). The fairing for reducing the local loss in lift (
8
):
is housed, at least over most of its height, in the concavity of said rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
), and widens laterally toward the rear; and
comprises a projecting rear part (
12
) that tapers toward the rear and ends in an aerodynamic trailing edge (
16
) the length of which is very long by comparison with said maximum width of the fairing. |
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