CONNECTING ASSEMBLY FOR AN AIRCRAFT WING SLAT
The invention relates to a wing (3) for an aircraft (1), comprising a main wing (5), a slat (7), and a connecting assembly (9) movably connecting the slat (7) to the main wing (5), such that the slat (7) is movable between a retracted position and at least one extended position, wherein the connecti...
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Main Authors | , |
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Format | Patent |
Language | Chinese English |
Published |
22.02.2022
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a wing (3) for an aircraft (1), comprising a main wing (5), a slat (7), and a connecting assembly (9) movably connecting the slat (7) to the main wing (5), such that the slat (7) is movable between a retracted position and at least one extended position, wherein the connecting assembly (9) comprises a slat track (11) and a roller bearing (13), wherein a front section (17) of the slat track (11) is mounted to the slat (7), wherein a rear section (19) and an intermediate section (21) of the slat track (11) are mounted to the main wing (5) via the roller bearing (13), wherein the roller bearing (13) comprises a guide rail (23) mounted to the main wing (5) and a first roller (27), wherein the first roller (27) is rotatably mounted to the rear section (19) of the slat track (11), wherein the first roller (27) engages a first engagement surface (33) formed by the guide rail (23), wherein the roller bearing (13) comprises a second roller (31), wherein the second roller (31) is rotatably moun |
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Bibliography: | Application Number: CN202080050283 |