Control surface for wing of aircraft and method for manufacturing such control surface
The invention relates to a control surface for a wing of an aircraft and a method for manufacturing the control surface. A thin, lightweight control surface is produced by inductive consolidation of a thermoplastic component. The control surface includes a front section co-consolidated with a rear s...
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Main Authors | , , |
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Format | Patent |
Language | Chinese English |
Published |
03.03.2023
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a control surface for a wing of an aircraft and a method for manufacturing the control surface. A thin, lightweight control surface is produced by inductive consolidation of a thermoplastic component. The control surface includes a front section co-consolidated with a rear section. The forward section includes a cover and the aft section includes a truss core covered by an outer skin.
本申请涉及用于飞机的机翼的操纵面及制造该操纵面的方法。一种薄的、轻质的操纵面通过热塑性部件的感应固结来制造。操纵面包括与后区段共固结的前区段。前区段包括覆盖件,并且后区段包括被外蒙皮覆盖的桁架芯体。 |
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Bibliography: | Application Number: CN202211019190 |