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...

Full description

Saved in:
Bibliographic Details
Main Authors MATZEN, MARK, ROLLO, ASHMAWI VAIL, MARCO JEFFREY LEE
Format Patent
LanguageChinese
English
Published 03.03.2023
Subjects
AEROPLANES
AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES
PERFORMING OPERATIONS
SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR
SHAPING OR JOINING OF PLASTICS
TRANSPORTING
WORKING OF PLASTICS
WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Online AccessGet full text

Cover

More Information
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。
Bibliography:Application Number: CN202211019190