公开(公告)号：US11808667B2

公开(公告)日：2023-11-07

申请号：US17532305

申请日：2021-11-22

Applicant: Dalian University of Technology

Inventor： Wei Qian ,  Ling Xiao ,  Xing Li ,  Shaojie Ge ,  Weizhe Feng ,  Xinyu Ai

IPC: G01M9/08

CPC classification number: G01M9/08

Abstract: A wing model for static aeroelasticity wind tunnel test belongs to the technical field of aeroelasticity tests. In the wing model, the model steel joint and the spar frame are connected with the composite material skin. The piezometer wing ribs are arranged among the spar frame and the plurality of supporting wing ribs. The embedded piezometer tubes are arranged in the piezometer wing ribs, the lightweight filling foam is arranged among the spar frame and the plurality of supporting wing ribs. An outer surface of a frame segment formed by the lightweight filling foam, the plurality of supporting wing ribs, the piezometer wing ribs and the spar frame is covered with the composite material skin. The frame segment is assembled on the model steel joint to form the wing model for the static aeroelasticity wind tunnel test.