公开(公告)号：EP4509842A1

公开(公告)日：2025-02-19

申请号：EP24194673.0

申请日：2024-08-14

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： SCHWIE, Chester M. ,  PITERA, Rudy L.

IPC: G01P5/165 ,  B64D43/02 ,  G01P13/02

Abstract: An air-data probe component includes an additively manufactured inner member (102). The inner member includes integrally formed, monolithic structures including a mandrel bulkhead (104) defining a plurality of pneumatic chambers (106, 108, 110, 112, 114) therein in fluid communication with an outer surface (116) of the mandrel bulkhead through respective pressure ports, and a plurality of pneumatic tubes (120, 122, 124, 126, 128) extending aft of the mandrel bulkhead along a probe axis, each in fluid communication with a respective one of the plurality of pneumatic chambers. An outer cover tip (144) can be engaged about the mandrel bulkhead with a plurality of bores (146) therethrough for fluid communication of outside air pressure into the plurality of pneumatic tubes through the outer cover tip. A forward surface of the outer cover tip can be flush, conformal, and continuous with an aerodynamic outer surface of an aircraft.