Patent · US Active

Flow body for a vehicle and method for manufacturing a flow body

US11866172B2 · kind B2 · utility

0Cited by

3References

9Claims

0Family size

Assignee

Airbus Defence and Space GmbH · DE

Inventors

Florian Mayer · Freiberg am Neckar, DE
Alexander Kolb · Schwanau, DE
Simone Mancini · Schweinhub, DE

Key dates

Filing date	Oct 27, 2021
Grant date	Jan 9, 2024
Priority date	—
Expiry date	Jan 9, 2042

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY02T50/10
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

A flow body for an aircraft includes a recess in a surface of the flow body, a first structural component with a porous material and may also include a second structural component with a porous material. The recess includes a front recess region and a rear recess region. The first structural component is arranged in, or on, the front recess region and the second structural component may be arranged in, or on, the rear recess region. An aircraft having the flow body, a weapons system having the flow body and a method for manufacturing a flow body for a vehicle are also described.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.