Patent · US Active

Aircraft or spacecraft fluidic oscillator device

US10647416B2 · kind B2 · utility

0Cited by

5References

23Claims

0Family size

Assignee

Airbus Defence and Space GmbH · DE

Inventors

Karin Bauer · Oberhaching, DE
Markus Blechschmidt · Birkenfeld, DE
Sebastian Schwarz · Unterhaching, DE
Peter Langenbacher · Munich, DE

Key dates

Filing date	Dec 21, 2016
Grant date	May 12, 2020
Priority date	—
Expiry date	Sep 3, 2038

Classification

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

Abstract

A fluidic oscillator device, in particular for a or in a flow control system for an aircraft or spacecraft, has a first and a second fluidic actuator, wherein each of the actuators has an inlet for supplying pressure and a first and a second outlet, from which an actuator flow can be discharged. The device further has a fluidic control for controlling an oscillating discharge of the actuator flow from the first and second outlet of the actuators, wherein the control has a connection portion which is arranged between the first actuator and the second actuator.

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