Aircraft or spacecraft fluidic oscillator device
AssigneeAirbus Defence and Space GmbH
InventorsKarin Bauer, Markus Blechschmidt, Sebastian Schwarz, Peter Langenbacher
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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.
Claims23
An aircraft or Spacecraft fluidic oscillator device for or in a flow control system, the device comprising:
- a first fluidic actuator and an adjacent 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 is discharged;
- and 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 configured as a flat part which is arranged between the first actuator and the second actuator, wherein the control is devoid of a feedback line external to the connection portion.
Dependencies are inferred from the claim text.