IP Library › Granted Patent US 9,654,862
Granted Patent B2
US 9,654,862 · App. 14/014,139 · Granted May 16, 2017

Acoustic element

Inventor: Lars Strömbäck (Linköping, SE)
H04R1/22F04D29/305F04D33/00H04R23/00F05D2270/62
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Quick Facts
Patent No.
US 9,654,862
App. No.
14/014,139
Granted
May 16, 2017
Kind
B2
Abstract

A combined fan and loudspeaker element, comprising a motor driven rotor provided with wings or blades, wherein the wings or blades are adjustable in pitch resulting together with a rotation of the rotor in an air transport flow, said wings or blades having superimposed thereon a sound-pitch modulation corresponding to a desired sound-pitch with the rotation of the rotor.

Claims (16)

1. A combined fan and loudspeaker clement, comprising a motor driven rotor provided with wings or blades, wherein the wings or blades are adjustable in pitch resulting together with a rotation of the rotor air transport flow through the rotor and the blades, said wings or blades having superimposed thereon a sound-pitch modulation corresponding to a desired sound-signal, said element further comprising a microphone for providing feedback to minimize or inhibit sound from the element.

2. The element according to claim 1 , wherein permanent magnets are arranged on or integrated with blades or wings, and a fixed coil or coils are arranged for influencing the magnets for pivoting the wings or blades.

3. The element according to claim 2 , wherein the wings have integrated coils.

4. The element according to claim 1 , further comprising a piezo element for altering of a pitch of the wings or blades.

5. The element according to claim 1 , wherein each wing or blade has a pivot axis and a balance centre for a pressure with which said wing or blade press against the air, said balance centre lying behind the pivot axis of the element in a movement direction of the wing or blade when the rotor is rotated so that an increasing pitch requires an increasing adjustment force to enable a precise pitch control.

6. The element according to claim 1 , further comprising a flywheel or active speed control for compensating load dependent speed variations caused by signal modulated wing angles.

7. The element according to claim 1 , wherein the wing pitch is controlled with active feedback.

8. The element according to claim 1 , comprising a circular rotor provided with one or several wings.

9. The element according to claim 5 , comprising a circular rotor provided with one or several wings.

10. The element according to claim 1 , further comprising a first sensor or control for controlling a fan-pitch value, and a second sensor or control for controlling modulation around said fan-pitch value, the first sensor or control corresponding to air volume or power, and the second sensor or control corresponding to the sound that is sensed or generated.

11. The element according to claim 1 , wherein the wings or blades pitch is set at fabrication of the rotor.

12. The element according to claim 1 , wherein the wings or blades pitch modulation is achieved by a modulation of the shape of the wings or blades of the rotor.

13. The element according to claim 1 , wherein the wings or the blades have a pivot axle and a balance centre for a pressure with which said wings press against the air, said balance centre lying in front of the pivot axle in the movement direction of rotation so that with the pitch angle varying centrifugal forces on the wings are compensated.

14. The element according to claim 1 , wherein a pivoting center for the sound pitch is located in front of a symmetry line or a balance point of a wing area so that a rear area of the wing becomes larger and thereby provides increasing resistance against increasing pitch so that improved linearity is obtained for pressure and air transport as a response to a controlling signal.

15. The element according to claim 1 , wherein the sound pitch is modulated to reduce the sound from the element.

16. The element according to claim 1 , wherein the microphone comprises an external microphone.

Continuity (2)
Continuation In Part 11568179
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