Strain amplification structure and synthetic jet actuator

Patent metadata

Field	Value
Publication number	US-10153420-B2
Application number	US-201414569464-A
Country	US
Kind code	B2
Filing date	Dec 12, 2014
Priority date	Jun 15, 2012
Publication date	Dec 11, 2018
Grant date	Dec 11, 2018

Abstract

A strain amplification structure has a frame with a hexagonal structure incorporating a plurality of rigid beams that are connected to opposing end beams by a plurality of flexible joints. A piezoceramic actuator assembly is connected to the opposing end beams having a collar including an opening. A shaft providing an output is connected to the plurality of rigid beams with flexible joints and passes through the opening in the collar for non-interfering motion orthogonal to the actuator assembly.

First claim

What is claimed is:

1. A strain amplification structure comprising:
a frame having a hexagonal structure incorporating a plurality of rigid beams that are connected to opposing end beams by a plurality of flexible joints, the plurality of rigid beams comprising:
a first pair of actuation beams extending angularly from the end beams;
a second pair of actuation beams extending angularly from the end beams longitudinally separated from the first pair of actuation beams and parallel thereto;

a piezoceramic actuator assembly connected to the opposing end beams and having
a collar including an opening;
a pair of piezoceramic stacks each connected at an inner end to the collar and at an opposite end to a respective one of the end beams, said piezoceramic stacks intermediate the first pair of actuation beams and the second pair of actuation beams;

a shaft providing an output and connected to each of the plurality of rigid beams with flexible joints, said shaft passing through said opening;
attachment brackets supporting the end beams for resilient lateral movement;
a housing from which the attachment brackets are rigidly supported;
a piston attached to the shaft and received in a cavity in the housing, said cavity having an orifice,
wherein a first condition of the piezoceramic stacks places the end beams in a first relative lateral position with the first and second pair of actuation beams extending at a first angle from the end beams to place the shaft in a first longitudinal position and wherein a second condition of the piezoceramic stacks places the end beams in a second relative lateral position with the first and second pair of actuation beams extending at a second angle from the end beams to place the shaft in a second longitudinal position, a distance between said first and second longitudinal positions comprising an amplification of a second distance between the first and second lateral positions, and
whereby oscillation of the piezoceramic stacks between the first and second conditions creates a synthetic jet.

2. The strain amplification structure as defined in claim 1 wherein the flexible joints are flexible webs machined or etched between the end beams and actuation beams and the center shaft and actuation beams.

3. The strain amplification structure as defined in claim 1 wherein the amplification structure frame is fabricated from a material selected from the set of aluminum, beryllium, beryllium alloys, titanium, steel and carbon fiber reinforced plastic.

4. The strain amplification structure as defined in claim 1 wherein the piezoceramic actuator assembly is operable to reciprocate at a first frequency providing mechanical resonance of the shaft for increased amplification.

5. The strain amplification structure as defined in claim 1 wherein the piezoceramic actuator assembly is operable to reciprocate at a second frequency providing acoustic resonance of the piston, cavity and orifice.

6. The strain amplification structure as defined in claim 1 wherein the piezoceramic actuator assembly reciprocation occurs at a frequency to couple a mechanical resonance of the shaft and acoustic resonance of the piston, cavity and orifice for increased amplification.

7. A method for producing a synthetic jet comprising:
interconnecting a frame having a hexagonal structure incorporating a plurality of rigid beams to a pair of opposing laterally spaced flexing end beams with a plurality of flexible joints, the plurality of rigid beams comprising a first pair of actuation beams extending angularly from the end beams and a second pair of actuation beams extending angularly from the end beams, separated from the first pair of actuation beams and parallel thereto;
connecting a piezoceramic actuator assembly to the opposing end beams, said piezoceramic actuator assembly having
a collar including an opening,
a pair of piezoceramic stacks each connected at an inner end to the collar and at an opposite end to a respective one of the end beams, said piezoceramic stacks intermediate the first pair of actuation beams and the second pair of actuation beams;
inserting a shaft through the opening the collar, said shaft connected to each of the plurality of rigid beams with flexible joints;
supporting the end beams with attachment brackets for resilient lateral movement;
rigidly supporting the attachment brackets from a housing;
attaching a piston;
receiving the piston in a cavity in the housing, said cavity having an orifice;
oscillating the piezoceramic stacks between a first condition of the piezoceramic stacks placing the end beams in a first relative lateral position with the first and second pair of actuation beams extending at a first angle from the end beams to place the shaft in a first longitudinal position and a second condition of the piezoceramic stacks placing the end beams in a second relative lateral position with the first and second pair of actuation beams extending at a second angle from the end beams to place the shaft in a second longitudinal position, a distance between said first and second longitudinal positions comprising an amplification of a second distance between the first and second lateral positions, the oscillation of the piezoceramic stacks between the first and second conditions creating a synthetic jet.

8. The method as defined in claim 7 wherein reciprocation of the piezoceramic actuation assembly occurs at a first frequency to provide a mechanical resonance of the shaft for increased amplification.

9. The method as defined in claim 7 wherein reciprocation of the piezoceramic actuation assembly occurs at a second frequency for acoustic resonance of the piston, cavity and orifice.

10. The method as defined in claim 7 wherein reciprocation of the piezoceramic actuation assembly occurs at a frequency to couple a mechanical resonance of the shaft and acoustic resonance of the piston, cavity and orifice for increased amplification.

11. The method as defined in claim 7 further comprising machining flexible webs between the end beams and actuation beams and the center shaft and actuation beams as the flexible joints.

12. The method as defined in claim 7 further comprising etching flexible webs between the end beams and actuation beams and the center shaft and actuation beams as the flexible joints.

Assignees

• Boeing Co

Inventors

• Griffin Steven F
• Haar Shawn

Classifications

• B64C2230/06

  by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure · CPC title

• B64C2230/04

  by actively generating fluid flow · CPC title

• B64C2230/18

  by using small jets that make the fluid flow oscillate · CPC title

• Y10T29/42

  Piezoelectric device making · CPC title

• H01L41/25

  Electricity · mapped topic