Shock wave fluid pressure transducer element

Patent metadata

Field	Value
Publication number	US-12422289-B2
Application number	US-202217835151-A
Country	US
Kind code	B2
Filing date	Jun 8, 2022
Priority date	Jun 11, 2021
Publication date	Sep 23, 2025
Grant date	Sep 23, 2025

Abstract

A transducer element for the detection of a transverse transition pressure of a shock wave includes a body that extends along a longitudinal axis and includes a nose portion and a measurement portion disposed adjacent the nose portion, which tapers along the longitudinal axis from the measurement portion until a nose end. The transducer is arranged with its longitudinal axis extending parallel to the propagation direction of the shock wave, with the nose portion facing the shock wave. The measurement portion contains at least three pressure transducers arranged in the body with respective pressure-sensitive pressure receiving surfaces arranged parallel to the longitudinal axis. The three pressure transducers are spaced apart from each other at a distance along the longitudinal axis. The transducer element is configured for determining the velocity and the acceleration of the shock wave.

First claim

What is claimed is:

1. A transducer element for the detection of a transverse transition pressure of a shock wave acting along a pressure axis in a fluid, wherein the transverse transition pressure acts in a direction that is normal to the pressure axis, the transducer element comprising:
a body extending along a longitudinal axis that defines a central axis of symmetry of the body;
wherein the body defines a nose portion terminating in a nose vertex at one opposite end of the nose portion;
wherein the body defines a metallic measurement portion defining a rigid external wall extending parallel to the central axis of symmetry of the body without any protrusions in a direction normal to the central axis of symmetry of the body;
wherein the nose portion oppositely disposed from the nose vertex is disposed adjacent to the measurement portion and tapers along the longitudinal axis from the measurement portion to the nose vertex of the nose portion;
wherein for the detection of a transverse transition pressure of a shock wave in a fluid, the body is configured to be arrangeable with its longitudinal axis extending parallel to the expected propagation direction of the shock wave;
wherein for the detection of a transverse transition pressure of a shock wave in a fluid, the nose portion is configured to be arrangeable to face the shock wave;
at least three pressure transducers disposed in the measurement portion in alignment along the longitudinal axis;
wherein each of the at least three pressure transducers includes a pressure-sensitive pressure receiving surface;
wherein the pressure receiving surface of each of the at least three pressure transducers extends in a plane that is arranged parallel to the longitudinal axis; and
wherein the at least three pressure transducers are arranged spaced apart at a distance from each other along the longitudinal axis.

2. The transducer element according to the preceding claim 1 , wherein each of the at least three pressure transducers is configured to detect a respective transient pressure acting on the respective pressure receiving surface and to provide each respective transient pressure as a respective pressure signal.

3. The transducer element according to claim 1 , further comprising an electronic unit disposed in the measurement portion of the body; wherein each of the at least three pressure transducers is configured to detect a transient pressure acting on the respective pressure receiving surface; wherein each of the at least three pressure transducers is configured to detect an acceleration of the respective pressure transducer independently of the pressure that acts on the pressure receiving surface; wherein the electronic unit is configured to calculate a difference between the detected transient pressure and a fraction of the detected acceleration and provide that difference as a pressure signal.

4. The transducer element according to claim 2 , wherein the nose portion is designed to be substantially rotationally symmetrical with respect to the longitudinal axis and a length of the nose portion along the longitudinal axis is at least three times larger than the largest diameter of the nose portion when cut perpendicular to the longitudinal axis; and wherein the nose portion has the shape of a cone or wherein the nose portion has the shape of an ogive in cross-section when cut parallel to the longitudinal axis.

5. The transducer element according to claim 1 , wherein the measurement portion is substantially shaped like a cylinder along the longitudinal axis.

6. The transducer element according to claim 5 , wherein the body defines a flattened portion that the flattened portion is shaped like a chord in a cross-section perpendicular to the longitudinal axis; wherein the flattened portion extends in a planar manner at least partially along the longitudinal axis and spaced at a distance in a direction that is perpendicular from the longitudinal axis; wherein the respective pressure receiving surfaces of the at least three pressure transducers are arranged parallel to the flattened portion; and wherein the pressure receiving surfaces of the at least three pressure transducers are flush with the flattened portion, or wherein the pressure receiving surfaces of the at least three pressure transducers are moved backwards in the direction of the longitudinal axis relative to the flattened portion.

7. The transducer element according to claim 2 , wherein each of the at least three pressure transducers includes at least one piezoelectric pressure sensing element that is operatively connected to the pressure receiving surface.

8. The transducer element according to claim 7 , wherein each of the at least three pressure transducers includes a piezoelectric acceleration sensing element that is configured and disposed to detect an acceleration of the pressure transducer independently of the transient pressure acting on the respective pressure transducer surface.

9. The transducer element according to claim 1 , wherein the nose portion defines a shape that is streamlined so as to gradually compress a shock wave that reaches the nose portion as the shock wave moves along the longitudinal axis.

10. The transducer element according to claim 1 , wherein the body is made of a metal alloy.

11. The transducer element according to claim 1 , wherein each pressure-sensitive pressure receiving surface of each respective pressure transducer is coated by a flexible protective layer.

12. A transducer assembly comprising:
a transducer element, which includes a body extending along a longitudinal axis, the body defining a nose portion with a nose vertex at one opposite end of the nose portion, the body defining a measurement portion disposed adjacent the end of the nose portion opposite the nose vertex, three pressure transducers are disposed in the measurement portion and disposed spaced apart at a distance from each other along the longitudinal axis, each of the three pressure transducers includes a pressure-sensitive pressure receiving surface disposed parallel to the longitudinal axis, wherein each of the three pressure-sensitive pressure receiving surfaces is configured to detect a respective transient pressure, wherein the nose portion tapers along the longitudinal axis from the measurement portion to the vertex of the nose portion;
an acquisition unit; and
a cable electrically connecting the acquisition unit to the transducer element;
wherein each of the three pressure transducers is configured to generate a respective pressure signal from each of the respective detected transient pressures; and
wherein the acquisition unit is configured to compare the three respective pressure signals generated by the three respective pressure transducers.

13. The transducer assembly according to claim 12 , wherein the acquisition unit is configured to compare the three pressure signals;
wherein said acquisition unit is configured to calculate and provide a shock wave velocity by means of the temporal sequence of the three pressure signals;
wherein the acquisition unit is configured to calculate and provide a shock wave acceleration by means of the temporal sequence of the three pressure signals.

14. The transducer assembly according to claim 12 , wherein the nose portion defines a shape that is streamlined so as to gradually compress a shock wave that reaches the nose portion as the shock wave moves along the longitudinal axis.

15. The transducer element according to claim 12 , wherein each pressure-sensitive pressure receiving surface of each respective pressure transducer is coated by a flexible protective

Assignees

• Kistler Holding Ag

Inventors

• Weber David
• Frommenwiler Tobias
• Laffranchi Marco
• Wyss Andreas

Classifications

• G01F1/662

  Constructional details · CPC title

• G01H5/00

  Measuring propagation velocity of ultrasonic, sonic or infrasonic waves {, e.g. of pressure waves} · CPC title

• G01P15/00

  Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration · CPC title

• G01P3/00

  Measuring linear or angular speed; Measuring differences of linear or angular speeds (G01P5/00 - G01P11/00 take precedence; {direction and speed indication G01P13/045}; counting mechanisms G06M) · CPC title

• G01F1/667 Primary

  Arrangements of transducers for ultrasonic flowmeters; Circuits for operating ultrasonic flowmeters · CPC title