Hydrophones and similar devices

• US 4,928,263 A
• Filed: 02/10/1989
• Issued: 05/22/1990
• Est. Priority Date: 12/19/1988
• Status: Expired due to Term

• Current Assignee: Hermes Electronics Incorporated
• Original Assignee: Hermes Electronics Limited
• Inventors: Dunn, Robert G., Armstrong, Bruce A.
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): ELDRED, JOHN W
• Application Number:
  US07/308,512
• Time in Patent Office: 466 Days
• Field of Search: 367/157, 367/159, 367/165, 367/173, 367/179, 367/180, 367/118, 367/162, 310/329, 310/337, 310/800, 33/308, 33/365, 33/366, 33/391, 33/397
• US Class Current: 367/118
• CPC Class Codes: G01S 3/801 Details G01S3/82, G01S3/84, G01S3/86 take precedence
• CPC Class Codes: G01V 1/184 Multi-component geophones
• CPC Class Codes: G01V 1/189 Combinations of different types of receiving elements
• CPC Class Codes: G10K 11/006 Transducer mounting in underwater equipment, e.g. sonobuoys

Abstract

An accelerometer-based direction finding and ranging transducer such as a hydrophone uses piezoelectric ceramic as the active material. Orthogonally arranged accelerometers share an inertial mass and resonance control system and the accelerometers together with a pressure hydrophone and electronics are all housed within one pressure vessel.

Claims

1. A direction finding, motion-sensitive transducer, comprising:

(a) an inertial mass;

(b) means defining a mounting base;

(c) resilient means interconnecting said inertial mass with said mounting base, said inertial mass extending along a symmetry axis when at rest in a non-accelerated condition, and said resilient means being adapted to permit the inertial mass to wobble relative to the mounting base in radial directions relative to said symmetry axis in response to and in accordance with the direction of components of acceleration of the mounting base which are transverse to the symmetry axis;

(d) a plurality of sensing elements arranged to respond to the wobbling motion of the inertial mass relative to the mounting base, with said sensing elements being located so as to define multiple directional channels which are adapted to produce outputs dependent on the directions of said acceleration components, and wherein

(e) said inertial mass, said resilient means and said sensing elements together define resonant systems, and damping means common to said inertial mass, said resilient means, said sensing elements and the multiple directional channels defined by the latter for controlling the resonance of said systems.

2. The apparatus of claim 1 wherein said sensing elements comprise stress-sensitive electrical circuit elements positioned to provide orthogonally arranged directional channels and adapted to respond to the radially directed wobbling oscillations of said inertial mass relative to the mounting base.

3. The apparatus of claim 2 wherein said resilient means interconnecting the inertial mass with said mounting base comprises a neck portion centered with and extending along said symmetry axis and having a length and thickness selected to keep the fundamental resonance frequency of the inertial mass along said symmetry axis above the highest acoustic frequency to be sensed while at the same time said neck portion is sufficiently compliant so as to permit the inertial mass to wobble relative to said mounting base in said radial directions.

4. The apparatus of claim 1 wherein said sensing elements are disposed in equally spaced relation around the symmetry axis and the sensing elements each include a piezo-electric layer secured to a backing which is capable of flexing as said inertial mass wobbles relative to the mounting base.

5. The apparatus of claim 3 wherein said sensing elements are disposed in equally spaced relation around the symmetry axis and mechanical coupling means for effecting flexure of said sensing elements as said inertial mass wobbles relative to said mounting base.

6. The apparatus of claim 3 wherein said sensing elements are disposed in equally spaced relation around the symmetry axis and means for effecting flexure of said sensing elements as said inertial mass wobbles relative to said mounting base, comprising plural means on said inertial mass radially displaced upwardly from the symmetry axis and each contacting a respective one of the sensing elements so that the motions of the inertial mass relative to the mounting base are transmitted to the sensing elements, and the sensing elements having resilience enabling same to flex or deflect in response to said motions.

7. The apparatus of claim 6 wherein the sensing element each include a piezo-electric layer secured to a backing which is capable of flexing as said inertial mass pivots relative to the mounting base.

8. The apparatus of claim 7 wherein both the piezo-electric layer and the backing are disc-shaped, the backing for each sensing element being supported over a pocket or recess in the mounting base to permit the flexing thereof, and said means contacting the respective sensing elements including screw-threaded adjustment means to permit the resonance frequencies of the systems defined by the inertial mass, resilient means and the respective sensing elements to be adjusted and make equal.

9. The apparatus of claim 2 wherein said sensing elements are disposed in equally spaced relation around the symmetry axis, said resilient means comprising a diaphragm-like structure to which both the inertial mass and said sensing elements are affixed so that the wobbling motion of said inertial mass effects flexure and stressing of the sensing elements.

10. The apparatus of claim 2 wherein said sensing elements comprise two orthogonally arranged pairs with the sensors of each pair being of opposite polarity.

11. The apparatus of claim 4, wherein said sensing elements comprise two orthogonally arranged pairs with the sensors of each pair being of opposite polarity and electrically connected in parallel.

12. The apparatus of claim 6 wherein said sensing elements comprise two orthogonally arranged pairs with the sensors of each pair being of opposite polarity and electrically connected in parallel.

13. The apparatus according to claim 1 wherein said damping means for controlling the resonance of said systems includes a canister surrounding said inertial mass but spaced therefrom the canister being fixed rigidly relative to said mounting base, and a fluid of sufficient viscosity as to effect damping of the wobbling motion being located in the space between the canister and the inertial mass.

14. The apparatus according to claim 1 wherein said damping means for controlling the resonance of said systems includes a canister surrounding said inertial mass but spaced therefrom the canister being fixed rigidly relative to said mounting base, and a fluid of sufficient viscosity as to effect damping of the wobbling motion being located in the space between the canister and the inertial mass, and temperature responsive means for changing the amount and hence the level of said fluid in said canister in response to temperature changes thereby to compensate for changes in damping effect due to temperature related viscosity changes in said fluid.

15. The apparatus of claim 2 wherein said damping means for controlling the resonance of said systems includes a canister surrounding said inertial mass but spaced therefrom, the canister being fixed rigidly relative to said mounting base, and a fluid of sufficient viscosity as to effect damping of the wobbling motion being located in the space between the canister and the inertial mass;

16. The apparatus according to claim 6 wherein said damping means for controlling the resonance of said systems includes a canister surrounding said inertial mass but spaced therefrom, the canister being fixed rigidly relative to said mounting base, and a fluid of sufficient viscosity so as to effect damping of the wobbling motion being located in the space between the canister and the inertial mass, and a resilient ring in compression between said canister and the inertial mass providing a force tending to urge the inertial mass into a concentric relationship with said canister.

17. The apparatus according to claim 1 including pressure vessel means encompassing and enclosing the inertial mass, mounting base, resilient means and sensing elements and preventing ingress of water into the interior of the pressure vessel when in use.

18. The apparatus according to claim 6 including pressure vessel means encompassing and enclosing the inertial mass, mounting base, resilient means and sensing elements and preventing ingress of water into the interior of the pressure vessel when in use, said pressure vessel including a pair of opposed cup-shaped seamless, bodies fixed and sealed to said mounting base.

19. The apparatus according to claim 13 including pressure vessel means encompassing and enclosing the inertial mass, mounting base, resilient means and sensing elements and preventing ingress of water into the interior of the pressure vessel when in use, said pressure vessel including a pair of opposed cup-shaped seamless bodies fixed and sealed to said mounting base, one of said seamless bodies encompassing the inertial mass, the sensing elements and the damping means, and the other of said seamless bodies enclosing a region for the mounting of electronic components.

20. The apparatus according to claim 6 including pressure vessel means encompassing and enclosing the inertial mass, mounting base, resilient means and sensing elements and preventing ingress of water into the interior of the pressure vessel when in use, said pressure vessel including a pair of opposed cup-shaped seamless bodies fixed and sealed to said mounting base, one of said seamless bodies encompassing the inertial mass, the sensing elements and the damping means, and the other of said seamless bodies enclosing a region for the mounting of electronic components, wherein said opposed cup-like seamless bodies have mouth portions which sealingly embrace and engage the mounting base, said seamless bodies being constructed such that any resonance frequencies of these bodies are higher than the highest acoustic frequency to be analyzed.

21. The apparatus according to claim 20 wherein one of said seamless bodies includes a pressure sensing element thereon to detect and provide a pressure-dependent output.

22. The apparatus according to claim 2 wherein an all-metal thermal pathway from each of said sensing elements to an exterior portion of the apparatus is provided thereby to reduce thermally induced output signals therefrom.

23. The apparatus according to claim 2 wherein the polarity of said sensing elements and electrical connections therebetween are such as to protect said elements against thermally induced voltages.