Method for monitoring the state of a composite structure and pressurized fluid reservoir having a device performing said method

• US 6,675,659 B1
• Filed: 09/29/1999
• Issued: 01/13/2004
• Est. Priority Date: 09/29/1998
• Status: Expired due to Term

• Current Assignee: Aerospatiale Matra
• Original Assignee: Aerospatiale Matra
• Inventors: Souvannavong, Frédéric, Angoulvant, Manuel, Louis-Calixte, Bruno
• Primary Examiner(s): Lefkowitz, Edward
• Assistant Examiner(s): DAVIS, OCTAVIA L
• Application Number:
  US09/408,457
• Time in Patent Office: 1,567 Days
• Field of Search: 737/60, 738/66, 737/74, 737/75, 737/89, 738/00, 735/88, 735/94, 735/79, 735/87, 737/68, 737/69, 737/86, 156/382, 428/195, 428/114, 428/461, 385/11, 385/12, 166/369, 166/259, 166/251, 702/36, 310/340, 310/334, 340/541
• US Class Current: 73/760
• CPC Class Codes: G01B 21/32 for measuring the deformation in a solid
• CPC Class Codes: G01B 7/16 for measuring the deformation in a solid, e.g. by resistance strain gauge

Abstract

To monitor the operating state of a composite structure formed from at least two different materials and subject to a uniform force or load over its entire surface, the deformation at the interface between the two materials is measured. A comparison with a reference quantity of the structure, normally produced by the force applied thereto, indicates the operating state. When the composite structure forms the wall (14) of a reservoir (10), monitoring takes place in an instrumentation box (30) joined to the reservoir. When a critical threshold is exceeded, an alarm indicator (32) is triggered on the box (30).

Claims

1. A method for monitoring in situ over a period of time a composite structure having a given total surface and comprising at least a first part including at least two layers formed from different materials and adjacent one another along a given interface, said structure being subject to a uniform pressure applied over said total surface, said method comprising the following stages:

measuring in situ at a time t a deformation or stress level of said structure, produced by said uniform pressure by a monitoring means positioned at said interface; and

comparing the measured deformation or stress level with a reference deformation or stress level of said structure at a time t₀, produced by said uniform pressure.

2. The method according to claim 1, further comprising a stage of determining the reference deformation or stress level by measuring a deformation or stress level of a second part of the structure formed from only one of said layers.

3. The method according to claim 1, wherein said comparison stage comprises comparing the measured deformation or stress level and the reference deformation or stress level with a reference curve giving a normal evolution of the deformation or stress level of the first part of the structure as a function of the force applied thereto.

4. The method according to claim 3, further comprising a stage of obtaining the reference curve by measuring beforehand an evolution of the deformation or stress level of said first part of the structure, when said structure is new, as a function of the force applied to said new structure.

5. The method according to claim 3, further comprising a stage of modeling the reference curve by a second degree equation.

6. The method according to claim 2, wherein said stage of determining the reference deformation or stress level by measuring the deformation or stress level of the second part of the structure is performed by installing at least one transducer on said second part.

7. The method according to claim 1, wherein said in situ measurement stage is performed by installing the monitoring means in the form of at least one transducer at said interface.

8. The method according to claim 7, wherein said in situ measurement stage is performed by installing the transducer at the interface between an envelope and a reinforcement of long fibres embedded in a resin matrix.

9. The method according to claim 8, wherein the transducer is integrated into the composite structure during a manufacturing of said structure prior to producing the reinforcement on the envelope.

10. The method according to claim 2, for monitoring the state of a composite structure forming a reservoir able to contain a pressurized fluid.

11. The method according to claim 10, wherein said further stage of determining the reference deformation or stress level is performed by measuring the deformation or stress level of a partition separating an internal area of the reservoir able to contain the pressurized fluid from an instrumentation box.

12. The method according to claim 11, wherein the instrumentation box is placed on a bottom of the reservoir.

13. The method according to claim 11, further comprising a stage of measuring at least one other quantity chosen from within a group including a temperature at the interface of the structure, a temperature in an immediate vicinity of the structure, an internal pressure of the reservoir, possible shock levels suffered by the reservoir, a time which has elapsed since a previous inspection, a time which has elapsed since the reservoir has entered service, “

empty” and

“

full”

states of the reservoir and a number of fillings thereof.

14. The method according to claim 13, wherein said further stage of measuring at least one other quantity is carried out by installing a monitoring means at least partly in the instrumentation box.

15. A pressurized fluid reservoir comprising:

at least a first part formed from a composite wall formed from an envelope and a reinforcement of long, resin-impregnated fibres adjacent one another along a given interface; and

at least one first transducer integrated into the composite wall at the interface between the envelope and the reinforcements, so as to permit an in situ monitoring of a state of the wall, by comparing a stress level or deformation measured by the first transducer with a reference stress level or deformation of the wall, produced by the uniform pressure of the fluid applied over a total surface of the pressurized fluid reservoir.

16. The reservoir according to claim 15, wherein at least one second transducer is installed on a second part of the reservoir, comprising only said envelope, said second transducer being adapted to measure a stress level or deformation of said second part.

17. The reservoir according to claim 16, wherein said second part is a partition separating an internal area of the reservoir able to contain the fluid from an instrumentation box.

18. The reservoir according to claim 17, wherein said partition forms a bottom of the reservoir.

19. The reservoir according to claim 17, wherein the instrumentation box contains means for monitoring said state of the wall, connected to the first transducer and to the second transducer.

20. A method for monitoring the state of a composite structure, the method comprising the steps of:

exposing the composite structure to a uniform non pressure applied over a total surface of the composite structure, the composite structure having an envelope layer and a reinforcement layer adjacent the envelope layer forming an interface between the envelope layer and reinforcement layer, said envelope layer and said reinforcement layer having different materials;

measuring a deformation or stress level of the composite structure at the interface; and

comparing the measured deformation or stress level of the composite structure at the interface with a reference quantity.

21. The method according to claim 20, wherein the reference quantity is determined by measuring the deformation or stress level of a part of the structure formed from only the envelope layer.

22. The method according to claim 20, wherein the measured deformation or stress level and the reference quantity are compared with a reference curve giving a normal evolution of the deformation or stress level of the structure as a function of the force applied thereto.

23. The method according to claim 22, wherein the reference curve is obtained by measuring beforehand the evolution of the deformation or stress level of said composite structure, in a new state, as a function of the force applied to said new structure.

24. The method according to claim 22, wherein the reference curve is modeled by a second degree equation.

25. The method according to claim 21, wherein the deformation or stress level of the composite structure is measured by at least one transducer installed on the part of the structure formed from only the envelope layer.

26. The method according to claim 20, wherein the deformation or stress level of the composite structure is measured by at least one transducer installed at the interface of the composite structure.

27. The method according to claim 26, wherein at least one transducer is integrated into the composite structure during manufacturing of the envelope layer prior to producing the reinforcement layer on the envelope layer.

28. The method according to claim 20, wherein the composite structure forms a reservoir able to contain a pressurized fluid.

29. The method according to claim 28, wherein a part of the structure is a partition separating an internal area of the reservoir able to contain the pressurized fluid from an instrumentation box.

30. The method according to claim 29, wherein the instrumentation box is placed on a bottom of the reservoir.

31. The method according to claim 28, further comprising a stage of measuring at least one other quantity chosen from within the group including the temperature at the interface of the structure, a temperature in the immediate vicinity of the structure, an internal pressure of the reservoir, the possible shock levels suffered by the reservoir, a time which has elapsed since a previous inspection, a time which has elapsed since the reservoir has entered service, an “

empty” and

“

full”

states of the reservoir, and a number of fillings thereof.

32. The method according to claim 31, wherein said further stage of measuring is carried out with the aid of a monitoring means at least partly installed in the instrumentation box.

33. A method for monitoring the state of a composite structure, the method comprising the steps of:

exposing the composite structure to a uniform pressure applied over a total surface of the composite structure, the composite structure formed from at least two different materials adjacent one another along a given interface;

measuring a deformation or stress level of the composite structure at the interface; and

comparing the measured deformation or stress level of the composite structure at the interface with a reference quantity.

34. The method according to claim 33, wherein the reference quantity is determined by measuring the deformation or stress level of a part of the structure formed from only one of the materials.

35. The method according to claim 33, wherein the measured deformation or stress level and the reference quantity are compared with a reference curve giving a normal evolution of the deformation or stress level of the structure as a function of the force applied thereto.

36. The method according to claim 35, wherein the reference curve is obtained by measuring beforehand the evolution of the deformation or stress level of said composite structure, in a new state, as a function of the force applied to said new structure.

37. The method according to claim 35, wherein the reference curve is modeled by a second degree equation.

38. The method according to claim 34, wherein the deformation or stress level is measured by at least one transducer installed on the part of the structure formed from only one of the materials.

39. The method according to claim 33, wherein the deformation or stress level of the composite structure is measured by at least one transducer installed at the interface of the composite structure.

40. The method according to claim 39, applied to the monitoring of the state of the composite structure, whose different adjacent materials comprise an envelope and a reinforcement of long fibres embedded in a resin matrix.

41. The method according to claim 40, wherein at least one transducer is integrated into the composite structure during manufacturing of the envelope layer prior to producing the reinforcement layer on the envelope layer.

42. The method according to claim 33, wherein the composite structure forms a reservoir able to contain a pressurized fluid.

43. The method according to claim 42, wherein a part of the structure is a partition separating an internal area of the reservoir able to contain the pressurized fluid from an instrumentation box.

44. The method according to claim 43, wherein the instrumentation box is placed at a bottom of the reservoir.

45. The method according to claim 42, further comprising a stage of measuring at least one other quantity chosen from within the group including the temperature at the interface of the structure, a temperature in the immediate vicinity of the structure, an internal pressure of the reservoir, the possible shock levels suffered by the reservoir, a time which has elapsed since a previous inspection, a time which has elapsed since the reservoir has entered service, an “

empty” and

“

full”

states of the reservoir, and a number of fillings thereof.

46. The method according to claim 45, wherein said further stage of measuring is carried out with the aid of a monitoring means at least partly installed in the instrumentation box.

47. A container for containing a pressurized fluid, the container comprising:

an envelope layer;

a reinforcement layer of long resin-impregnated fibers adjacent the envelope layer along an interface, said envelope layer and said reinforcement layer having different materials; and

a first transducer positioned at the interface to permit in situ monitoring of a state of the interface,

wherein the container is subject to uniform pressure applied over a total surface of the container.

48. The container according to claim 47, wherein at least one second transducer is installed on a partition of the reservoir, which is free from any reinforcement, in order to measure the deformation or stress level of said partition.

49. The container according to claim 48, wherein said partition separates an internal area of the reservoir able to contain the fluid from an instrumentation box.

50. The container according to claim 48, wherein said partition forms a bottom of the reservoir.

51. The container according to claim 49, wherein the instrumentation box contains a means for monitoring a state of the reservoir, and is connected to the first transducer and to the second transducer.