Sensor Mounting System
20220403986 · 2022-12-22
Inventors
Cpc classification
F17C2260/015
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G01D11/30
PHYSICS
F17C2270/0171
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/054
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/011
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0107
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/014
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/043
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0119
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E60/32
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F17C2205/0157
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0465
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/083
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/011
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0491
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F17C13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A sensor mounting assembly is configured for use with a vessel arrangement including at least four vessels. The assembly includes first and second elongated frame members, first and second rollers, and first and second sensors. The first sensor is attached to the first elongated frame member and is configured to contact the surface of the first vessel upon actuation in a first direction. The second sensor is attached to the second elongated frame member and is configured to contact the surface of the second vessel upon actuation in a second direction that is substantially orthogonal to the first direction. This disclosure also describes a method of mounting at least six sensors for use with a vessel arrangement including at least four vessels, the vessel arrangement disposed in a container in a two-by-two stacked configuration having a central space.
Claims
1.-20. (canceled)
21. A method of gathering information on a vessel arrangement having a central space between first, second, third and fourth vessels, the method comprising: inserting an interior assembly into the central space; positioning a first sensor of the interior assembly proximate the first vessel; positioning a second sensor of the interior assembly proximate the second vessel; moving the first sensor in a first direction into contact with the first vessel; and moving the second sensor in a second direction into contact with the second vessel.
22. The method of claim 21, comprising disposing the vessel arrangement in a container.
23. The method of claim 22, comprising orienting the first, second, third and fourth vessels horizontally within the container.
24. The method of claim 22, comprising: attaching a top assembly to the container proximate a top of the container; and positioning a third sensor proximate one of the first or second vessels.
25. The method of claim 22, comprising: attaching a bottom assembly to the container proximate a bottom of the container; and positioning a third sensor proximate one of the first or second vessels.
26. The method of claim 21 wherein the first direction and the second direction are substantially orthogonal to each other.
27. The method of claim 21, comprising positioning a third sensor of the interior assembly proximate the third vessel.
28. The method of claim 27, comprising positioning a fourth sensor of the interior assembly proximate the fourth vessel.
29. The method of claim 28, comprising: moving the third sensor in a third direction into contact with the third vessel; and moving the fourth sensor in a fourth direction into contact with the fourth vessel; wherein the third direction and the fourth direction are substantially orthogonal to each other.
30. The method of claim 21, comprising removing the interior assembly from the central space.
31. The method of claim 21, wherein the first sensor is one of a plurality of first vessel sensors, the method comprising positioning the plurality of first vessel sensors along a length of the first vessel.
32. The method of claim 31, wherein the second sensor is one of a plurality of second vessel sensors, the method comprising positioning the plurality of second vessel sensors along a length of the second vessel.
33. The method of claim 21, wherein the information comprises acoustic wave data relevant to at least one of the first and second vessels.
34. The method of claim 21, wherein moving the first sensor is accomplished with a pneumatic actuator.
35. The method of claim 21, comprising applying a couple force between the first sensor and an outer surface of the first vessel.
36. The method of claim 21, comprising: retracting the first sensor out of contact with the first vessel; and retracting the second sensor out of contact with the second vessel.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0026] The disclosed subject matter will be further explained with reference to the attached figures, wherein like structure or system elements are referred to by like reference numerals throughout the several views. It is contemplated that all descriptions are applicable to like and analogous structures throughout the several embodiments.
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[0049] While the above-identified figures set forth one or more embodiments of the disclosed subject matter, other embodiments are also contemplated, as noted in the disclosure. In all cases, this disclosure presents the disclosed subject matter by way of representation and not limitation. It should be understood that numerous other modifications and embodiments can be devised by those skilled in the art that fall within the scope of the principles of this disclosure.
[0050] The figures may not be drawn to scale. In particular, some features may be enlarged relative to other features for clarity. Moreover, where terms such as above, below, over, under, top, bottom, side, end, right, left, vertical, horizontal, etc., are used, it is to be understood that they are used only for ease of understanding the description. It is contemplated that structures may be oriented otherwise.
DETAILED DESCRIPTION
[0051] As a result of the principal stress state and anisotropic construction of Type III and Type IV cylindrical composite pressure vessels (also called pressure cylinders), several unique wave propagation characteristics are observed by MAE sensors. These principal stress states are caused, for example, by the metallic load sharing liner on the interior of Type III cylinders and the inherently asymmetric laminate construction of Type IV composite pressure cylinders. From a laminated plate theory perspective, the non-symmetric laminate results in non-zero components of the coupling stiffness matrix (B.sub.ij); from a wave propagation perspective, such a result indicates that unlike isotropic plates, pure extensional and flexure mode deformation will not be observed.
[0052] A key component to optimizing the sensor spacing for the MAE testing of composite pressure cylinders and ensuring full coverage of the cylinder is understanding the attenuation behavior of the composite laminate as a function of the propagation angle and the frequency at which the wave propagates. From experimental measurements and considerations of the principal stress state of the vessel, for an equivalent frequency, waves are attenuated more severely at angles approaching the axial direction of the vessel. Conversely, waves are attenuated less severely in the hoop direction, a fact that can be exploited when determining sensor spacing and placement schemes of composite pressure cylinders.
[0053] To minimize the number of sensor locations necessary to fully cover a vessel, increases in signal sensitivity and SNR (signal-to-noise ratio) can be realized through a Phased Array Modal Acoustic Emission (PA-MAE™) approach over traditional single-element MAE measurements. The increase in system sensitivity and SNR provided with PA-MAE™ are utilized in determining sensor spacing in highly attenuative wave propagation measurements, as is common in composite pressure cylinders. Furthermore, it has been shown that accurate source location from a multiple element array is possible.
[0054] In light of the above discussion, sensor array placement that is adequately dense in the axial direction 60, but which simultaneously takes advantage of the less attenuative nature of wave propagation in the hoop direction, is utilized to minimize the number of sensor placement locations, while fully covering the pressure vessel.
[0055] Sensor arrays have been used to assess the structural integrity of pressure vessels in laboratory settings. In the current state of the art, the pressure vessel is removed from its field application and shipped to a laboratory for testing. Thus, pressure vessels are typically not tested when they are deployed in arrangements in use. This disclosure is directed to a sensor mounting system that allows for the testing of pressure vessels in the field, such as in an arrangement 20 of four pressure vessels 22 contained within a container 24, as shown in
[0056] In an exemplary embodiment, container 24 is a typical intermodal shipping container, such as one suitable for use with semi-trailer trucks, trains, cargo ships and barges.
[0057] As shown in
[0058] As shown in
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[0060] In
[0061] In the illustrated embodiments, each of the pressure vessels 22 has a row of sensors 34 (mounted on rail assemblies 32, 44, 46, 48) on diametrically opposed sides of the pressure vessel 22. Thus, in the illustrated embodiment, the rows of sensors 34 are arranged around each pressure vessel 22 with a radial spacing of about 180 degrees. Such an arrangement 20 is particularly suitable for use with phased array MAE sensors. However, it is contemplated that additional rows of sensors 34 (and corresponding rail assemblies) could be added, such as would be suitable with other types of sensors, such as the more traditional single-element MAE sensors, or as vessel diameter, material attenuation behavior, and other factors warrant. For example, additional rail assemblies may be used to space rows of sensors around each pressure vessel 22 with a radial spacing of about 90 degrees. Moreover, where a pressure vessel is removed from a container, additional flexibility is afforded, and a radial spacing between three rows of sensors around a pressure vessel with a radial spacing of about 120 degrees is useful. It is contemplated that still other radial spacings are suitable, such as might be used with other types of sensors.
[0062] As shown in
[0063] Because the interior rail assemblies 44, 46 each include two frame elements 50, the frame elements of the interior rail assemblies 45, 46 in some cases will be referred to with reference numerals 50a and 50b. However, it is to be understood that all references to frame member 50 will also apply to frame members 50a and 50b, unless otherwise indicated.
[0064] Upper interior rail assembly 44 has a plurality of casters 56 arranged similarly to those described with reference to lower interior rail assembly 46. To position the interior rail assemblies 44, 46 in the space 64 between the four pressure vessels 22, in an exemplary method of positioning rail assemblies of an exemplary sensor mounting system, the upper interior rail assembly 44 is inserted into space 64 while the lower interior rail assembly 46 remains outside of arrangement 20. Upper interior rail assembly 44 is inserted into space 64 proximate an end of the pressure vessels 22 by rolling the upper interior rail assembly 44 on casters 56 on the cylindrical surfaces of the two bottom pressure vessels 22. Thus, the upper interior rail assembly 44 would occupy essentially the position shown as being occupied by the lower interior rail assembly 46 in
[0065] After the upper interior rail assembly 44 is lifted into the position shown in
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[0076] Thereafter, the plurality of sensor brackets 58, spaced apart from each other by intervening spacer bars 108, are attached to frame element 50 by moving rollers 84 from one end of frame element 50 toward the other end of frame element 50. To position sensor 34 to obtain information on pressure vessel 22, an actuation device 38 is actuated to move sensor 34 in direction 40, so that the sensing surface of sensor 34 contacts the outer surface of pressure vessel 22 with an appropriate coupling force. In exemplary embodiments, suitable actuation devices 38 include, for example, pneumatic cylinders, electric motors, and magnetic actuators. In an exemplary embodiment, direction 40 is substantially orthogonal to a tangent of the outer surface of pressure vessel 22.
[0077] After gathering and processing information from sensors 34 and data acquisition boxes 36, actuation devices 38 may be activated to retract sensors 34 away from the respective surfaces of pressure vessel 22 so that rail assemblies 32, 44, 46, 48 can be removed from container 24 in a reverse method of their installation. The rail assemblies 32, 44, 46, 48 can then be deployed on a different pressure vessel arrangement 20 for assessment of the structural integrity and estimated useful remaining life of a different set of pressure vessels 22.
[0078] For example, for removal of bottom rail assembly 48, in an exemplary embodiment, the connected line of multiple sensor brackets 58 and attached intervening spacer bars 108 can be pulled off one end of frame 50. Then, two portions 88, 92 of pipe bracket 82 can be disconnected, allowing frame 50 to be pulled out opening 75 in end wall 73 of container 24.
[0079] Lower interior rail assembly 46 can be rolled via casters 56 on the two bottom pressure vessels 22, out of opening 74 of end wall 72 of container 24, to thereby remove lower interior rail assembly 46 from space 64 between the pressure vessels 20. For removal of upper interior rail assembly 44, cable 68 is detached from hook 70 and upper interior rail assembly 44 is lowered so that casters 56 contact the two bottom pressure vessels 22. Upper interior rail assembly 44 can be rolled via casters 56 on the two bottom pressure vessels 22, out of opening 74 of end wall 72 of container 24, to thereby remove upper interior rail assembly 44 from space 64 between the pressure vessels 20.
[0080] For removal of upper rail assembly 32 from container 24, two portions 120, 128 of container bracket 42 can be disconnected, allowing their removal from sill 132 of side wall 62 of container 24. Frame 50 can be lifted out of container 24 so that a roof of container 24 can be replaced.
[0081] Although the subject of this disclosure has been described with reference to several embodiments, workers skilled in the art will recognize that changes may be made in form and detail without departing from the scope of the disclosure. In addition, any feature disclosed with respect to one rail assembly 32, 44, 46, 48 may be incorporated in another rail assembly 32, 44, 46, 48, and vice-versa.