GB2141539A - Apparatus for detecting structural faults in materials - Google Patents
Apparatus for detecting structural faults in materials Download PDFInfo
- Publication number
- GB2141539A GB2141539A GB08414965A GB8414965A GB2141539A GB 2141539 A GB2141539 A GB 2141539A GB 08414965 A GB08414965 A GB 08414965A GB 8414965 A GB8414965 A GB 8414965A GB 2141539 A GB2141539 A GB 2141539A
- Authority
- GB
- United Kingdom
- Prior art keywords
- energy
- transmission
- arm
- pivotally mounted
- structural fault
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M11/00—Testing of optical apparatus; Testing structures by optical methods not otherwise provided for
- G01M11/08—Testing mechanical properties
- G01M11/083—Testing mechanical properties by using an optical fiber in contact with the device under test [DUT]
- G01M11/086—Details about the embedment of the optical fiber within the DUT
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B21/00—Alarms responsive to a single specified undesired or abnormal condition and not otherwise provided for
- G08B21/18—Status alarms
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Investigating Or Analysing Materials By Optical Means (AREA)
Abstract
The apparatus comprises a body (10) pivotally mounting therein a bell crank lever (38). The latter mounts at one end an external foot (48) for engaging with the material and at its other end presents an optical window (44, 46) normally disposed in a gap between aligned ends within the body (10) of fibre optic cables (24, 30). An infra-red beam is transmitted along the cables (24, 30) and any slight movement of the foot (48) caused by a fault in the material will displace the optical window to interrupt the infra-red beam and thus give an indication of structural or component failure. Such a probe is isolated electrically and is free from sparking and fire hazards. <IMAGE>
Description
SPECIFICATION
Fault detecting apparatus
This invention relates to a fault detecting
apparatus and particularly an apparatus for
non-destructive detecting of structural faults in
materials in hostile or inaccessible areas for
example oil rigs and the petrochemical industry.
Problems are encountered in using probes for detecting faults in such areas where conventional x-ray and ultrasonic test techniques cannot be used, equipment being required to
be electrically isolated and free from sparking and fire hazards.
According to the present invention there is provided apparatus for detecting 8 structural fault in a material, said apparatus comprising
a body, means pivotally mounted within the
body and providing a first part, extending externally of the body for engagement with the material on which any structural fault is to
be detected, and a second part presenting a
path for transmission of energy therethrough,
means for transmitting a beam of said energy within the body and means for receiving the beam of said energy, said second part of the pivotally mounted means being normally positioned with the transmission path aligned with the transmitting and receiving means, but being movable in the event of a structural fault on the material engaged by said first part, whereby to affect the transmission of energy.
Preferably, the pivotally mounted means comprises a lever of generally bell crank configuration having a first arm defining the transmission path at a free end thereof, and a second arm providing said first part at a free end thereof. The length of the first and second arms may be in a ratio of 8:1.
Preferably also the energy transmitting means comprises a first fibre optic cable connectible to the body with an end located therein for transmission of infra-red light into the body and the energy receiving means comprises a further fibre optic cable having an end within the body aligned with said end of the first cable.
An embodiment of the present invention will now be described by way of example only, with reference to the accompanying drawings, in which:
Figure 1 is a perspective view of an apparatus according to the invention;
Figure 2 is an exploded view of the apparatus of Fig. 1; and
Figure 3 is an elevation showing part of one of the components of the apparatus.
Referring to the drawings, a detection apparatus or probe has a main body 10 defined by a housing 12 and a cover 14 which is removably mounted on the housing 12. At one end, the housing 1 2 defines a cavity 1 6 opening on to one side face 1 8 and an elongate recess 20 extends from, and is in communication with, the cavity 1 6 to the other end of the housing 12, the recess 20 also opening onto the side face 1 8. At the other end, the recess 20 turns through 90 to also open onto an edge 22 of the housing 1 2.
The cover 1 4 is securable by any suitable means on to the side face 1 8 to close the cavity 1 6 and the recess 20, except for the end thereof which opens onto the edge 22.
On the end of the housing 1 2 at the cavity 1 6 a first fibre optic cable 24 is mounted through the end wall 26 of the housing 1 2 to locate an end 28 within the cavity 16. Also connected to the housing 1 2 to extend through the end wall 26 is a further fibre optic cable 30 which continues within the cavity 1 6 and has an end 32 mounted in an internal support 34 to face, and be in alignment with, the end 28 of the cable 24.
The cables 24, 30 therefore present a path for transmission of a beam of infra-red light through the cables 24, 30 and across the gap between the ends 28, 32.
At the end of the recess 20 remote from the cavity 1 6 a pivot pin 36 is provided and pivotally mounts a lever 38 of generally bell crank configuration, having a first arm 40 extending along the recess 20 towards the cavity 1 6 and a second arm 42 extending at substantially 90 to the arm 40 through the opening in the edge 22 of the housing 1 2.
Within the cavity 16, the arm 40 provides an end section 44 extending at right angles to the main part of the arm 40 and having a through aperture 46. In a normal operating position the end part 44 is positioned in the gap between the ends 28, 32 of the cables 24, 30 such that the aperture 46 is in alignment with the ends 28, 32 thereby enabling continued transmission of the infra-red beam. The end part 44 presenting such an "optical window" is machined to a thickness of 0.030 inches and the aperture 46 is drilled to the same diameter as the cables. The fibre optic cable connector has to be machined as close to the end part 44 with the aperture 46 as possible.
The arm 42 pivotally mounts a foot 48 externally of the housing 12, the foot 48 having a mounting lug 50 for receiving the end of the arm 42 and a pivot pin (not shown) extending through aligned apertures in the lug 50 and the arm 42. The foot 48 also has a pad 52 which is intended to engage with the material in respect of which any structural fault is to be detected.
The body 10 is preferably produced from stainless steel or abs plastic and the lever 40 preferably has a ratio of 1:8 from the foot 48 through the pivot point 36 to the optic window. The movement of the lever can be adjusted to accomodate variations in the degree of accuracy required. The arrangement is such that the slightest movement on the foot 48 will move the lever 40 such as to close the optical window and thus break transmission of the infra-red beam. This break in transmission can be discernable from a remote location to give an early visual and/or audible warning of structural failure, cracks and defects.
The probe can be totally enclosed and sealed, for example with silicon rubber, and, being isolated electrically and thus free from sparking and fire hazards, is particularly useful in hostile environments such as oil rig and airframe work and other inaccessible areas where x-ray and ultrasonic test techniques cannot be used. The probe can be attached to structures by either bonding, strapping or bolting into the required position and the cover 14 has a connecting flange 54 to assist in this.
It will be appreciated that although a single channel device has been described, a multichannel unit can be provided, giving for example 20 to 30 channels. It is envisaged that a multiplexer will be used in such a multichannel unit for line selection.
Various modifications may be made without departing from the invention. For example the configuration of the various components may differ from that described and shown provided sufficient movement is derived at the optical window on slightest movement of the foot so that an induction of structural or component failure can be given at any desired location.
The apparatus may be controlled at a remote location for example by a microprocessor.
Claims (9)
1. Apparatus for detecting a structural fault in a material, said apparatus comprising a body, means pivotally mounted within the body and providing a first part, extending externally of the body for engagement with the material on which any structural fault is to be detected, and a second part presenting a path for transmission of energy therethrough, means for transmitting a beam of said energy within the body and means for receiving the beam of said energy, said second part of the pivotally mounted means being normally positioned with the transmission path aligned with the transmitting and receiving means, but being movable in the event of a structural fault on the material engaged by said first part, whereby to affect the transmission of energy.
2. Apparatus according to claim 1, wherein the pivotally mounted means comprises a lever of generally bell crank configuration having a first arm defining the transmission path at a free end thereof, and a second arm providing said first part at a free end thereof.
3. Apparatus according to claim 2, wherein the length of the first and second arms are in a ratio of 8:1.
4. Apparatus according to claim 2 or 3, wherein said second arm includes said first part in the form of a pivotally mounted foot member.
5. Apparatus according to any of claims 2 to 4, wherein said first arm has an end provided with a through hole to define the transmission path.
6. Apparatus according to any of the preceding claims, wherein the energy transmitting means comprises a first fibre optic cable connectible to the body with an end located therein for transmission of infra-red light into the body and the energy receiving means comprises a further fibre optic cable having an end within the body aligned with said end of the first cable.
7. Apparatus according to any of the preceding claims, wherein the body is enclosed within a coating of silicon rubber.
8. Apparatus for detecting a structural fault in a material substantially as hereinbefore described with reference to the accompanying drawings.
9. Any novel subject matter or combination including novel subject matter herein disclosed, whether or not within the scope of or relating to the same invention as any of the preceding claims.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08414965A GB2141539B (en) | 1983-06-16 | 1984-06-12 | Apparatus for detecting structural faults in materials |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB838316356A GB8316356D0 (en) | 1983-06-16 | 1983-06-16 | Fibre-optic system |
GB08414965A GB2141539B (en) | 1983-06-16 | 1984-06-12 | Apparatus for detecting structural faults in materials |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8414965D0 GB8414965D0 (en) | 1984-07-18 |
GB2141539A true GB2141539A (en) | 1984-12-19 |
GB2141539B GB2141539B (en) | 1986-10-01 |
Family
ID=26286379
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08414965A Expired GB2141539B (en) | 1983-06-16 | 1984-06-12 | Apparatus for detecting structural faults in materials |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2141539B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2200748A (en) * | 1987-01-16 | 1988-08-10 | Europ Microwaves Limited | Door alarm system |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2095825A (en) * | 1981-03-26 | 1982-10-06 | Johnson Matthey Plc | Profile change sensor |
-
1984
- 1984-06-12 GB GB08414965A patent/GB2141539B/en not_active Expired
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2095825A (en) * | 1981-03-26 | 1982-10-06 | Johnson Matthey Plc | Profile change sensor |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2200748A (en) * | 1987-01-16 | 1988-08-10 | Europ Microwaves Limited | Door alarm system |
Also Published As
Publication number | Publication date |
---|---|
GB2141539B (en) | 1986-10-01 |
GB8414965D0 (en) | 1984-07-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |