Abstract:
For continuous monitoring of dynamic loads, including stresses and strains in large hull structures for vessels (5), a strain measurement system (2) is employed with fibre optic cables which connect optical strain sensors (7; 16) at different points in the hull structure. Optical signals for detection of stresses and strains are distributed to the strain sensors (7; 16) from an optical transmitter (11). The strain measurement system (2) is connected via a central monitoring unit (10) to a computer-implemented control system (1) which in turn is connected to a display and data presentation unit (4) and possibly other measurement systems (3). In a first operating mode in this method strain values during loading and unloading of the vessel (5) are detected by means of the strain sensors (7; 16). By means of the control system (1) a curve is generated which shows an average strain, and an alarm signal if the average strain exceeds a predetermined threshold which indicates an unacceptable level of strain. In a second operating mode when the vessel (5) is underway, strains are continuously detected by means of the strain sensors (7; 16). An alarm signal is generated if the average strain exceeds a predetermined threshold which indicates an unacceptable level of strain. A strain measurement system and a fibre optic strain sensor (16) for use with this method are also described.
Abstract:
A fiber optic load sensor (12) and method of forming the same are disclosed for sensing the load applied to a structural surface (18). The sensor (12) comprises a length of fiber optic material (14) disposed adjacent to the surface (18). The fiber optic material is connectable to a light source (22) and to a light detector (26). The fiber optic material (14) includes at least one curved portion deformable in response to the applied load. The curved portion is dimensioned such that the light passing through the fiber optic material (14) is attenuated in linear relation to the deformation of the curved portion in response to the load applied to the surface.
Abstract:
The invention relates to a vehicle intrusion detector for detecting the severity of an accident. The inventive intrusion detector comprises a first optical guide system (2) and a second optical guide system (5), said systems (2, 5) being separated by an intermediate gap (8) with a width (h). The inventive intrusion detector is characterised in that the first optical guide system (2) is placed in the direction of an intrusion side and in that the second optical guide system (5) is placed in the direction of the inside of the vehicle.
Abstract:
The device according to the present invention includes an optical sensing device including first and second lightguides positioned side by side, and preferably covered as a unit with a layer of transmissive material, wherein the lightguides are adapted to detect or sense the presence, location, identity and shape of external media through modulation of the intensity of light coupled from one lightguide to the other through the transmissive material.
Abstract:
The aim of the invention is to provide a deformation sensor that requires no additional sensor for operational testing. The inventive deformation sensor consists of an optical transmission medium (UM1, UM2), several transmitting elements (S1, S2) which couple light of different wavelengths ( lambda 1, lambda 2) into the transmission medium (UM1, UM2); and several receiving elements (E1, E2) which selectively couple the transmitted light out of the transmission medium (UM1, UM2) according to wavelengths. An evaluating unit (AW) detects deviations between the output signals (a1, a2) for the receiving elements (E1, E2) and indicates defective functioning of the sensor if these deviations exceed a predetermined value. The receiving elements (E1, E2) can also react inversely. The invention is suitable for detecting a side crash.
Abstract:
A strain transducer (14) is responsive to a deflection thereof for providing a detectable output signal having a characteristic that is expressive of the deflection. The transducer includes an optical fiber having an input port (16) for coupling to a source (18) of optical radiation and an output port (20) for coupling to a receiver (22) of the optical radiation. The optical fiber has at least one region (14') that has a radius of curvature that is equal to or less than a critical radius of curvature for the optical fiber. The at least one region includes a detectable loss in the optical signal in response to being deflected. The optical fiber is disposed within a plane and the detectable loss is shown to be greater for an out-of-plane deflection than for an in-plane deflection. The strain transducer is shown to be especially useful for inclusion within a laminated composite structure, such as a component of an aircraft wing.
Abstract:
Systems and methods of monitoring posture and vital signs are disclosed. In some embodiments, the system includes a cushion on which a user can sit. The cushion includes a first optical fiber sensor, a second sensor, and a first computing device. The system may further include a second computing device communicatively coupled to the first computing device and configured to receive sensor data from the first computing device. One or both of the first and second computing devices may operate to combine a signal indicative of the movement of the user with a signal indicative of the direction of movement of the user to determine a posture of the user. The system may provide feedback based on the user's posture and recommend actions to improve posture. The system may further monitor the user's heart rate, respiration rate, or other vital signs.
Abstract:
Es werden ein mehrschichtiger Sensor (10) und eine Verwendung des vorgestellten Sensors (10) beschrieben. Dieser Sensor ist mehrschichtig ausgebildet. Durch den Sensor (10) ist ein Lichtwellenleiter (18) derart geführt, dass im Falle einer äusseren Krafteinwirkung these auf den Lichtwellenleiter einwirkt.
Abstract:
An optical fibre strain gauge (1) for an engineering structure e.g. a bridge, building, pipe, plant or the like, comprises: (a) a plurality of supports (8, 10) for the optical fibre that can be located on a surface of the structure and are spaced apart from one another over a part of the surface; and (b) at least one optical fibre (12) that is looped around the supports so that it extends between the supports, the optical fibre being fixed to the supports so that the length of the part of the fibre extending between the supports will vary in accordance with strain of the surface of the structure. The optical fibre(s) (12) can be looped around the supports (8, 10) a number of times, which enables the fibre(s) to be held more easily, and enables the strain gauge to incorporate a length of fibre significantly greater than the dimension of the area of the structure that is being monitored. The fibre(s) will normally contain reflectors such as Bragg gratings to enable signals to be monitored.
Abstract:
An optical fibre (7) exhibits varying transmission characteristics in different strain states and can have an S-shaped microbend. For producing such a fibre it is heated locally in a small region, as viewed in the longidutinal direction of the fibre, and then the portions of the fibre (1) located at the two sides of the heated region are displaced in relation to each other in a transverse direction in relation to the longitudinal direction of the fibre. It can be performed in a conventional fusion-splicing apparatus for optical fibres. Alternatively, a laser can be used as a heating source, what is particularly suitable for processing optical fibres having longitudinal cavities in order to infer to it similar transmission characteristics. The optical fibres produced by this method are suited for use as sensors, e.g. strain gauges.