Triangular prism type fiber grating acceleration detector
A fiber grating and detector technology, which is applied in multi-dimensional acceleration measurement, acceleration measurement using inertial force, etc., can solve the problems of connection loss, fiber bending loss, not suitable for harsh working environment, large size and mass of detector, etc. Prevent chirp problem, improve lateral anti-interference ability, small size effect
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Embodiment 1
[0036] see figure 1As shown, the triangular prism type fiber grating low frequency geophone of the present invention adopts a special triangular prism type hollow tube column and a triangular prism type mass structure, and mainly consists of the packaging point 1 of the fiber grating, the fiber through hole 2, and the three points of the inertial mass block. Prismatic inertial mass blocks 3 and 4, triangular prism hollow tube wall 5, sensing fiber grating 6, detector base 7, optical fiber through hole 8 at the detector base, and fiber grating packaging point 9 at the base. The inertial mass is mainly composed of two concentric triangular prism structures with unequal side lengths (the side lengths and heights of the triangular prism type inertial mass can be different), the central axis of the inertial mass is in line with the packaging The sensing fiber grating coincides (that is, the packaging position of the sensing fiber grating is located in the geometric center of the in...
Embodiment 2
[0042] In this embodiment, the structural parameters and materials of the geophone are the same as those in Embodiment 1, the difference is that the inertial mass is composed of two parts with different side lengths, and the volume of the upper part of the triangular prism with a larger side length remains unchanged. The height of the triangular prism inertial mass block with a smaller side length of the hollow tube column is increased to 3mm, and the other components and the connection relationship of the components are the same as in Embodiment 1.
Embodiment 3
[0044] In this embodiment, the structural parameters and materials of the sensor are all the same as in Embodiments 1 and 2, the difference is that the cross-sectional area and height of the triangular prism hollow tube of the geophone vary, and the outer length of the triangular prism hollow tube is 15 mm. , the inner side length is 6.9mm, and the wall thickness is 2mm. Therefore, the height of the larger side of the inertial mass block is 30mm, and the side length is 15mm. The height of the smaller side of the mass block is 25mm, and the side length is 6.3mm. , the coupling relationship of other components and components is the same as that of Embodiments 1 and 2.
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