Structural monitoring sensor system

• US 6,647,161 B1
• Filed: 11/13/2002
• Issued: 11/11/2003
• Est. Priority Date: 12/15/1995
• Status: Expired due to Term

• Current Assignee: EFS International SA
• Original Assignee: Malcolm H. Hodge
• Inventors: Hodge, Malcolm H.
• Primary Examiner(s): Ullah, Akm Enayet
• Assistant Examiner(s): CONNELLY, MICHELLE R
• Application Number:
  US10/293,811
• Time in Patent Office: 363 Days
• Field of Search: 385/12, 385/13
• US Class Current: 385/12
• CPC Class Codes: G01B 11/16 for measuring the deformation in a solid, e.g. optical strain gauge
• CPC Class Codes: G01D 5/268 using optical fibres G01D5/28 - G01D5/38 take precedence
• CPC Class Codes: G01M 11/086 Details about the embedment of the optical fiber within the DUT
• CPC Class Codes: G01M 5/0008 of bridges
• CPC Class Codes: G01M 5/0033 by determining damage, crack or wear
• CPC Class Codes: G01M 5/0041 by determining deflection or stress
• CPC Class Codes: G01M 5/0066 by exciting or detecting vibration or acceleration vibration testing of structures G01M7/00

Abstract

The present invention is directed to a system for continuous physical integrity monitoring of large civil structures such as bridges and high-rise buildings . . . wherein the relevant sensor data stream is generated continuously and transmitted to the data gathering location without the need for an incoming triggering signal of any kind; i.e., it is a one way transmission system. Specifically, it is a concept for an interlinked multi-parameter Early Warning Sensor system with a full time data management capability for structures. The invention is also directed to both the system construction, with its communication capability, and also designs of specific sensors applicable to the system as a whole. As a practical example of application of the present invention to a structure, the description in this application is directed primarily towards system applications for bridge integrity early warning systems.

Claims

1. Apparatus for monitoring a structure comprising:

(a) a source of power;

(b) a transceiver connected to said source of power for transmitting and receiving pulses of light;

(c) a plurality of optical sensors for deployment on said structure, at least one of said sensors having a first element operatively connected to a first part of said structure and a second element movable relative to said first element and operatively connected to a second part of said structure, at least one position of said second element relative to said first element being a first state of said sensor and at least one position of said second element relative to said first element being a second state of said sensor, each of said sensors being capable of receiving pulses of light in said first and second states and for transmitting said pulses of light in said second state;

(d) a cable of optical fibers for development said structure, said cable having at least one plurality of optical fibers operatively connected to said transceiver, each of said sensors being connected to at least one of said optical fibers for transmitting said optical pulses from said transceiver to said sensor and for returning said optical pulses from said sensor to said transceiver when said sensor is in its second state; and

(e) the first and second elements of at least one of said sensors being connected to said structure by a drone cable so that changes in a selected condition of said structure are transmitted to said one sensor through said drone cable, thereby enabling said drone cable to be made of a material which has desirable characteristics for physically transmitting changes in the selected condition of said structure and for deployment in environmentally hazardous areas and enabling said cable of optical fibers to passively deploy in environmentally safe areas of the structure.

2. Apparatus for monitoring a structure as recited in claim 1, wherein said drone cable is made of an aramid fiber.

3. Apparatus for monitoring a structure as recited in claim 1, wherein said optical sensor has a first element and a second element which is movable relative to said first element, said drone cable having a first length which is connected to a first part of said structure and to said first element and a second length which is connected to a second part of said structure and to said second element.