System and Method For Monitoring Mechanically Coupled Structures

• US 20130291637A1
• Filed: 12/05/2011
• Published: 11/07/2013
• Est. Priority Date: 12/06/2010
• Status: Abandoned Application

• Current Assignee: Northrop Grumman Litef Gmbh (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Litef Gmbh (Northrop Grumman Corporation)
• Inventors: Dorner, Georg, Schreiber, Ulrich, Rasch, Andreas, Igel, Heiner, Wassermann, Joachim
• Application Number:
  US13/990,794
• Publication Number:
  US 20130291637A1
• Time in Patent Office: Days
• US Class Current: 73/504.08
• CPC Class Codes: G01C 1/00 Measuring angles
• CPC Class Codes: G01C 15/00 Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
• CPC Class Codes: G01C 19/38 with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
• 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

A system for monitoring a mechanically coupled structure with a first sensor configured to determine at predetermined times its orientation relative to Earth'"'"'s rotation axis as a first measurement. The first sensor is connectable with a first part of the mechanically coupled structure with at least one second sensor which has a known first orientation to the first sensor at startup of the system and which is configured to determine a rotation rate or an acceleration as a second measurement. The at least one second sensor is connectable with a second part of the mechanically coupled structure with a central unit and with a communication network over which the central unit is connected with the first sensor and the second sensor wherein the first sensor is configured to transmit the first measurement to the central unit. The second sensor is configured to transmit the second measurement to the central unit and the central unit is configured to monitor the mechanically coupled structure by means of the first and second measurement.

Claims

1. System for monitoring a mechanically coupled structure with

a first sensor configured to determine at predetermined times its orientation relative to Earth'"'"'s rotation axis as a first measurement, wherein the first sensor is connectable with a first part of the mechanically coupled structure,

at least one second sensor, which has a known first orientation to the first sensor at startup of the system and which is configured to determine a rotation rate as a second measurement,

at least one third sensor, which has a known first orientation to the first sensor at startup of the system and which is configured to determine an acceleration as a third measurement, wherein the at least one second sensor and the at least one third sensor is connectable with a second part of the mechanically coupled structure,

a central unit, and

a communication network over which the central unit is connected with the first sensor, the second sensor, and the third sensor,

wherein the first sensor is configured to transmit the first measurement to the central unit, the second sensor is configured to transmit the second measurement to the central unit, the third sensor is configured to transmit the third measurement to the central unit, and the central unit is configured to monitor the mechanically coupled structure by means of the first, second, and third measurements.

2. System according to claim 1, characterized in that

the at least one second sensor is formed as rotation sensor which has compared to the first sensor less precision for determining the orientation of Earth'"'"'s rotation axis.

3. System according to claim 2, characterized in that

the first sensor and the second sensor comprise a time measurement unit and transmit the first and second measurements together with the times at which the measurements were taken to the central unit and

that the central unit is configured to determine a chronological sequence of the orientation of the first sensor and the second sensor to each other from the transmitted measurements and the transmitted times.

5. System according to claim 1, characterized in that

the first sensor and the at least one second sensor are attached at different positions to the monitored mechanically coupled structure.

6. System according to claim 1,

characterized in that

the communication network is configured for bidirectional direct communication between the sensors.

7. System according to claim 1,

characterized in that

the second sensor is configured to be recalibrated on the basis of the measurements of the first sensor after a predetermined time interval after startup of the system.

4. (canceled)

8. Method for monitoring of mechanically coupled structures comprising the following steps:

determining at predetermined times the orientation of a first sensor relative to the Earth'"'"'s rotation axis by means of the sensor, wherein the first sensor is connected with a first part of the mechanically coupled structure,

transmitting the first measurement to a central unit over a communication network,

determining a rotation rate of at least one second sensor, which has a known first orientation to the first sensor at startup of the system as a second measurement,

determining of the acceleration of at least one third sensor, which has a known first orientation to the first sensor at startup of the system as a third measurement, wherein the at least one second sensor at the at least one third sensor are connected with a second part of the mechanically coupled structure,

transmitting of the second and the third measurement to the central unit over the communication network,

generating a monitoring value from the first, the second, and the third measurement.

9. Method according to claim 8,

characterized in that

the second sensor measures his change of orientation independently from the transmitted orientation of the first sensor and a change of the position of the second sensor with respect to the position of the first sensor is determined by means of the transmitted orientation of the first sensor.

10. Method according to claim 8,

characterized in that

the first sensor and the second sensor are each attached at different parts of a mechanically coupled structure, wherein the different parts are unmoveably mechanically coupled with respect to each other.

11. Method according to claim 8,

characterized in that

the first sensor and the second sensor are each attached at different parts of a mechanically coupled structure, wherein the different parts are moveably mechanically coupled with respect to each other,

the respective different parts can perform movement with respect to each other allowed by the mechanical coupling, and

the monitoring value determined from the central unit indicates whether one of the allowed or non-allowed movements between the different parts is present.

12. Method according to claim 8,

characterized in that

vibration excitations are impressed from outside on the mechanically coupled structure,

the third sensor is formed as translation sensor and the apparent phase velocity of the measured vibration in the mechanically coupled structure is determined from the measured orientation of the first sensor or of the second sensor and the measured acceleration of the translation sensor.

13. Method according to claim 8,

characterized in that

the central unit detects a measuring error in case the measurement of the first sensor does not contain Earth'"'"'s rotation rate.

14. Method according to claim 8, characterized in that

the central unit determines time-dependent frequency spectra from a chronological sequence of the transmitted first measurements, and the transmitted third measurements and generates a further monitoring value from the frequency spectra.

15. Method according to claim 8,

characterized in that

the second sensor and/or the third sensor is recalibrated after a predetermined time interval after the startup of the system.

16. Method according to claim 8, characterized in that

the mechanically coupled structure is formed as an antenna of a Global Navigation Satellite System GNSS.