Inertial dynamics measurement and structural configuration variation for hydrodynamic stability evaluation of a towed body

• US 9,057,738 B1
• Filed: 11/02/2012
• Issued: 06/16/2015
• Est. Priority Date: 11/02/2012
• Status: Expired due to Fees

• Current Assignee: the united states of america as represented by the secretary of the navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Sterling, John A., Hanback, Michael George, Ebner, Stephen Paul, Nashold, Daniel Richard, Strano, Paul Michael, Pickett, David Marcus, Colegrove, Dana Carl
• Primary Examiner(s): KWOK, HELEN C
• Application Number:
  US13/667,833
• Time in Patent Office: 956 Days
• US Class Current: 1/1
• CPC Class Codes: G01C 19/5783 Mountings or housings not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719
• CPC Class Codes: G01P 1/023 for acceleration measuring devices
• CPC Class Codes: G01P 21/00 Testing or calibrating of apparatus or devices covered by the preceding groups

Abstract

A typical inventive device is self-contained and is designed for adjunctive placement at the unconnected end of a towed body in order to test dynamic motions of the towed body. The inventive device includes an IMU, a computer, wired/wireless communication electronics, a fluid-dynamically shaped member, and a cylindrical housing (which encloses the IMU, the computer, and the communication electronics). The housing is connected to the towed body aft of the towed body, and the shaped member is connected to the housing aft of the housing. Data is acquired that is indicative of the inertial dynamics of the towed body while in motion through a fluidic medium. Differently shaped members can be independently connected to the housing at different times, each influencing in its own way the inertial dynamics of the towed body and yielding its own set of data. Comparisons can thus be drawn between/among differently shaped members.

Claims

1. A dynamic motion testing apparatus for a towed body, the apparatus comprising an inertial dynamics measurement device and a configurative structure, the towed body and the apparatus each being characterized by a longitudinal axis, the apparatus being capable of being coaxially coupled with the towed body whereby the inertial dynamics measurement device is coaxially attached to the towed body at the aft axial-longitudinal end of the towed body and the configurative structure is coaxially attached to the inertial dynamics measurement device at the aft axial-longitudinal end of the inertial dynamics measurement device, the inertial dynamics measurement device including an inertial measurement unit for obtaining inertial dynamics data pertaining to the towed body during motion of the towed body while the apparatus is coaxially coupled with the towed body, wherein the configurative structure is characterized by a shape selected from the group consisting of:

a cylinder having an attachable axial-cylindrical end and a concave axial-cylindrical end;

the combination including a truncated cone and plural axial fins projecting from the truncated cone;

the combination including a truncated cone and a wheel having spokes projecting from the truncated cone at the truncated end of the truncated cone;

wherein if the configurative structure is characterized by the shape of the cylinder having an attachable axial-cylindrical end and a concave axial-cylindrical end, then the configurative structure is coaxially attached to the inertial dynamics measurement device at the attachable axial-cylindrical end of the cylinder;

wherein if the configurative structure is characterized by the shape of the combination including a truncated cone and plural axial fins projecting from the truncated cone at the truncated end of the truncated cone, then the truncated cone tapers in the aft axial-longitudinal direction, away from the aft axial-longitudinal end of the inertial dynamics measurement device;

wherein if the configurative structure is characterized by the shape of the combination including a truncated cone and a wheel having spokes projecting from the truncated cone at the truncated end of the truncated cone, then the truncated cone tapers in the aft axial-longitudinal direction, away from the aft axial-longitudinal end of the inertial dynamics measurement device.

2. The dynamic motion testing apparatus of claim 1 wherein the motion of the towed body includes marine navigation of the towed body, and wherein the inertial dynamics data pertaining to the towed body includes hydrodynamics data pertaining to the towed body during marine navigation of the towed body.

3. The dynamic motion testing apparatus of claim 1 wherein the inertial dynamics measurement device further includes an onboard computer for collecting the inertial dynamics data, and at least one communication device for transmitting the inertial dynamics data from the onboard computer to an off-board computer.

4. The dynamic motion testing apparatus of claim 3 wherein the at least one communication device includes at least one of a wired communication device and a wireless communication device.

5. The dynamic motion testing apparatus of claim 3 wherein the inertial dynamics measurement device further includes an at least substantially cylindrical housing, the inertial dynamics measurement device further comprising an onboard computer for collecting inertial measurement data, and at least one communication device for transmitting the inertial measurement data from the onboard computer to an off-board computer, the at least substantially cylindrical housing enclosing the inertial measurement unit, the onboard computer, and the at least one communication device.

6. The dynamic motion testing apparatus of claim 5 wherein the at least one communication device includes at least one of a wired communication device and a wireless communication device.

7. The dynamic motion testing apparatus of claim 1, wherein the apparatus comprises at least two separate differently shaped configurative structures for alternative attachment to the inertial dynamics measurement device, each configurative structure being capable of uniquely affecting the inertial dynamics of the towed body during motion of the towed body, the inertial measurement unit being capable of obtaining a set of inertial dynamics data corresponding to each configurative structure during motion of the towed body while the apparatus is coaxially coupled with the towed body.

8. The dynamic motion testing apparatus of claim 7 wherein:

the inertial dynamics measurement device includes an at least substantially cylindrical housing;

the apparatus comprises an onboard computer for collecting inertial measurement data, and at least one communication device for transmitting the inertial measurement data from the onboard computer to an off-board computer, the housing enclosing the inertial measurement unit, the onboard computer, and the at least one communication device.

15. The dynamic motion testing apparatus of claim 1 wherein the configurative structure is characterized by the shape of the cylinder having an attachable axial-cylindrical end and a concave axial-cylindrical end.

16. The dynamic motion testing apparatus of claim 1 wherein the configurative structure is characterized by the shape of the combination including a truncated cone and plural axial fins projecting from the truncated cone.

17. The dynamic motion testing apparatus of claim 1 wherein the configurative structure is characterized by the shape of the combination including a truncated cone and a wheel having spokes projecting from the truncated cone at the truncated end of the truncated cone.

9. A device for evaluating stability of a towed body in motion, the device comprising:

an inertial dynamics measurement component including an inertial measurement unit capable of sensing dynamic motions, a computer for generating data based on signals received from the inertial measurement unit, and a substantially cylindrical housing for enclosing said inertial measurement unit and said computer, said housing capable of coaxially connecting to and disconnecting from an elongate towed body at the trailing end of said towed body; and

a structural configuration variation component including at least two individually configured alternate structures, each said alternate structure capable of coaxially connecting to and disconnecting from said substantially cylindrical housing at the trailing end of said substantially cylindrical housing in the absence of any other said individually configured alternate structure;

wherein said at least two individually configured alternate structures are at least two different said individually configured alternate structures selected from the group consisting of;

a said individually configured alternate structure characterized by a cylindrical shape having an attachment cylindrical end and a nonattachment cylindrical end, said nonattachment cylindrical end characterized by a concave surface, wherein said coaxial connection of said individually configured alternate structure to said housing includes attachment of said individually configured alternate structure at said attachment cylindrical end so that said nonattachment cylindrical end is aft of said attachment cylindrical end;

a said individually configured alternate structure characterized by a shape describing a truncated cone and plural axial fins projecting from said truncated cone, wherein said truncated cone tapers aft;

a said individually configured alternate structure characterized by a shape describing a truncated cone and a wheel having spokes, said wheel situated coaxial with said truncated cone at the aft end of said truncated cone, wherein said truncated cone tapers aft.

10. The device for evaluating stability of claim 9 wherein the device comprises communication instrumentation for sending said data from said computer to a remote location, said substantially cylindrical housing enclosing said communication instrumentation.

11. The device for evaluating stability of claim 9 wherein each said alternate structure has its own said data associated therewith when said alternate structure is connected to said substantially cylindrical housing, said substantially cylindrical housing is connected to said towed body, and said towed body is in motion.

12. The device for evaluating stability of claim 11 wherein the device comprises communication instrumentation for sending said data from said computer to a remote location, said substantially cylindrical housing enclosing said communication instrumentation.

13. A method for testing dynamic motion of a towed body, the method comprising:

attaching an inertial dynamics measurement device to an elongate towed body at the aft longitudinal end of said elongate towed body, wherein said elongate towed body and said inertial dynamics measurement device are each characterized by a geometric axis, and wherein said attachment of said inertial dynamics measurement device to said elongate towed body is performed so that said elongate towed body and said inertial dynamics measurement device are at least substantially coaxial;

attaching a first configurative structure to said inertial dynamics measurement device at the aft longitudinal end of said inertial dynamics measurement device, wherein said first configurative structure is characterized by a geometric axis, and wherein said attachment of said first configurative structure to said inertial dynamics measurement device is performed so that said elongate towed body, said inertial dynamics measurement device, and said first configurative structure are at least substantially coaxial;

obtaining, using said inertial dynamics measurement device, a first set of inertial dynamics data, set first set of inertial dynamics data pertaining to said elongate towed body during motion of said elongate towed body while said inertial dynamics measurement device is attached to said elongate towed body and said first configurative structure is attached to said inertial dynamics measurement device;

detaching said first configurative structure from said inertial dynamics measurement device;

attaching a second configurative structure to said inertial dynamics measurement device at the aft longitudinal end of said inertial dynamics measurement device, wherein said second configurative structure is characterized by a geometric axis, and wherein said attachment of said second configurative structure to said inertial dynamics measurement device is performed so that said elongate towed body, said inertial dynamics measurement device, and said second configurative structure are at least substantially coaxial;

obtaining, using said inertial dynamics measurement device, a second set of inertial dynamics data, said second set of inertial dynamics data pertaining to said elongate towed body during motion of said elongate towed body while said inertial dynamics measurement device is attached to said elongate towed body and said second configurative structure is attached to said inertial dynamics measurement device;

comparing said first set of inertial dynamics data and said second set of inertial dynamics data.

14. The method for testing of claim 13 wherein the method further comprises collecting said inertial dynamics data using an on-board computer, and transmitting said inertial dynamics data from said onboard computer to an off-board computer using at least one of a wired communication device and a wireless communication device.

18. The method for testing of claim 13 wherein said first configurative structure and said second configurative structure are each one of the following types of configurative structure:

a first type of configurative structure, said first type of configurative structure including a nearly cylindrical element having a fore cylindrical end and an aft cylindrical end, said aft cylindrical end characterized by concavity;

a second type of configurative structure, said second type of configurative structure including a truncated conical element and axial fins projecting from said truncated conical element, said truncated conical element having a fore truncated conical end and an aft truncated conical end, said truncated conical element tapering toward said aft truncated conical end;

a third type of configurative structure, saide third type of configurative structure including a truncated conical element and a wheel, said truncated conical element having a fore truncated conical end and an aft truncated conical end, said truncated conical element tapering toward said aft truncated conical end, said wheel coaxially coupled with said truncated conical element at said aft truncated conical end.

19. The method for testing of claim 13 wherein said first configurative structure and said second configurative structure are the same type of configurative structure among the following types of configurative structure:

a first type of configurative structure, said first type of configurative structure including a nearly cylindrical element having a fore cylindrical end and an aft cylindrical end, said aft cylindrical end characterized by concavity;

a second type of configurative structure, said second type of configurative structure including a truncated conical element and axial fins projecting from said truncated conical element, said truncated conical element having a fore truncated conical end and an aft truncated conical end, said truncated conical element tapering toward said aft truncated conical end;

a third type of configurative structure, saide third type of configurative structure including a truncated conical element and a wheel, said truncated conical element having a fore truncated conical end and an aft truncated conical end, said truncated conical element tapering toward said aft truncated conical end, said wheel coaxially coupled with said truncated conical element at said aft truncated conical end.

20. The method for testing of claim 13 wherein said first configurative structure and said second configurative structure are different types of configurative structure among the following types of configurative structure:

a first type of configurative structure, said first type of configurative structure including a nearly cylindrical element having a fore cylindrical end and an aft cylindrical end, said aft cylindrical end characterized by concavity;

a second type of configurative structure, said second type of configurative structure including a truncated conical element and axial fins projecting from said truncated conical element, said truncated conical element having a fore truncated conical end and an aft truncated conical end, said truncated conical element tapering toward said aft truncated conical end;

a third type of configurative structure, said third type of configurative structure including a truncated conical element and a wheel, said truncated conical element having a fore truncated conical end and an aft truncated conical end, said truncated conical element tapering toward said aft truncated conical end, said wheel coaxially coupled with said truncated conical element at said aft truncated conical end.