IP Library Granted Patent US 10,345,271
Granted Patent B2
US 10,345,271 · App. 15/232,923 · Granted Jul 9, 2019

Modular film-covered elastomeric inspection device

Inventors: Michael R. Grosser (Serby, KS); Kendall Ford Koerner (Wellington, KS)
Assignee: Spirit AeroSystems, Inc.
G01N29/28G01N29/043G01N29/265G01N2291/0231G01N2291/106
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,345,271
App. No.
15/232,923
Granted
Jul 9, 2019
Kind
B2
Abstract

An inspection system for ultrasonic inspection of a part, such as an aircraft component. The inspection system may include one or more transducers, an acoustic coupler made of an acoustic coupling compliant solid, a low friction contact film, a location sensor, and a processor. The contact film may substantially surround the acoustic coupler or portions thereof. The transducers may transmit ultrasonic or sound waves through the acoustic coupler, the contact film, and at least partially through the part being inspected thereby. The location sensor may sense and output information regarding how far the ultrasonic inspection system has traveled along the part. The processor may associate signals from the transducers with signals from the location sensor to determine precise locations on the part at which particular signals are received by the transducers.

Claims (33)

1. An ultrasonic inspection system for ultrasonic inspection of a part having a surface, the system comprising:

at least one transducer, wherein the at least one transducer is configured to transmit ultrasonic or sound waves through the part;

an acoustic coupler made of an acoustic coupling compliant solid and fixed to a transmitting or a receiving portion of the transducer;

a low friction contact film substantially surrounding the acoustic coupler or portions of the acoustic coupler; and

an outrigger configured to be rigidly coupled to the at least one transducer so as to maintain normality of the at least one transducer to the surface of the part such that the at least one transducer transmits ultrasonic or sound waves through the part at an angle normal to the surface of the part, the outrigger being independently removable from the at least one transducer for accommodating a shape of the part.

2. The system of claim 1 , further comprising a modular housing attachable to the transducer and a contact film retainer attached to the modular housing.

3. The system of claim 1 , further comprising structure forming a boundary around at least a portion of the acoustic coupler for stabilizing the acoustic coupler.

4. The system of claim 1 , wherein the outrigger comprises wheels configured to rotate forward or aftward along the surface of the part during inspection of the part.

5. The system of claim 2 , further comprising a handle and a handle bracket attachable to the modular housing, wherein the handle is at least one of removeably, rotatably, and pivotally attached to the handle bracket.

6. The system of claim 1 , wherein the low friction contact film comprises at least one of polytetrafluoroethylene (PTFE), fluorinated ethylene propylene (FEP), and polyethylene (PE).

7. The system of claim 1 , wherein the acoustic coupling compliant solid is a low durometer solid couplant elastomer material.

8. The system of claim 1 , wherein the at least one transducer includes a linear array of transducers configured to at least one of send and receive ultrasonic waves through the part.

9. The system of claim 1 , further comprising a rotary encoder rotatably coupled with a resilient member and configured to provide location information regarding a distance the ultrasonic inspection system has traveled along the part.

10. An ultrasonic inspection system for ultrasonic inspection of a part having a surface, the system comprising:

at least one transducer configured to transmit ultrasonic or sound waves through the part;

an acoustic coupler made of an acoustic coupling compliant solid and fixed to the transducer;

a low friction contact film substantially surrounding the acoustic coupler or portions of the acoustic coupler;

a location sensor configured to sense and output information regarding how far the ultrasonic inspection system has traveled along the part;

a processor configured to associate signals from the at least one transducer with signals from the location sensor to determine precise locations on the part at which particular signals are received by the at least one transducer; and

an outrigger configured to be rigidly coupled to the at least one transducer so as to maintain normality of the at least one transducer to the surface of the part such that the at least one transducer transmits ultrasonic or sound waves through the part at an angle normal to the surface of the part, the outrigger being independently removable from the at least one transducer for accommodating a shape of the part.

11. The system of claim 10 , further comprising structure forming a boundary around at least a portion of the acoustic coupler for stabilizing the acoustic coupler.

12. The system of claim 10 , wherein the low friction contact film comprises at least one of polytetrafluoroethylene (PTFE), fluorinated ethylene propylene (FEP), and polyethylene (PE).

13. The system of claim 10 , wherein the acoustic coupling compliant solid is a low durometer solid couplant elastomer material.

14. The system of claim 10 , wherein the at least one transducer includes a linear array of transducers configured to at least one of send and receive ultrasonic waves through the part.

15. The system of claim 10 , wherein the location sensor includes a rotary encoder and a spring-biased engagement wheel rotatably coupled with the rotary encoder, wherein the engagement wheel is configured to freely roll along a surface of the part as the low-friction contact film is slid along the surface of the part, wherein the rotary encoder is actuated to rotate by rotation of the engagement wheel and is configured to provide location information regarding a distance the ultrasonic inspection system has traveled along the part.

16. A method for ultrasonic inspection of a part having a surface, the method comprising the steps of:

sliding a low friction contact film of an ultrasonic inspection system against a surface of the part, wherein the film is fixed to a transducer with an acoustic coupler made of an acoustic coupling compliant solid and positioned between the film and the transducer;

transmitting ultrasonic or sound waves from the transducer through the acoustic coupler and the film to the part;

receiving with the transducer, or a secondary transducer aligned on an opposing surface of the part, ultrasonic or sound waves reflected by or transmitted through the part;

determining one or more physical or structural characteristics or flaws of the part based on the ultrasonic or sound waves reflected by or transmitted through the part;

maintaining normality of the transducer to the surface of the part via an outrigger rigidly coupled to the transducer such that the transducer transmits the ultrasonic or sound waves through the part at an angle normal to the surface of the part; and

independently removing the outrigger from the transducer for accommodating a shape of the part.

17. The method of claim 16 , wherein the ultrasonic inspection system further includes a rotary encoder having a spring-biased attachment to a frame or a housing of the ultrasonic inspection system, wherein the rotary encoder is positioned to naturally rotate along the surface of the part during the step of sliding the low friction contact film against the surface of the part, wherein the method further comprises determining a distance or location of the ultrasonic inspection system on the part based on signals from the rotary encoder.

Assignments (15)
RELEASE OF SECURITY INTEREST Recorded Dec 11, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073932/0669 →
RELEASE OF SECURITY INTEREST Recorded Dec 10, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073900/0356 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073916/0346 →
SECURITY AGREEMENT Recorded Jul 8, 2024
From: SPIRIT AEROSYSTEMS, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 068217/0456 →
RELEASE OF SECURITY INTEREST Recorded Dec 4, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
To: SPIRIT AEROSYSTEMS, INC.; SPIRIT AEROSYSTEMS HOLDINGS, INC.; SPIRIT AEROSYSTEMS NORTH CAROLINA, INC.
Reel/Frame 065772/0456 →
SECURITY AGREEMENT (SECOND LIEN NOTES) Recorded Nov 21, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 065659/0585 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 061993/0847 →
RELEASE OF SECURITY INTEREST Recorded Nov 23, 2022
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 061995/0281 →
RELEASE OF SECURITY INTEREST Recorded Oct 28, 2020
From: BANK OF AMERICA, N.A.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 054230/0578 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 053993/0569 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053993/0505 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053983/0350 →
SECURITY INTEREST Recorded Apr 17, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 052433/0843 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Feb 24, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 052004/0929 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 10, 2016
From: GROSSER, MICHAEL R.; KOERNER, KENDALL FORD
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 039391/0888 →
Continuity (1)
Related Publication 20180045685A1 · Feb 15, 2018