Methods and systems for automated ply boundary and orientation inspection
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G06F-015/00
B32B-038/00
출원번호
UP-0836242
(2007-08-09)
등록번호
US-7555404
(2009-07-09)
발명자
/ 주소
Brennan, Joseph Daniel
Atsebha, Solomon T.
Dorsey Palmateer, John W.
Anderson, Patrick L.
출원인 / 주소
The Boeing Company
대리인 / 주소
Armstrong Teasdale LLP
인용정보
피인용 횟수 :
22인용 특허 :
28
초록▼
A method for determining the positional laydown accuracy of an automated lamination machine during fabrication of a multiple layered part is described. The method includes measuring a position of a placement head of the lamination machine in a coordinate system, determining a location of a ply edge
A method for determining the positional laydown accuracy of an automated lamination machine during fabrication of a multiple layered part is described. The method includes measuring a position of a placement head of the lamination machine in a coordinate system, determining a location of a ply edge with respect to the placement head, transforming the location of the ply edge into the coordinate system, based on the measured head position, transforming the location of the ply edge from the coordinate system into a second coordinate system that is associated with the part being fabricated, and comparing actual ply edge location in the second coordinate system to an expected ply edge location defined in the second coordinate system, the second coordinate system associated with the part being fabricated, to determine the laydown accuracy of the machine.
대표청구항▼
What is claimed is: 1. A method for determining the positional laydown accuracy of an automated lamination machine during fabrication of a single or multiple layered part, said method comprising: determining a position of a placement head of the lamination machine in a coordinate system; determinin
What is claimed is: 1. A method for determining the positional laydown accuracy of an automated lamination machine during fabrication of a single or multiple layered part, said method comprising: determining a position of a placement head of the lamination machine in a coordinate system; determining a location of a ply edge with respect to the placement head using a machine vision system; transforming, with a processing device, the location of the ply edge into the coordinate system, based on the placement head position; transforming the location of the ply edge from the coordinate system into a second coordinate system that is associated with the part being fabricated; comparing actual ply edge location in the second coordinate system to an expected ply edge location defined in the second coordinate system, the second coordinate system associated with the part being fabricated; and determining the laydown accuracy of the machine based on the comparison. 2. A method according to claim 1 wherein determining a location of a ply edge comprises: operating a machine based vision system, the position of which is known with respect to the placement head, to project at least one laser line at an acute angle to the surface tangent and of known positional relationship to the vision system onto a surface of the part being fabricated; utilizing discontinuities in the projected at least one laser line to determine where, within a frame of reference for the vision system, the edges of plies are being laid; and correlating the frame of reference for the vision system to the surface of the part being fabricated. 3. A method according to claim 2 wherein correlating the frame of reference for the vision system to the surface of the part comprises: defining a mounting position of a plurality of proximity sensors with respect to the vision system; projecting, utilizing the plurality of proximity sensors, onto the surface of the part, signals that substantially correlate to the field of view of the vision system; and correlating the position of the projected symbols on the part being fabricated to the defined mounting positions of the proximity sensors. 4. A method according to claim 3 wherein transforming the location of the ply edge into the independent coordinate system comprises interpolating a three dimensional coordinate position for each laser line discontinuity relative to a position of the placement head. 5. A method according to claim 1 wherein determining a position of the placement head in an independent coordinate system comprises: defining a mounting position of the plurality of laser tracking devices with respect to the placement head of the lamination machine; receiving distances between the placement head and each respective laser tracking device; and correlating the distances received from the laser tracking devices with their mounting positions to determine a position of the placement head. 6. A method according to claim 5 further comprising utilizing a gyroscope to provide an orientation of the placement head. 7. A method according to claim 1 further comprising measuring an orientation and rotation of a mandrel associated with the part being fabricated utilizing at least one of an encoder, a global positioning system, and a tracking interferometer. 8. An automated fiber placement (AFP) machine comprising: an AFP head; at least one positioning device configured to provide a position of said AFP head within a coordinate system; and a vision system configured to determine an edge placement of a ply of fiber material as the material is placed by said AFT head, said machine programmed to calculate a position of the edge of the ply based on a position of said vision system with respect to said AFP head, and transform the position from the coordinate system associated with said AFP head to a coordinate system associated with a part fabricated by said machine. 9. An AFP machine according to claim 8 further configured to compare a determined ply edge location in the coordinate system associated with the part fabricated to an expected ply edge location defined in the coordinate system associated with the part being fabricated to determine an accuracy of machine placement. 10. An AFP machine according to claim 8 wherein said at least one positioning device comprises: a plurality of tracking devices each at a known position within the coordinate system associated with said AFP head; and a plurality of reflective devices mounted on said AFP head, said tracking devices configured to track a position of said AFP head within the coordinate system based on reflections received from said reflective devices. 11. An AFP machine according to claim 10 wherein said plurality of tracking devices are configured to provide a three dimensional location of a respective said reflective device, positions of said reflective devices referenced to said AFP head. 12. An AFP machine according to claim 10 wherein said at least one positioning device comprises a gyroscope configured to provide orientation data, said machine operable to correlate the received orientation from said gyroscope, and data from said tracking devices, to provide a position and orientation within the coordinate system for said AFP head. 13. An AFP machine according to claim 10 wherein said at least one positioning device comprises a global positioning system (GPS), said machine operable to correlate the received position from said GPS, and data from said tracking devices, to provide a position and orientation within the coordinate system for said AFP head. 14. An AFP machine according to claim 8 further comprising a laser source, wherein to determine edge placement, said laser source is configured to project at least one laser line of known positional relationship to said vision system, the projection across the center of the field of view of said vision system such that a discontinuity, indicative of the edge of a ply, can be discerned by said vision system, and a location of said discontinuity calculated by said machine. 15. An AFP machine according to claim 14 configured to measure a position of said AFP head with respect to a part mandrel associated with said machine. 16. An AFP machine according to claim 8 further comprising a plurality of proximity sensors, said proximity sensors in known positions with respect to said AFP head and dispersed such that in combination, projections from said proximity sensors onto the part fabricated by said machine substantially define the field of view of said vision system. 17. An AFP machine according to claim 16, said machine configured to receive a distance measurement from each of said proximity sensors, said machine further comprising a laser source configured to project at least one laser line of known positional relationship to said vision system across the center of the field of view of said vision system such that a discontinuity, indicative of the edge of a ply, can be discerned by said vision system, said machine further configured to: correlate the distances with a known position for each of said proximity sensors; interpolate a three dimensional coordinate position for each laser line discontinuity relative to said AFP head. 18. An AFP machine according to claim 8 further comprising an encoder configured to output data relating to a rotational position of a mandrel associated with the part relative to said plurality of laser tracking devices. 19. A method for determining a position, within a coordinate system, for an edge of a ply of fiber material placed on a part mandrel, said method comprising: determining, utilizing a plurality of tracking devices having a known position in the coordinate system, distances to a placement head; receiving an orientation of the placement head from an inertial device; calculating a position and orientation in space for the placement head from the orientation, distances, and known positions; identifying, utilizing a vision system, an edge for the fiber material, a position of the vision system based on the position of the placement head; determining an orientation of the vision system with respect to the part mandrel; and calculating a position of the identified edge based on the position of the placement head and the orientation of the vision system. 20. A method according to claim 19 wherein determining distances to a placement head comprises measuring the distances to respective reflective devices, the reflective devices being of known position with respect to the placement head. 21. A method according to claim 19 wherein receiving an orientation of the placement head comprises receiving pitch, roll, and yaw data from a gyroscope, the gyroscope being of known position with respect to the placement head. 22. A method according to claim 19 further comprising receiving a rotational position of the part mandrel relative to said plurality of laser tracking devices. 23. A method according to claim 19 wherein determining an orientation of the vision system with respect to the part mandrel comprises: measuring distances to the part mandrel utilizing a plurality of sensors, the sensors dispersed in a known position with respect to the placement head, projections from the sensors within a field of view of the vision system; and interpolating a three dimensional coordinate position for the identified edge relative to the placement head.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (28)
Kiang Meng-Hsiung ; Lau Kam Y. ; Muller Richard S. ; Solgaard Olav, Apparatus and method for optical scanning with an oscillatory microelectromechanical system.
Brockman John P. (Cincinnati OH) Carman Robert A. (Cincinnati OH) Swope David C. (North Bend OH) Neal Norman D. (Loveland OH) Wiebe Harold D. (Springdale OH), Intelligent servo-controlled fiber placement machine tensioner.
Engelbart,Roger W; Hannebaum,Reed; Schrader,Steve; Holmes,Scott T; Walters,Craig, Systems and method for identifying foreign objects and debris (FOD) and defects during fabrication of a composite structure.
Dorris, Steven A.; Ayyagari, Arun; Vance, Jonathan Blake; Corman, David E.; Fonda, James W.; Engelbart, Roger W.; Freeman, Philip L., Composite inspection and structural check of multiple layers.
Georgeson, Gary Ernest; Griess, Kenneth Harlan, Process for inhibiting galvanic corrosion of an aluminum structure connected, without using a splice plate, to a composite structure having a fiber including graphite.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.