Automated fiber placement with course trajectory compensation
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B29C-070/02
B29C-070/38
G06F-017/50
B29L-031/30
출원번호
US-0406972
(2017-01-16)
등록번호
US-9862153
(2018-01-09)
발명자
/ 주소
Yarker, Thomas
Hasenjaeger, William H.
출원인 / 주소
CGTech
대리인 / 주소
Knobbe, Martens, Olson & Bear, LLP
인용정보
피인용 횟수 :
0인용 특허 :
74
초록▼
Various automated fiber placement systems and methods are disclosed. The system can determine steerable paths for the application of a composite material over highly contoured surfaces. The system can determine when a course trajectory would violate a steering limitation (e.g., a maximum bendability
Various automated fiber placement systems and methods are disclosed. The system can determine steerable paths for the application of a composite material over highly contoured surfaces. The system can determine when a course trajectory would violate a steering limitation (e.g., a maximum bendability of the composite material) and can adjust the trajectory to avoid such violations. The adjustment can create gaps between adjacent courses, which can have a generally flared peripheral shape. The system can fill such gaps with subsequent courses of the composite material. Thus, the system can automatically apply composite material to highly contoured surfaces while also avoiding violation of the steering limitations.
대표청구항▼
1. A system for determining course trajectories for the application of tows of composite material to a curved surface using an automated fiber placement machine, the system comprising: a data repository that stores data related to the shape and dimensions of the surface and that stores an indication
1. A system for determining course trajectories for the application of tows of composite material to a curved surface using an automated fiber placement machine, the system comprising: a data repository that stores data related to the shape and dimensions of the surface and that stores an indication of a comfortable steering limitation and an indication of a length limitation; anda computing system comprising one or more computing devices, the computing system in communication with the data repository and programmed to: produce a plurality of generally parallel path course trajectories for application of the tows to the curved surface;determine, for each of the plurality of generally parallel path course trajectories, whether any of the tows would violate the comfortable steering limitation;determine, for at least one of the generally parallel path course trajectories in which any of the tows would violate the comfortable steering limitation, whether to make a course adjustment, wherein the determination of whether to make a course adjustment comprises comparing the length of the portion of the tow that violates the comfortable steering limitation to the length limitation; andadjust, in response to determining to make a course adjustment, the trajectory of the least one of the generally parallel path course trajectories in which any of the tows would violate the comfortable steering limitation to a flared path course trajectory, the flared path course trajectory intentionally diverging from the trajectory of an adjacent course, thereby creating a gap between the flared path course and the adjacent course. 2. The system of claim 1, wherein the computing system is further programmed to produce at least one additional course trajectory located in the gap. 3. The system of claim 2, wherein the comfortable steering limitation comprises a maximum amount an individual tow is permitted to bend on the surface. 4. The system of claim 2, wherein the comfortable steering limitation corresponds approximately to a maximum amount an individual tow can bend without incurring a flawing event. 5. The system of claim 1, wherein comparing the length of the portion of the tow that violates the comfortable steering limitation to the length limitation comprises determining whether the length of the portion of the tow that violates the comfortable steering limitation is greater than or equal to the length limitation. 6. The system of claim 1, wherein the adjustment of the course trajectory to the flared path course trajectory comprises: determining a tow in the particular course trajectory that is located laterally farthest from an adjacent and previous course;determining, for the tow located laterally farthest from the adjacent and previous course, the longest segment of the tow that complies with the comfortable steering limitation;determining a curve that approximates the longest segment of the tow; andplotting a flared path course trajectory having the curve as the centerline. 7. A computer implemented method of controlling an automated fiber placement machine configured to apply a plurality of layers of courses of composite material to a form, each course comprising a plurality of tows, the method comprising, under the control of one or more processors: determining a plurality of generally parallel course trajectories over the form, the plurality of generally parallel courses trajectories being in the same layer;identifying a course to be adjusted, wherein identifying the course to be adjusted comprises: identifying at least one of the plurality of generally parallel course trajectories that has a tow that would violate a comfortable steering limitation;determining, for the tow that would violate the comfortable steering limitation, the length of the portion of the tow that would violate the comfortable steering limitation for greater than a length limitation; andadjusting the trajectory of the course to be adjusted to include a flared path trajectory portion,wherein, in flared path trajectory portion, all of the tows diverge from an adjacent one of the generally parallel path course trajectories, thereby creating a gap between the tows in the flared path trajectory portion and the tows of the adjacent generally parallel path course trajectory. 8. The method of claim 7, further comprising producing at least one additional course trajectory to fill at least a portion of the gap, the additional course trajectory being in the same layer as the flared path course trajectory. 9. The method of claim 8, wherein the additional course trajectory is generally parallel to the flared path trajectory portion. 10. The method of claim 8, wherein the additional course trajectory is generally parallel to the adjacent one of the generally parallel path course trajectories. 11. The method of claim 7, wherein the comfortable steering limitation comprises a maximum amount an individual tow is permitted to bend on the form. 12. The method of claim 7, wherein the steering limitation corresponds approximately to a maximum amount an individual tow can bend without incurring a flawing event. 13. A computing system configured to implement a process comprising: receiving dimensional data for a contoured surface on which a plurality of layers of composite material are to be applied, each of the layers comprising a plurality of courses, each course comprising a plurality of tows;producing a plurality of course trajectories over the surface in the same layer, the course trajectories being generally parallel to each other;determining that at least one of the course trajectories comprises a steering violation, the steering violation occurring when a steering radius of any of the tows of the at least one course trajectory is less than a comfortable steering radius, the comfortable steering radius being related to the ability of an individual tow to traverse a curve;determining a length of the steering violation for the at least one course trajectory; andin response to determining that the length of the steering violation is greater than or equal to a length limitation, replacing the portion of the least one course trajectory that comprises the steering violation with a flared path trajectory, the flared path trajectory being non-parallel with the generally parallel path course trajectories. 14. The system of claim 13, further comprising producing at least one additional course trajectory to fill at least some of a gap between the flared path trajectory and an adjacent one of the generally parallel path course trajectories, the additional course trajectory being in the same layer as the flared path trajectory. 15. The system of claim 13, wherein the computing system is in communication with a data repository. 16. The system of claim 15, wherein the data repository stores dimensional data for the contoured surface, the comfortable steering radius, and the length limitation. 17. The system of claim 13, wherein the computing system is in communication with a user input. 18. The system of claim 13, wherein the comfortable steering radius corresponds approximately to a minimum radius of curvature around which a given tow can bend on the surface. 19. The system of claim 13, further comprising: determining, over the length of the steering violation, an average steering radius of the tows; andin response to determining that the average steering radius is less than or equal to the comfortable steering radius, replacing the portion of the least one course trajectory that comprises the steering violation with the flared path trajectory.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (74)
McCowin, Peter D.; Jones, Darrell D.; Banks, David P.; Zenkner, Grant C., Apparatus and method for composite material trim-on-the-fly.
Senibi, Simon D.; Rassaian, Mostafa; Huizenga, Richard N.; Lewis, Gilbert L.; Waugh, Jeffery L.; Dondlinger, Leo E., Automated fiber placement including layup mandrel tool.
Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures.
Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections.
Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections.
Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures, and methods for systems for manufacturing such barrel sections.
Chapman, Michael R.; Watson, Robert M.; Anderson, Donald A.; Piehl, Marc J.; Sweetin, Joseph L.; Grose, Douglas L., Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections.
Chapman, Michael R.; Watson, Robert M.; Anderson, Donald A.; Piehl, Marc J.; Sweetin, Joseph L.; Grose, Douglas L., Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections.
Chapman,Michael R.; Watson,Robert M.; Anderson,Donald A.; Piehl,Marc J.; Sweetin,Joseph L.; Grose,Douglas L., Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections.
Harvey,James L.; Harris,Douglas G.; Brown,James M.; Hatch,Boyd, Fiber redirect system, multi-axis robotic wrist and fiber placement apparatus incorporating same and related methods.
Guzman, Juan Carlos; McCarville, Douglas Alan; Sweetin, Joseph L.; Messinger, Ross, Method and apparatus for producing contoured composite structures and structures produced thereby.
Venkataramani Venkat Subramaniam (Clifton Park NY) Smith Lowell Scott (Niskayuna NY), Method for fabricating lamellar piezoelectric preform and composite.
McCarville, Douglas A.; Stickler, Patrick B.; Guzman, Juan C.; Noel, Jennifer S.; Sweetin, Joseph L., Method for producing contoured composite structures and structures produced thereby.
Hawkins, Robert D.; Willden, Kurtis S.; Modin, Andrew E.; Depase, Edoardo; Glain, Michael L.; Mussi, Benjamin Adam; Kismarton, Max U., Method of laying up prepreg plies on contoured tools using a deformable carrier film.
Brennan, Joseph Daniel; Atsebha, Solomon T.; Dorsey Palmateer, John W.; Anderson, Patrick L., Methods and systems for automated ply boundary and orientation inspection.
Shair, Sultan; O'Flynn, Julian Thomas; Messmer, Mathias; Worthoff, Frank; Ostojic, Mile; Vermilyea, Mark E., Methods and systems for automated ply layup for composites.
Boyl-Davis, Theodore M.; Jones, Darrell Darwin; Valenzuela, Dario I., Methods and systems for processing surface data for the manufacturing of optimum fit mating parts.
Hagman, Thomas J.; Branch, Gregory Lowman; Dwyer, James P.; Hood, Brian Edward; Lund, Erik; Morris, Wade Matthew; Schwedhelm, Jonathan Richard; Stone, Thomas C., Methods for laminating composites.
Chapman, Michael R.; Watson, Robert M.; Anderson, Donald A.; Piehl, Marc J.; Sweetin, Joseph L.; Grose, Douglas L., Methods for manufacturing composite sections for aircraft fuselages and other structures.
Brennan, Joseph D.; Hempstead, George D.; Jones, Darrell D.; Lum, Matthew K.; McCowin, Peter D.; Rowe, Terrence J.; Schlosstein, Hugh R., Pre-patterned layup kit and method of manufacture.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.