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[0001] The present invention relates to an improved automated method and apparatus for finishing aircraft panel surfaces and more particularly to an improved automated method of aircraft surface finishing for aircraft wings and fuselage.
[0002] Conventional surface finishing of aircraft panels, such as fuselage and wing panels is typically accomplished through manual sanding, polishing and other related processes. Traditional machining and forming processes include creep forming, hot forming, break forming, stretch forming, shot peen forming and super elastic forming which typically require surface improvement techniques in order to remove burrs, parting lines, scratches, tool marks and the like in order to reduce surface roughness.
[0003] In a first preferred embodiment according to the present invention, there is provided an apparatus for surface finishing of aircraft panels comprising a retaining means for retaining a panel to be processed, a surface panel processing means for acting on a panel retained by the retaining means, the surface processing means being movable about a plurality of axes relative to the panel to present the processing means to act on the surface contour of the panel, means for effecting relative movement between the retaining means and the surface processing means and control means for controlling said surface panel processing means in combination with said means for effecting relative movement.
[0004] In another embodiment according to the above, wherein the device further includes scanning means.
[0005] In another embodiment having the above structures, the scanning means includes panel scanning means to for scanning for surface anomalies, wherein the scanning means is adapted to generate an output control signal to actuate and control the surface finishing means whereby the finishing means is actuated to correct the surface anomalies.
[0006] In another embodiment according to any of the above structures, there is provided means to generate a first control signal relative to different locations of anomalies on the panel, the output control signal being adapted to control relative movement between the finishing means and the mounted panel for positioning the finishing means at different locations about the panel.
[0007] In a second embodiment according to the present invention, there is provided an improvement in a method of surface finishing of an aircraft panel comprising providing an aircraft panel to be surface finished, mounting the panel in a fixed position, providing finishing means for surface finishing the panel, effecting relative movement between the finishing means and the mounted panel, in which the improvement includes the steps of detecting surface anomalies in the panel, generating a data-input control signal based on the surface anomalies; and generating a data output control signal to actuate the finishing means to act on the anomalies.
[0008] In another embodiment, there is provided a method according to the above wherein the improvement includes the steps of scanning a defined area of the panel with scanning means to generate the data input control signal relative to the surface anomalies, and generating an output control signal to actuate and control the finishing means whereby the finishing means is actuated to correct the surface anomalies.
[0009] In another embodiment there is provided a method according to any of the above methods wherein the improvement includes the step of generating a first control signal relative to different locations of anomalies on the panel, the output control signal being adapted to control relative movement between the finishing means and the mounted panel for positioning the finishing means at different locations about the panel.
[0010] In any ofthe above embodiments, suitable scanning means and control means are utilized as are known in the field.
[0011]
[0012]
[0013]
[0014] With reference to the drawing figures, there is illustrated a preferred form of a device for the automated surface finishing of aircraft panels depicted generally by reference numeral
[0015] In a preferred embodiment, the device includes a controller or programmable control means
[0016] In a preferred embodiment, the device
[0017] The scanning device or sensor means
[0018] Surface finish sensors or scanning means
[0019] The robot or surface processor
[0020] Tools
[0021] The robot or surface processor
[0022] In use, the robot end effector
[0023] In use, the panel or part
[0024] In an alternative embodiment as illustrated in
[0025] As illustrated in
[0026] The robot
[0027] In an alternative embodiment, sensor means
[0028] In a further alternative embodiment, the controller
[0029] In various alternatives embodiments, sensor means
[0030] In another alternative embodiment, additional robots or surface processors may be positioned within the device
[0031] In a further alternative embodiment, head pressure may be controlled through air pressure or other like drive means.
[0032] In various versions according to the present invention, the device
[0033] In various embodiments, the aircraft panel
[0034] Although embodiments of the invention have been described above, it is not limited thereto and it will be apparent to those skilled in the art that numerous modifications form part of the present invention insofar as they do not depart from the spirit, nature and scope of the claimed and described invention.