Rope saw cutting apparatus and method for scarfing composites
AssigneeThe Boeing Company
InventorsEverett A. Westerman, Jr., Philip E. Roll
Life of this patent
Estimating the term…
Abstract
A rope saw cutting apparatus is partially insertable through a bore in a composite panel to scarf the panel without access to the blind side of the panel. The same apparatus can also be used to prepare a tapered repair plug to close tolerance to repair the scarfed panel. The apparatus preferably uses a rope saw blade to perform a plunge cut followed by a circumferential cut which has a desired taper or scarf angle.
Claims26
A cutting apparatus for trimming a damaged area of a composite structure panel for subsequent repair, comprising:
- a frame member for contacting a first side of the panel;
- a foldable reaction member for contacting a second side of the panel;
- a tension member rotatably connected between the frame and the reaction members for tightening the panel between the frame and reaction members;
- and
- a saw connected to the tension member, the saw having a blade and a folding mechanism for moving the blade between folded position for insertion of at least a portion of the saw along with a portion of the reaction member through an aperture in the panel and an unfolded position for performing a plunge cut into the panel, whereupon subsequent rotation of the tension member cuts out a plug from the panel.
A rope saw cutting apparatus for trimming out a damaged area of a composite structure panel for subsequent repair, comprising:
- frame means for contacting an exposed side of the panel to be repaired;
- reaction means for contacting an opposite side of the panel;
- tension means rotatably connected between the frame and the reaction means for holding the panel between the frame and reaction means;
- and
- a collapsible saw having a rope saw blade, the saw having a folding mechanism for moving the blade between a folded position for insertion of at least a portion of the saw through an aperture in the panel and an unfolded position for performing a plunge cut into the panel, so that subsequent rotation of the tension means cuts out a plug from the panel.
A rope saw cutting apparatus for cutting a substantially frustoconic section from a first composite panel for use as a repair plug having a complementary scarf angle for mating with a scarf angle in a trimmed area of a second composite panel, the apparatus comprising:
- a frame member;
- a saw support member rotatably connected to the frame member for supporting a rope saw and for rotating the supported rope saw up to 360.degree. about the support member's longitudinal axis;
- and
- a saw having a rope saw blade pivotally connected to the saw support member, the saw having a folding mechanism for moving the blade between a folded position preparatory to making a plunge cut in the first panel to a desired depth and angle and an unfolded position for performing the plunge cut and for performing a substantially frustoconic cut, the unfolded position orienting the blade at an angle relative to the first panel corresponding to the complementary scarf angle whereupon subsequent rotation of the saw support member about its axis up to 360.degree. causes the saw to cut the section.
A method for scarfing a damaged area of a substantially closed surface in a composite structure panel for subsequent repair, comprising the steps of:
- forming an aperture in the panel around the damaged area and to define a rotation axis;
- positioning a frame member of a cutting apparatus against an exposed side of the panel;
- passing a fodable reaction member of the apparatus in a substantially folded condition through the aperture;
- unfolding the reaction member so that portions of the reaction member extend radially beyond the aperture;
- drawing the frame member and reaction member towards one another so as to hold the panel therebetween;
- pivoting a cutting apparatus into the panel, thereby making a plunge cut to a desired depth and at a desired scarf angle;
- and
- rotating the cutting apparatus about the rotation axis, thereby cutting a plug from the panel.
Dependencies are inferred from the claim text.