Apparatus for Automated Maintenance of Aircraft Structural Elements
First Claim
1. An automated apparatus for moving an end effector over a surface of an airfoil-shaped body having leading and trailing edges, comprising:
- a chassis comprising leading and trailing edge subassemblies which are movable relative to each other to change a state of said chassis from a first state to a second state;
a plurality of rolling elements rotatably mounted to said leading and trailing edge subassemblies, said plurality of rolling elements being situated so that said airfoil-shaped body cannot be engaged with a gripping force when said chassis is in said first state and being situated so that said airfoil-shaped body can be engaged with a gripping force when said chassis is in said second state;
a first actuator coupled to rotate one of said plurality of rolling elements when activated;
a support assembly coupled to and displaceable along said chassis;
a second actuator coupled to displace said support assembly when activated;
an end effector coupled to and carried by support assembly; and
a third actuator coupled to actuate operation of said end effector when activated.
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Accused Products
Abstract
Automated apparatus for performing maintenance functions on airfoil-shaped bodies having short chord lengths, the apparatus being movable in a spanwise direction along the airfoil-shaped body. In accordance with various embodiments, the apparatus comprises a blade crawler capable of supporting any one of a plurality of end effectors for performing a set of maintenance functions on an airfoil-shaped body, such as a blade component. Included in these functions are multiple options for nondestructive inspection, drilling, grinding, fastening, appliqué application, scarfing, ply mapping, depainting, cleaning, and painting devices that are attached as the end effector for the blade crawler. As a whole, the blade crawler reduces maintenance time, labor hours and human errors when robotic maintenance functions are performed on blade components.
91 Citations
21 Claims
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1. An automated apparatus for moving an end effector over a surface of an airfoil-shaped body having leading and trailing edges, comprising:
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a chassis comprising leading and trailing edge subassemblies which are movable relative to each other to change a state of said chassis from a first state to a second state; a plurality of rolling elements rotatably mounted to said leading and trailing edge subassemblies, said plurality of rolling elements being situated so that said airfoil-shaped body cannot be engaged with a gripping force when said chassis is in said first state and being situated so that said airfoil-shaped body can be engaged with a gripping force when said chassis is in said second state; a first actuator coupled to rotate one of said plurality of rolling elements when activated; a support assembly coupled to and displaceable along said chassis; a second actuator coupled to displace said support assembly when activated; an end effector coupled to and carried by support assembly; and a third actuator coupled to actuate operation of said end effector when activated. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. An automated apparatus for moving an end effector over a surface of an airfoil-shaped body having leading and trailing edges, comprising:
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a first support assembly comprising a forward body part, a rearward body part, and an intercostal element that interconnects said forward and rearward body parts, at least one of said forward and rearward body parts being displaceable along an axis of said intercostal element to facilitate adjustment of a distance separating said forward and rearward body parts; a first drive motor carried by said forward body part; a drive mechanism coupled to and depending from an output shaft of said drive motor and arranged to contact the airfoil-shaped body; a rolling element supported by said rearward body part and arranged to contact the airfoil-shaped body; a biasing mechanism coupled to said intercostal element and one of said forward and rearward body parts for exerting a force that urges said drive mechanism and said rolling element to grip the airfoil-shaped body; a guide element supported by said first support assembly; a second support assembly which is mounted on and displaceable along said guide element; and an end effector coupled to and carried by said second support assembly, wherein said first support assembly is displaceable in a spanwise direction along the airfoil-shaped body when said drive mechanism is driven by said drive motor, and said end effector is displaceable in a chordwise direction independent of spanwise displacement of said first support assembly. - View Dependent Claims (15)
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- 16. An apparatus comprising a ladder, a frame member attached to said ladder, a height adjustment mechanism comprising a lower part attached to said ladder and an upper part which is coupled to said lower part of said height adjustment mechanism, a pair of cable pay-out rollers rotatably coupled to said frame member, and a grip attached to said upper part of said height adjustment mechanism, wherein said grip is configured to engage and stabilize a tip of a rotorcraft blade, and the height of said upper part of said height adjustment mechanism is adjustable by movement relative to said lower part.
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18. A system comprising:
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an airfoil-shaped body having leading and trailing edges which extend from a root to a tip; a tip support assembly comprising a frame, a height adjustment mechanism comprising a lower part attached to said frame and an upper part which is coupled to said lower part of said height adjustment mechanism, first and second cable pay-out rollers rotatably coupled to said frame, and a grip attached to said upper part of said height adjustment mechanism and coupled to said tip of said airfoil-shaped body, wherein the height of said upper part of said height adjustment mechanism is adjustable by movement relative to said lower part; an automated blade crawler mounted to said airfoil-shaped body, said automated blade crawler comprising an end effector, first means for moving said blade crawler in a spanwise direction along said airfoil-shaped body, and second means for moving said end effector in a chordwise direction; and a cable having one end connected to said automated blade crawler and having another portion disposed between said first and second cable pay-out rollers. - View Dependent Claims (19, 20)
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21. An automated crawler configured to be mountable on a rotorcraft blade and capable of spanwise travel along the rotorcraft blade, comprising an end effector configured to perform a maintenance function.
Specification