Aircraft airframe assembly
First Claim
1. A method of producing a single, unitary, assembly tool (60), the assembly tool (60) being for assembling an assembly (6) comprising one or more components (8-20), the method comprising:
- providing at least a portion of a jig frame (62);
fixing one or more support plates (65) to the at least a portion of the jig frame (62);
machining the one or more support plates (65) such that a surface of each of the support plates (65) lies in a common plane (130);
positioning the at least a portion of the jig frame (62) such that the surfaces of the support plates (65) that lie in the common plane (130) are in contact with a supporting surface (138);
fixing one or more pickup device mounting plates (140a, 140b) to the at least a portion of the jig frame (62);
machining, with respect to the supporting surface (138), each of the pickup device mounting plates (140a, 140b) such that a pickup device receiving surface of that pickup device mounting plate (140a, 140b) has a respective predetermined position and orientation with respect to the supporting surface (138); and
fixing, to the pickup device receiving surface of each of the pickup device mounting plates (140a, 140b), a respective pickup device (66-72), each pickup device (66-72) having a receiving element (74-80) for receiving a component (8-20) of the assembly (6);
wherein the assembly (6) comprises at least one fuselage frame (8, 10, 12), and at least one longeron (14, 16, 18); and
whereby the receiving elements (74-80) of the single, unitary, assembly tool (60) are configured to hold the at least one fuselage frame (8, 10, 12) in an orientation with respect to the at least one longeron (14, 16, 18) for attachment of the at least one longeron (14, 16, 18) to the at least one fuselage frame (8, 10, 12).
1 Assignment
0 Petitions
Accused Products
Abstract
A method of producing an assembly tool (60) for assembling an assembly (6), the method comprising: providing at least a portion of a jig frame (62); fixing support plates (65) to the jig frame (62); machining the one or more support plates (65) such that a surface of each of the support plates (65) lies in a common plane (130); positioning the jig frame (62) such that the machined surfaces of the support plates (65) contact with a supporting surface (138); fixing pickup device mounting plates (140a, 140b) to the jig frame (62); machining, with respect to the supporting surface (138), the pickup device mounting plates (140a, 140b) such that a surface of each mounting plate (140a, 40b) has a respective predetermined position and orientation with respect to the supporting surface (138); and fixing, to the machined surfaces of the mounting plates (140a, 140b), a respective pickup device (66-72).
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Citations
10 Claims
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1. A method of producing a single, unitary, assembly tool (60), the assembly tool (60) being for assembling an assembly (6) comprising one or more components (8-20), the method comprising:
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providing at least a portion of a jig frame (62); fixing one or more support plates (65) to the at least a portion of the jig frame (62); machining the one or more support plates (65) such that a surface of each of the support plates (65) lies in a common plane (130); positioning the at least a portion of the jig frame (62) such that the surfaces of the support plates (65) that lie in the common plane (130) are in contact with a supporting surface (138); fixing one or more pickup device mounting plates (140a, 140b) to the at least a portion of the jig frame (62); machining, with respect to the supporting surface (138), each of the pickup device mounting plates (140a, 140b) such that a pickup device receiving surface of that pickup device mounting plate (140a, 140b) has a respective predetermined position and orientation with respect to the supporting surface (138); and fixing, to the pickup device receiving surface of each of the pickup device mounting plates (140a, 140b), a respective pickup device (66-72), each pickup device (66-72) having a receiving element (74-80) for receiving a component (8-20) of the assembly (6); wherein the assembly (6) comprises at least one fuselage frame (8, 10, 12), and at least one longeron (14, 16, 18); and whereby the receiving elements (74-80) of the single, unitary, assembly tool (60) are configured to hold the at least one fuselage frame (8, 10, 12) in an orientation with respect to the at least one longeron (14, 16, 18) for attachment of the at least one longeron (14, 16, 18) to the at least one fuselage frame (8, 10, 12). - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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Specification