Apparatus and methods for fabricating a helicopter main rotor blade
Abstract
An apparatus for fabricating a helicopter main rotor blade includes a compaction fixture for assembling and compacting blade subassembly components and a sheath spreading/insertion apparatus for spreading and inserting a leading-edge sheath onto in combination with the blade subassembly during the compaction process. The compaction fixture includes a lower assembly having a contoured upper airfoil nest mounted in combination with a support structure and an upper assembly having a pressure bag affixed in sealed combination to a contoured backplate affixed in combination to a structural support truss. With the upper and lower assemblies in locked combination, the pressure bag is pressurized to compact the assembled blade subassembly components. The sheath spreading/insertion apparatus includes a movable stanchion, upper first and lower second elongate carriage members mounted in synchronized movable combination with the stanchion, and a row of suction cups mounted in combination with each carriage member. Pneumatic cylinders are mounted in combination with the stanchion and the respective carriage members. Pressurization of the pneumatic cylinders causes synchronized movement of the upper first and lower second carriage members between a disengaged position wherein the leading-edge sheath can be inserted between the upper first and lower second rows of suction cups, an engaged position wherein the suction cups abuttingly engage respective OML surfaces of the leading-edge sheath and an operating position wherein the leading-edge sheath is spread apart for insertion onto in combination with the blade subassembly during compaction thereof. A vacuum source is pneumatically interconnected to the suction cup to generate suction forces therein in the engaged position to cause the suction cups to hold the respective OML surfaces of the leading- edge sheath such that subsequent synchronized movement of the first and second carriage members to the operating position causes the leading - edge sheath to be spread apart. Movement of the stanchion causes the spread - apart leading - edge sheath to be inserted in combination with the blade subassembly during compaction thereof.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1. A sheath spreading/insertion positioning apparatus for spreading a leading-edge sheath and for inserting positioning the spread-apart leading-edge sheath in combination with relation to a blade subassembly, comprising:
a movable stanchion;
an uppera first elongate carriage member mounted in movable combination with said movable stanchion;
a plurality of suction cups mounted in combination with said upper first elongate carriage member;
a lower second elongate carriage member mounted in movable combination with said movable stanchion;
a plurality of suction cups mounted in combination with said lower second elongate carriage member;
means for imparting synchronized movement to said upper first and lower second elongate carriage members between a disengaged position wherein the leading-edge sheath member may be inserted between said pluralities of suction cups mounted in combination with said upper first and lower second elongate carriage members without contact therewith, an engaged position wherein said pluralities of suction cups abuttingly engage respective OML surfaces of the leading-edge sheath, and an operating position wherein the leading-edge sheath is spread apart for insertion onto positioning in relation to the blade subassembly;
means for generating suction forces in said pluralities of suction cups in the engaged position to cause said suction cups to hold the respective OML surfaces of the leading-edge sheath such that subsequent synchronized movement of said upper first and lower second elongate carriage members to the operating position causes the leading-edge sheath to be spread apart; and
means for moving said movable stanchion imparting relative movement between the spread- apart leading - edge sheath and the blade subassembly to insert position the spread-apart leading-edge sheath onto in relation to the blade subassembly.
2. The sheath spreading/insertion positioning apparatus of claim 1 further comprising means for indicating that the spread-apart leading-edge sheath has been fully inserted onto positioned in relation to the blade subassembly.
3. The sheath spreading/insertion positioning apparatus of claim 1 wherein said synchronized movement imparting means comprises:
a plurality of pneumatic cylinders mounted in combination with said upper first elongate carriage member and said movable stanchion;
a plurality of pneumatic cylinders mounted in combination with said lower second elongate carriage member and said movable stanchion; and
a pressure source fluidically interconnected to said pluralities of pneumatic cylinders;
actuation of said pressure source providing pressurized air to said pluralities of pneumatic cylinders to cause synchronized movement of said upper first and lower second elongate carriage members between said disengaged position wherein the leading-edge sheath may be inserted between said pluralities of suction cups mounted in combination with said upper first and lower second elongate carriage members without contact therewith, said engaged position wherein said pluralities of suction cups abuttingly engage respective OML surfaces of the leading-edge sheath, and said operating position wherein the leading-edge sheath is spread apart for insertion onto positioning in relation to the blade subassembly.
4. The sheath spreading/insertion positioning apparatus of claim 1 wherein said plurality of suction cups mounted in combination with said upper first elongate carriage member comprises ninety suction cups, and wherein said plurality of suction cups mounted in combination with said lower second elongate carriage member comprises ninety suction cups.Cited by (0)
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