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An array of blades for use in an engine includes a disk having a slot, a pair of rails adjacent the slot and extending above an upper surface of the slot, and a pair of shoulders located outside the rails. A plurality of radially loaded blades are inserted into the slot. A plurality of snaps overhan

An array of blades for use in an engine includes a disk having a slot, a pair of rails adjacent the slot and extending above an upper surface of the slot, and a pair of shoulders located outside the rails. A plurality of radially loaded blades are inserted into the slot. A plurality of snaps overhang the rails and rest on the shoulders. Each of the blades is positioned between a pair of snap seals and overlaps a side edge of each one of the pair of snap seals.

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1. An array of blades for use in an engine comprising: a disk having a slot, a pair of rails adjacent the slot and extending above an upper surface of said slot, and a pair of shoulders located outside said rails;a plurality of radially loaded blades inserted into said slot;a plurality of snap seals

1. An array of blades for use in an engine comprising: a disk having a slot, a pair of rails adjacent the slot and extending above an upper surface of said slot, and a pair of shoulders located outside said rails;a plurality of radially loaded blades inserted into said slot;a plurality of snap seals which overhang said rails and rest on said shoulders; andeach of said blades being positioned between a pair of snap seals and overlapping a side edge of each one of said pair of snap seals. 2. The array of claim 1, wherein: said slot is a tangential slot;each of said rails has an inner surface adjacent said tangential slot and an outer surface opposed to said inner surface, andeach said shoulder portion abuts said outer surface of one of said rails, and said rails extend above said shoulder portions. 3. The array according to claim 2, wherein said tangential slot has a continuous sectional profile. 4. The array of claim 1, wherein said slot has a continuous sectional profile. 5. The array of claim 1, wherein each said blade has a platform, an airfoil portion extending radially above said platform, and an attachment part beneath said platform. 6. The array of claim 5, wherein said attachment part comprises a non-rectangular neck portion and a dovetail portion. 7. The array of claim 6, wherein said neck portion is circular. 8. The array of claim 6, wherein said neck portion is multi-sided. 9. The array of claim 6, wherein said dovetail portion has two opposed end faces and wherein each of said end faces has upper and lower chamfered edges. 10. The array of claim 6, wherein each said dovetail portion has two flat sides and each said side is perpendicular to a longitudinal axis of said slot when said blade is positioned within said slot. 11. The array of claim 5, further comprising a pair of load locks and each of said load locks being positioned so as to mate with a notch in a platform of one of said blades. 12. The array of claim 11, further comprising a load locking blade and said load locking blade being held in place by said load locks. 13. The array of claim 12, wherein each of said load locks includes a set screw and said load locking blade has a plurality of notches for receiving a plurality of said set screws. 14. The array of claim 1, wherein said plurality of blades includes a first blade and a second blade which define a space for a load locking blade, each of said first blade and said second blade having a cut-out portion, and said load locking blade having a platform with mating portions for fitting into said and mating with said cut-out portions in said first and second blades. 15. A method of loading and locking a plurality of tangential rotor blades comprising the steps of: providing a disk having a tangential slot, a pair of rails adjacent said slot and extending above an upper boundary of said slot, a first shoulder positioned outwardly of and adjacent to a first one of said rails and a second shoulder positioned outwardly of and adjacent to a second one of said rails, and said rails extending above said shoulders;positioning a first snap seal in a desired location so that said snap seal extends over said slot and said rails and rests on said shoulders;radially loading a first blade having a platform into said slot and rotating said blade after said blade has been loaded into said slot; andpositioning said first blade adjacent said snap seal so that a portion of said snap seal slides under said platform. 16. The method of claim 15, further comprising: loading a second snap seal onto said rails; andmoving said second snap seal into position adjacent said first blade so that said second snap seal slides under said platform of said first blade. 17. The method of claim 16, further comprising: radially loading a second blade having a second platform into said slot and rotating said second blade; andsliding said second blade into a position adjacent said second snap seal so that a portion of said second snap seal slides under said platform of said second blade. 18. The method of claim 17, further comprising: loading additional snap seals and blades until there is a space for only one more blade. 19. The method of claim 18, further comprising: loading a pair of locks into said slot and sliding each of said locks into a slot in a blade platform of a blade adjacent to said space. 20. The method of claim 19, further comprising: radially loading a load locking blade into said space; andpositioning said locks to secure said load locking blade into place.