7 8 6 4 5 2 3 1 Fuel Tank (2) F F Collective Control Fuel out Rotor Spar Tail Fin Cover with aircraft fabric such as Ceconite Azmuth Control Blade Control Horn E E 45.00° Isometric View Scale = 1:16 Parachute Harness release shown for reference only DETAIL AU SCALE 1 : 4 G8-2-30 Jet Parachute harness release shown for reference only Blade assemby Cover with aircraft fabric such as Ceonite. Rotor Spar assembly Fuel Tanks Rotor Head Assembly D D To fuel feed at head AU Fuel Out Ram air intake scoop Top View C C MEG-2X REV 245.562 D AW B B Rotor Spar Rotor Head Blade Pitch Push Rod Swashplate Azmuth Control A Front View UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN INCHES TOLERANCES: FRACTIONAL ANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL Twist-Grip Throttle Fuel Transfer Assembly To Fuel Pressure Gauge DETAIL AW SCALE 1 : 4 8 7 Collective Control 6 INTERPRET GEOMETRIC TOLERANCING PER: PROPRIETARY AND CONFIDENTIAL To Fuel Tank(s) Fuel Shutoff 5 Driver Gear Needle Valves THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF ROBERT Q RILEY ENTERPRISES LLC. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF ROBERT Q RILEY ENTERPRISES LLC IS PROHIBITED. Tank Pressure Connection 4 3 MATERIAL USED ON NEXT ASSY APPLICATION 2 FINISH NAME DATE A DRAWN CHECKED TITLE: General Layout Master Assembly ENG APPR. MFG APPR. Q.A. COMMENTS: SIZE DWG. NO. D MEG-2X SCALE: 1:8 WEIGHT: 1 REV SHEET 1 OF 26 7 8 6 4 5 2 3 1 NOTE: Intake stages 1 & 2 are part of Duct Cowl Asmy-6. They are shown here for clarity Stage 3 Intake Stage 2 Intake (part of Duct Cowl Asmy-6) Locator F NOTE: Because engine is shown level blade is shown at an angle. This foreshortens the cord and shows bolts & holes at an 8 degree angle in top & bottom views. Stage 1 intake (part of Duct Cowl Asmy-6) Channel Firewall-1 F This is welded to inside of Duct Cowl Asmy-6 Injection Nozzle Is positioned by hole inside Duct Cowl Asmy-6 Pass-through for liquid propane fuel line Fuel line hole/pass-through not shown Ignition Wire use doorbell wire Super-heated gas from coil & into injection nozzle Burner Tail Pipe Retention Bracket 1/32 inch gap around tail pipe Ream holes to fit 8-32 bolts Jet Mounting Plate 2 sides Ream holes in place to fit 10-32 screws Grommet E E Wood screw Tail Pipe Retention Bracket Connector Bottom View Liquid fuel routed to side & through hole in Firewall and to connection on jet. Attach to Firewall-Rib here and below Hand fit tabs after jet is in place Trailing Edge-7 D D Top View C C Blade cover Top-5 & Bottom-6 .025 Aluminum 12.123 .031 1.250 10.00° Minimum .250 gap between skin and jet .500 25% cord line Attach to inside of Rib-Firewall-2 upper return .531 .488 .188 .313 5.625 .750 CONNECTOR .031 Brass 2 req (1 each blade) GH-2-20 Jet Center of Injection Nozzle Scoop & Cowl A Tail Pipe Retention Bracket Ignition terminal 1.770 1.41° 11.39° Top cover at engine 3.563 3.575 3.650 1.688 Rear View 8.00° DIMENSIONS ARE IN INCHES TOLERANCES: FRACTIONAL ANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL Center-line of blade INTERPRET GEOMETRIC TOLERANCING PER: PROPRIETARY AND CONFIDENTIAL THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF ROBERT Q RILEY ENTERPRISES LLC. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF ROBERT Q RILEY ENTERPRISES LLC IS PROHIBITED. 7 1.000 6 5 4 Attach to inside of Rib-Firewall-2 lower return UNLESS OTHERWISE SPECIFIED: Viewed from Rotor Head Side 8 B TAIL PIPE RETENTION BRACKET .040 4139 N Steel 2 req (1 per engine) Must fit loose on Tail Pipe 1/32 inch gap around perimeter. SKIN TOP-5 & BOTTOM-6 .025 24ST Aluminum 4 req (2 each blade) Hand form to ribs Center-line of jet Fuel Connection 13.313 .125 B R1.821 .715 10.313 D 1.031 REV .250 7.623 MEG-2X .750 3 MATERIAL USED ON NEXT ASSY APPLICATION 2 FINISH NAME DATE A DRAWN CHECKED TITLE: ENG APPR. Jet/Blade Detail MFG APPR. Q.A. COMMENTS: SIZE DWG. NO. D MEG-2X SCALE: 1:4 WEIGHT: 1 REV SHEET 24 OF 26