Vertical Take Off Vertical Take Off and Landingand Landing

HYO216HYO216

SACRED TEXTS AND LEGENDS

Leonardo da Vinci

Jules Verne

Paul Cornu

Cierva

Focke

VTOL

• SAME PROPULSION SYSTEM FOR HOVER AND FORWARD FLIGHT

• SEPARATE POWER PLANT FOR HOVER

• COMBINED POWER PLANT FOR HOVER

• AUGMENTED POWER PLANT FOR HOVER

SAME PROPULSION SYSTEM FOR HOVER AND FORWARD

FLIGHT

Tilt Shaft/Rotor

1. Transcendental Model 1G

2. Bell XV-3

Tilt Prop

3. Curtiss-Wright X-100

4. Curtiss-Wright X-19

Tilt Ducts

5. Doak 16 VZ-4

6. Bell X-22A

7. Nord 500 Cadet

Tilt Wing

8. Vertol 76 VZ-2

9. Hiller X-18

10. LTV-Hiller-Ryan XC-142

• General characteristics• Crew: 2 • Capacity: 12 passengers • Length: 47 ft 3.5 in (14.415 m) • Wingspan: 34 ft 4 in (10.46 m) • Height: 14 ft 3 in (4.34 m) • Wing area: 233.3 sq ft (21.67 m2) • Airfoil: NACA 633-418 • Empty weight: 8,417 lb (3,818 kg) • Max takeoff weight: 14,500 lb (6,577 kg) (STOL), 12,600 lb (5,710 kg) (VTOL) • Maximum width over propeller tips:34 ft 8 in (10.56 m) • Maximum height over propellers during wing tilt: 17 ft 1½ in (5.22 m) • Powerplant: 2 × Lycoming T53 shaft-turbines, 1,500 shp (1,100 kW) each • Main rotor diameter: 7 ft 0 in (2.13 m) • Propellers: 4-bladed, 14 ft 0 in (4.27 m) diameter • Performance• Maximum speed: 321 mph (517 km/h; 279 kn) • Cruise speed: 301 mph (262 kn; 484 km/h) • Never exceed speed: 415 mph (361 kn; 668 km/h) • Range: 421 mi (366 nmi; 678 km) with max wing fuel, VTOL, & 10% reserves • Rate of climb: 4,200 ft/min (21 m/s)

11. Canadair CL-84 Dynavert

Tilt Rotor

• Crew: 2, • engine: 2 x Avco Lycoming LTC1K-4K • rated at 1140kW, • rotor diameter: 7.62m, • take-off weight: 5897kg, • empty weight: 4341kg, • max speed: 550km/h, • range: 800km

12. Bell XV-15

• Engine: 2 x Allison T406-AD-400 turboshaft, • rated at 4585kW, • rotor diameter: 14.02m, • length with wings and rotors folded: 19.09m, • height with engine nacelles in a vertical position: 6.35m, height with wings and rotors

folded: 5.61m, • max width with rotors turning: 25.78m, • wingspan (without nacelles): 14.02m, • take-off weight: 27440kg, • loaded weight: 13995kg, • fuel: 6215kg, • cruising speed as a helicopter: 185km/h, • cruising speed as an airplane: 555km/h, • hovering ceiling, OGE: 915m,• range with a vertical start with 21150kg take-off weight and 5445kg • payload: 2225km, • range with a normal start with 24950kg take-off weight and 9070kg payload: 3340km,• payload: 9070kg

13. Bell Boeing V-22 Osprey

Tilt Jet

14. Bell 65 Air Test Vehicle (ATV)

Deflected Slipstream

15. Robertson VTOL

16. Ryan 92 VZ-3 Vertiplane

17. Fairchild 224 VZ-5 Fledgling

Vectored Thrust

18. Bell X-14

19. Hawker P.1127 Kestrel

20. Yakovlev Yak-36 Freehand

21. McDonnell Douglas/British Aerospace Harrier

22. Boeing X-32

Tail Sitters

23. Lockheed XFV-1

24. Convair XFY-1 Pogo

25. Ryan X-13 Vertijet

26. SNECMA C450 Coléoptère

SEPARATE POWER PLANT FOR HOVER

Lift + Cruise

27. Short SC.1

28. Dassault Balzac V

29. Dassault Mirage III-V

COMBINED POWER PLANT FOR HOVER

Lift + Lift/Cruise

30. EWR VJ101C

31. Dornier Do 31

32. Lockheed XV-4B Hummingbird II

33. VFW VAK 191B

34. Yakovlev Yak-38 Forger

35. Yakovlev Yak-141 Freestyle

36. McDonnell XV-1

37. Fairey Rotodyne

AUGMENTED POWER PLANT FOR HOVER

Ejector

38. Lockheed XV-4A Hummingbird

39. Rockwell XFV-12A

Fan

40. Vanguard Omniplane

41. GE-Ryan XV-5A Vertifan

42. Lockheed Martin X-35

Rotor

43. Kamov Ka-22 Vintokryl 'Hoop'

44. Piasecki 16H-1 Pathfinder

45. Lockheed AH-56 Cheyenne

VZ Series

Hiller VZ-1 Pawnee "Flying Plathome"

Hiller VZ-1E Flying PlathomeVTOL Experimental Vehicle

SNECMA C-400 P-2 Atar Volant Frence

• Length : 8.05mRotor Diameter : 2.90mWidth : 7.60mHight : 3.25mngine : Lycoming YT53-L-1 (700hp) X 1Crew : 1

Vertol Model76The Prototype of VZ-2

• Length : 8.43mWing Span : 7.14mHight : 3.25mAll-Up Weight : 1,180KgEngine : Abco-Lycoming T53-L-1 (1,000shp) X 1Crew : 1

Ryan VZ-3RY Vertiplane

• Length : 9.75mWidth : 7.77mHight : 3.05mAll-Up Weight : 1,452KgEngine : Lycoming YT543 (840shp) X 1Max Speed : 370Km/hService Ceiling : 1,830mRange : 370KmCrew : 2

Doak VZ-4Ducted Fun VTOL

• Length : 10.26mHight : 5.13mAll-Up Weight : 1,803KgEngine : General Electric YT58-GE-2 Turboshaft (1,024shp) X 1Max Speed : 297Km/hCrew : 2

Firchild VZ-5 Fledgling

Piasecki

Lycoming

• Length : 6.55mPropella Diameter : 2.59mHight : 1.57mAll-Up Weight : 1,088KgEngine : Lycoming piston engine (500shp)Crew : 1

Chrysler Flying Jeep (VZ-6)

• Length : 5.18mPropella Diameter : 1.98mSpan : 4.87mHight : 2.83mAll-Up Weight : 952KgOwn weight : 771KgEngine : Turbom馗 a Artouste II B turboshaft engine (425shp)Max Speed : 51Km/hCruising Speed : 40Km/hService Ceiling : 60.9mArmament : NoneCrew : 1 (the second prototype : 2)

Curtiss-Wright VZ-7

• Length : 7.44mRotor Diameter : 2.5mWidth : 2.81mHight : 1.77mAll-Up Weight : 1,664KgOwn weight : 1,184KgEngine : Turbom馗 a Artouste II C turbine (400shp) X 2Max Speed : 136Km/hCruising Speed : 112Km/hService Ceiling : 914mRange : 56KmCrew : 2 + 3

Piasecki VZ-8

AVROCAR

• Diameter : 5.48mRotor Diameter : 1.52mHight : 1.77mEngine : Continental J69-T-9 Turbojet X 3Max Speed : 480Km/h (Plan Spec)Range : 1,600KmCrew : 2

AVRO CANADA VZ-9V AVROCAR

Some Patents and Simulations

• A VTOL aircraft including a fuselage with four nacelles, three vertical stabilizers and a horizontal stabilizer attached to the fuselage. The fuselage and the nacelles are lifting bodies that are configured to jointly form an aerodynamic lifting body which cooperates with the horizontal stabilize...Inventor: Paul S. MollerAssignees: Moller International, Inc.Primary Examiner: Anne E. Bidwell

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