Sikorsky XR-4C

Sikorsky R-4

LandNorge , Norge
RolleHelikopter
Første fly14. januar 1942
Bygget131

Den Sikorsky R-4 er et to-seters helikopter som ble designet av Igor Sikorsky med en enkelt, trebladet hovedrotor og drevet av en stjernemotor. R-4 var verdens første storskala masseproduserte helikopter og det første helikopteret som ble brukt av United States Army Air Forces, United States Navy, United States Coast Guard og Storbritannias Royal Air Force og Royal Navy. I US Navy og US Coast Guard-tjeneste var helikopteret kjent som Sikorsky HNS-1. I britisk tjeneste var den kjent som Hoverfly.

Kilde: Sikorsky R-4 på Wikipedia

Sikorsky XR-4C Walk Around
FotograferVladimir Yakubov
LokaliseringNational Air & Space Museum - Udvar-Hazy Center, Chantilly, VA
Bilder33
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General Characteristics

The Sikorsky R-4 (known as the Hoverfly in British service) was the world’s first mass-produced helicopter and the first to be successfully put into service by the United States Army Air Forces (USAAF) and Allied military forces during World War II. Designed by Igor Sikorsky, it pioneered the single-main-rotor, single-tail-rotor configuration common today. It was primarily used for training, liaison, and air-sea rescue.

Property Typical Value (R-4B Production Variant)
Rolle Liaison, Training, Search and Rescue (SAR)
Designer/Manufacturer Igor Sikorsky / Sikorsky Aircraft
First Flight (Prototype XR-4) 14. januar 1942
Mannskapet 2 (Pilot and Passenger/Co-pilot)
Rotor Diameter 11.58 m (38 ft)
Length (Fuselage) 10.2 m (33 ft 8 in)
Max Takeoff Weight 1,170 kg (2,581 lb)
Units Built 131 (All variants)

Design and Powerplant

  • Engine: One Warner R-550-3 7-cylinder air-cooled radial piston engine.
  • Power Output: 149 kW (200 hp). (Earlier variants used 165 hp or 180 hp engines.)
  • Rotor System: Single main rotor with three wooden blades, and a two-bladed anti-torque tail rotor.
  • Construction: Fuselage constructed from steel tubing truss, covered with doped fabric to reduce drag.
  • Pilot Controls: Incorporated the cyclic stick, collective pitch lever, and rudder pedals for the tail rotor, establishing the standard helicopter control layout.
  • Historic Use: Achieved the first air-based combat rescue in Burma in April 1944.

Prestasjon

  • Maximum Speed: 121 km/h (75 mph, 65 knots) at sea level.
  • Cruise Speed: 105 km/h (65 mph, 56 knots).
  • Range: Approximately 210 km (130 miles, 110 nautical miles).
  • Service Ceiling: 2,400 m (8,000 ft).
  • Climb Rate: 3.3 m/s (650 ft/min).
  • Piloting Difficulty: The R-4 was notoriously difficult to fly due to vibration and the lack of a governor to automatically coordinate throttle with collective pitch changes.

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