https://en.wikipedia.org/wiki/Sikorsky_R-4
The Sikorsky R-4 is a two-seat helicopter designed by Igor Sikorsky with a
single, three-bladed main rotor and powered by a radial engine. The R-4 was the
world's first large-scale mass-produced helicopter and the first helicopter used
by the United States Army Air Forces, the United States Navy, the United States
Coast Guard and the United Kingdom's Royal Air Force and Royal Navy. In U.S.
Navy and U.S. Coast Guard service, the helicopter was known as the Sikorsky
HNS-1. In British service, it was known as the Hoverfly.
The VS-316 was developed from the famous experimental VS-300 helicopter,
invented by Igor Sikorsky and publicly demonstrated in 1940. The VS-316 was
designated the XR-4, under the United States Army Air Forces' series for
"Rotorcraft". The XR-4 first flew on 14 January 1942 and was accepted by the
Army on 30 May 1942. The XR-4 exceeded all the previous helicopter endurance,
altitude and airspeed records that had been set before it. The XR-4 completed a
761-mile (1,225 km) cross-country flight from Connecticut to Wright Field, Ohio,
set a service ceiling record of 12,000 feet (3,700 m), while achieving 100
flight hours without a major incident and an airspeed approaching 90 mph (140
km/h).
The British Admiralty, having learned of the VS-300, made a ship available that
had been intended to show the USN their work with autogyros and ship operations.
platform. After her loss in 1942 to a U-boat, she was replaced by the SS
Daghestan. The first deck-landing trials on Daghestan were carried out in 1944.
The British received two of the first eight helicopters built.
On 5 January 1943, the United States Army Air Forces ordered 29 prototypes. The
first three prototypes were designated as the YR-4A and used for evaluation
testing. The YR-4A benefited from a larger, 180 hp (130 kW) Warner Super Scarab
(R-550-1) engine, compared to the 165 hp (123 kW) R-500-3 engine in the
prototype, and a rotor diameter increased by one foot (30 cm). Evaluation of the
YR-4A demonstrated a need for further improvements, including moving the
tailwheel further towards the rear of the tailboom, venting the exhaust to the
side instead of downward, and increasing the fuel capacity by 5 gallons (19
liters). These and other design changes led to the designation of later
prototypes as YR-4B, which were used for service testing and flight training.
Role
Helicopter
Manufacturer
Sikorsky Aircraft
Designer
Igor Sikorsky
First flight
14 January 1942
Primary users
United States Army Air Forces
United States Coast Guard
Royal Air Force
Produced
Number built
131
Developed from
Vought-Sikorsky VS-300
Developed into
Sikorsky R-6
Following the sinking in January 1944 of USS Turner, a Sikorsky R-4 flew life
Army Lieutenant Carter Harman of the 1st Air Commando Group conducted the first
combat rescue by helicopter using a YR-4B in the China-Burma-India theater.
Despite the high altitude, humidity, and capacity for only a single passenger,
Harman rescued a downed liaison aircraft pilot and his three British soldier
involved several legs for refueling and navigating through passes between
mountains nearly 10,000 feet (3,000 m) tall, to reach a weather station located
at an elevation of 4,700 feet (1,400 m). The higher-than-normal altitude
required a downhill run of 20 ft (6.1 m) to get airborne.
While the R-4 was being used for rescues in Burma and China, it was also being
used to ferry parts between floating Aviation Repair Units in the South Pacific.
On 23 May 1944, six ships set sail with two R-4s on board each vessel. The ships
had been configured as floating repair depots for damaged Army Air Forces
aircraft in the South Pacific. When the helicopters were not being used to fly
the parts from one location to another, they were enlisted for medical
evacuation and other mercy missions.
In Royal Air Force service, the R-4 was called the Hoverfly. The Helicopter
Training School, formed January 1945 at RAF Andover, was the first British
military unit to be equipped with the helicopter. Many RAF Hoverfly Mark Is were
transferred to the Royal Navy for training and one was used in 1945/46 by Fairey
Aviation to develop rotor systems for their Gyrodyne helicopter.
Specifications (R-4B)
General characteristics
Crew: one
Capacity: one
Length: 33 ft 8 in (10.2 m)
Rotor diameter: 38 ft (11.5 m)
Height: 12 ft 5 in (3.8 m)
Empty weight: 2,098 lb (952 kg)
Loaded weight: 2,581 lb (1,170 kg)
Performance
Maximum speed: 75 mph (120 km/h)
Cruise speed: 65 mph (105 km/h)
Range: 130 miles (210 km (110 nm))
Service ceiling: 8,000 ft (2400 m)
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