Jump to content

Sikorsky S-76: Difference between revisions

From Wikipedia, the free encyclopedia
Browse history interactively
← Previous editNext edit →
Content deleted Content added
VisualWikitext
YFdyh-bot (talk | contribs)
166,786 edits
m r2.7.3) (Robot: Adding sr:Сикорски С-76
Line 36: Line 36:
The S-76C+ was produced until December 2005. It is equipped with twin [[Turboméca Arriel 2S1]] engines with [[FADEC]] and a [[Honeywell]] [[Electronic Flight Instrument System|EFIS]] suite.<ref name="Simpson 2001 505"/> The aircraft incorporates active noise suppression, vibration dampers and a [[composite material|composite]] main rotor. On January 3, 2006, the S-76 C++ replaced earlier models in production. It is powered by two [[Turbomeca Arriel 2S2]] engines and incorporates an improved and quieter [[transmission (mechanics)|transmission]] as well as minor changes in the interior equipment and avionics. There were 92 orders for this model as of January 2006.
The S-76C+ was produced until December 2005. It is equipped with twin [[Turboméca Arriel 2S1]] engines with [[FADEC]] and a [[Honeywell]] [[Electronic Flight Instrument System|EFIS]] suite.<ref name="Simpson 2001 505"/> The aircraft incorporates active noise suppression, vibration dampers and a [[composite material|composite]] main rotor. On January 3, 2006, the S-76 C++ replaced earlier models in production. It is powered by two [[Turbomeca Arriel 2S2]] engines and incorporates an improved and quieter [[transmission (mechanics)|transmission]] as well as minor changes in the interior equipment and avionics. There were 92 orders for this model as of January 2006.


Development of the follow-on S-76D has been subject to delays due to technical problems in expanding the flight envelope.<ref>{{cite web|url=http://www.flightglobal.com/articles/2010/12/13/350865/sikorsky-explains-four-year-delivery-slip-for-s-76d.html|accessdate=2010-12-19|title=Sikorsky explains four-year delivery slip for S-76D}}</ref> It is to be powered by {{convert|1050|hp|kW|0|abbr=on}} [[Pratt & Whitney Canada PW210S]] engines driving composite rotors and will incorporate active vibration control. A prototype made its first flight on 7 February 2009 and [[Type certificate|type certification]] was initially expected in 2011, with deliveries forecast for the end of that year. Three prototypes will be used in the certification program. One aircraft will be used to obtain certification of an optional electric rotor ice-protection system. Performance is anticipated to be substantially improved with the added power, but initial certification will retain the same {{convert|11700|lb|kg|0|abbr=on}} gross weight and maximum {{convert|155|kn|km/h|0|abbr=on}} cruise speed.<ref>"First Flight for Improved Sikorsky S-76", p. 15. [[Aviation Week & Space Technology]], February 16, 2009.</ref>
The follow-on S-76D recieved its type certification in October of 2012. Further expansion of the flight envelope will continue into 2013 with first deliveries to the operational fleet planned for mid-2013. It is powered by {{convert|1050|hp|kW|0|abbr=on}} [[Pratt & Whitney Canada PW210S]] engines driving composite rotors and incorporates active vibration control. Prototype #1 made its first flight on 7 February 2009. Three prototypes were used in the certification program. One aircraft will be used to obtain certification of an optional electric rotor ice-protection system. Performance is anticipated to be substantially improved with the added power, but initial certification will retain the same {{convert|11700|lb|kg|0|abbr=on}} gross weight and maximum {{convert|155|kn|km/h|0|abbr=on}} cruise speed.<ref>"First Flight for Improved Sikorsky S-76", p. 15. [[Aviation Week & Space Technology]], February 16, 2009.</ref>


==Design==
==Design==

Revision as of 16:25, 17 January 2013

"S-76" redirects here. For other uses, see S76.
S-76
Galician Coast Guard S-76C+
Role SAR/utility helicopter
Manufacturer Sikorsky Aircraft Corporation
First flight March 13, 1977
Primary user CHC Helicopter Corporation[1]
Number built 774 as of March 2011[citation needed]
Variants Sikorsky S-75

The Sikorsky S-76 is an American medium-size commercial utility helicopter, manufactured by the Sikorsky Aircraft Corporation. The S-76 features twin turboshaft engines, four-bladed main and tail rotors and retractable landing gear.

Development

The development of the S-76 began in the mid-1970s as the S-74, with the design goal of providing a medium helicopter for corporate transportation and the oil drilling industry; the S-74 was later re-designated the S-76 in honor of the U.S. Bicentennial. Sikorsky's design work on the S-70 helicopter (which was selected for use by the United States Army as the UH-60 Black Hawk) was utilized in the development of the S-76, incorporating S-70 design technology in its rotor blades and rotor heads.[2][3] It was the first Sikorsky helicopter designed purely for commercial rather than military use.[4]

The prototype first flew on March 13, 1977.[5] Initial US Federal Aviation Administration type certification was granted on November 21, 1978, with the first customer delivery on February 27, 1979.[6] The S-76 was named "Spirit" late in 1978,[7] but this name was officially dropped by the company on October 9, 1980 due to translation issues into some foreign languages.[8][9]

An early production Sikorsky S-76A owned by Canadian Helicopters and used as an air ambulance.

The first production variant was the S-76A. In 1982, this model set class records for range, climb, speed and ceiling. Several airlines operate the S-76A on scheduled services including Helijet Airways of Vancouver, British Columbia, Canada. The S-76 Mk II was introduced in 1982 and the S-76B in 1987, with its top speed of 155 kn (287 km/h) at sea level. Over 500 S-76s had been delivered by early 2001.[5]

The S-76C+ was produced until December 2005. It is equipped with twin Turboméca Arriel 2S1 engines with FADEC and a Honeywell EFIS suite.[5] The aircraft incorporates active noise suppression, vibration dampers and a composite main rotor. On January 3, 2006, the S-76 C++ replaced earlier models in production. It is powered by two Turbomeca Arriel 2S2 engines and incorporates an improved and quieter transmission as well as minor changes in the interior equipment and avionics. There were 92 orders for this model as of January 2006.

The follow-on S-76D recieved its type certification in October of 2012. Further expansion of the flight envelope will continue into 2013 with first deliveries to the operational fleet planned for mid-2013. It is powered by 1,050 hp (783 kW) Pratt & Whitney Canada PW210S engines driving composite rotors and incorporates active vibration control. Prototype #1 made its first flight on 7 February 2009. Three prototypes were used in the certification program. One aircraft will be used to obtain certification of an optional electric rotor ice-protection system. Performance is anticipated to be substantially improved with the added power, but initial certification will retain the same 11,700 lb (5,307 kg) gross weight and maximum 155 kn (287 km/h) cruise speed.[10]

Design

The S-76 is of conventional configuration, with a four-bladed fully articulated main rotor and a four-bladed anti-torque rotor on the port side of the tailboom. Two turboshaft engines are located above the passenger cabin.[11] In the prototypes and initial production aircraft, these engines were Allison 250-C30s, a new version of the popular Allison 250 engine developed specially for the S-76, with a single-stage centrifugal compressor instead of the multi-stage axial/centrifugal compressor of earlier models of the engine, rated at 650 shp (480 kW) for take-off.[12] These engines are connected to the main rotor by the main gearbox, a three-stage unit with a bull gear as its final stage rather than the planetary gear used by previous generations of Sikorsky helicopters. This arrangement gave 30% fewer parts and lower costs than a more conventional design.[2][13]

S-76++ used for search-and-rescue duties at Royal Australian Air Force bases

The main rotor hub has a single piece aluminum hub with elastomeric bearings designed not to require lubrication or any other kind of maintenance throughout its design life.[2][13] The main rotor blades have titanium spars and incorporate a 10 degree twist to give an even loading when hovering, while the they use a non-symmetrical airfoil section with a drooped leading edge. The rotor tips are tapered and swept back.[13][3] Flight controls are servo-assisted, with a Stability Augmentation System fitted.[14] A retractable nosewheel undercarriage is fitted, which gave the S-76A a 6 knots (6.9 mph; 11 km/h) increase in cruising speed and emergency flotation gear can be fitted, with flotation bags that can be filled with helium in the event of a forced landing on water.[4]

The fuselage is of mixed metal and composites construction, with a fiberglass nose and a light alloy honeycomb cabin structure. The semi-monocoque tailboom is also constructed of light alloy.[11] Two pilots (or a pilot and a passenger) sit side in the cockpit, situated ahead of the cabin, which can accommodate a further 12 passengers in three rows of four, or four to eight passengers in more luxurious executive seating.[13]

Variants

Civil

S-76C search and rescue helicopter operated by Norrlandsflyg.
S-76C owned by LG Electronics as a VIP transport
Sikorsky S-76 SHADOW
  • S-76A : Original production version, powered by two 485 kW (650 shp) Rolls-Royce (Allison) 250-C30 turboshaft engines. Large number modified to S-76A+, A++, C, and C+. 284 manufactured.
  • S-76A Utility : Utility transport version, equipped with sliding doors and a strengthened floor.
  • S-76A+ : Unsold S-76s were fitted with two Turbomeca Arriel 1S turboshaft engines. 17 manufactured.
  • S-76A++ : S-76 helicopters fitted with two Turbomeca Arriel 1S1 turboshaft engines.
  • S-76A Mk II : Improved all-weather transport version, fitted with more powerful engines, and other detail improvements.
  • S-76B : Powered by two Pratt & Whitney Canada PT6B-36A or Pratt & Whitney Canada PT6B-36B turboshaft engines. 101 built.
  • S-76C  : Powered by two 539-kW (981-shp) Turboméca Arriel 1S1 turboshaft engines. 43 manufactured.
  • S-76C+ : Uprated version, fitted with improved Turboméca Arriel 2S1 turboshafts with FADEC. 35 manufactured.
  • S-76C++ : Turboméca Arriel 2S2
  • S-76D : Powered by two Pratt & Whitney Canada PW210S.

Military

AUH-76
Armed utility transport version, developed from the S-76 Mk. II.
H-76 Eagle
Announced in 1985 the Eagle was a military and naval variant of the S-76B, none sold.

Experimental derivatives

Sikorsky S-75
The Advanced Composite Airframe Program (ACAP) was an all-composite Sikorsky early LHX proof of concept aircraft. It mated a new composite airframe with S-76 engines, rotors and powertrain components.[15]
Sikorsky S-76 SHADOW
Boeing-Sikorsky MANPRINT study. The original concept of the LHX program was to produce a one-man helicopter that could do more than a two-man aircraft. The Sikorsky (S-76) Helicopter Advance Demonstrator of Operators Workload (SHADOW) had a single-pilot advanced cockpit grafted to its nose. The purpose was to study the MANPRINT or human engineering interface between the pilot and the cockpit controls and displays. The cockpit was the prototype of a single-pilot cockpit designed for use on the prototype RAH-66 Comanche armed reconnaissance helicopter. The cockpit was designed so sensors would feed data to the pilot through helmet mounted displays. The MANPRINT study determined that single-pilot operation of the Comanche was unsafe, and would result in pilot overload. As result of this study, the Comanche was designed to be operated by a crew of two.[16]

Operators

Civil

The S-76 is in civil service around the world with airlines, corporations, hospital, government operators and, notably, the British Royal Family. The world's largest civilian fleet is the 79 Sikorsky S-76 helicopters operated by CHC Helicopter Corporation.[1]

Military, and government operators

An S-76C of the Spanish Air Force.
Sikorsky S-76B of the Royal Thai Navy.
 Argentina
Hong Kong/Hong Kong Hong Kong
 Japan
 Philippines
 Republic of China
 India
 Saudi Arabia
 Serbia
 Spain
 Thailand

Accidents

Specifications (Sikorsky S-76C++)

An S-76A owned by Canadian Helicopters used for Ornge (Ontario Air Ambulance).
An S-76B prototype helicopter modified as a fantail demonstrator for the RAH-66 program at 1991 Paris Air Show

Data from Sikorsky[25]

General characteristics

  • Crew: two
  • Capacity: seats 12–13
  • Length: 52 ft 6 in (16 m) from tip of main rotor to tip of tail rotor
  • Width: 10 ft 0 in (3.05 m) at horizontal stabilizer
  • Height: 14 ft 6 in (4.42 m) to tip of tail rotor
  • Empty weight: 7,005 lb (3,177 kg) in utility configuration
  • Gross weight: 11,700 lb (5,306 kg)
  • Fuel capacity: 281 US gallons (1,064 liters), with 50 or 102 US gallons (189 or 386 liters) available in extra auxiliary tanks
  • Powerplant: 2 × Turbomeca Arriel 2S2 turboshaft, 922 shp (688 kW) each
  • Main rotor diameter: 4 × 44 ft 0 in (13.41 m)

Performance

  • Maximum speed: 155 kn (178 mph, 287 km/h) at maximum takeoff weight at sea level in standard atmospheric conditions
  • Cruise speed: 155 kn (178 mph, 287 km/h) maximum cruise speed is the same as maximum speed
  • Range: 411 nmi (473 mi, 761 km) no reserves, at long-range cruise speed at 4,000 ft altitude
  • Service ceiling: 13,800 ft (4,200 m)

Avionics

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ^ a b CHC Helicopter (2010). "CHC Fleet". Retrieved January 11, 2011.
  2. ^ a b c Devine, Vinny (April 2012). "Sikorsky Product History: S-76". Igor I Sikorsky Historical Archives. Retrieved 24 July 2012.
  3. ^ a b Lambert Flight International 6 May 1978, p. 1378.
  4. ^ a b Lambert Flight International 6 May 1978, p. 1377.
  5. ^ a b c Simpson 2001, p. 505
  6. ^ Air International March 1980, pp. 142, 144.
  7. ^ Air International March 1980, p. 144.
  8. ^ Kline, R.E., "Identification of S-76 Helicopter", Sikorsky Internal Correspondence P-2462, October 9, 1980.
  9. ^ "R-4 Coast Guard". Sikorsky Archives. Retrieved 2012-07-18.
  10. ^ "First Flight for Improved Sikorsky S-76", p. 15. Aviation Week & Space Technology, February 16, 2009.
  11. ^ a b Taylor 1982, pp. 476–477.
  12. ^ Air International March 1980, pp. 113–114.
  13. ^ a b c d Air International March 1980, p. 114.
  14. ^ Air International March 1980, pp. 114, 116.
  15. ^ Harding, Stephen. "Sikorsky S-75 ACAP". U.S. Army Aircraft Since 1947. Schiffer Publishing Ltd., 1997. ISBN 0-7643-0190-X.
  16. ^ Amsta-lc-cstr (2009). "Historic US Army Helicopters". Archived from the original on June 27, 2009. Retrieved July 2, 2011. {{cite web}}: Unknown parameter |month= ignored (help)
  17. ^ a b c d "World Military Aircraft Inventory". 2011 Aerospace. Aviation Week and Space Technology, January 2011.
  18. ^ "World Military Aircraft Inventory". 2012 Aerospace. Aviation Week and Space Technology, January 2012.
  19. ^ National Airborne Service Corps S-76B
  20. ^ Sikorsky Press release, September 4, 2008.
  21. ^ "Serbian Police Aviation". Aeroflight.co.uk. Retrieved 2012-07-18.
  22. ^ Press Releases - Xunta de Galicia's Search and Rescue Service Purchases Two S-76C++ Helicopters
  23. ^ SALVAMENTO MARÍTIMO - Los ángeles del mar de Galicia han salvado ya a 1.321 náufragos
  24. ^ Pesca tramita la adquisición del tercer helicóptero de Gardacostas
  25. ^ Sikorsky Aircraft Corporation (2007). "S-76 Technical Information: S-76C++ Helicopter, Executive Transport mission" (PDF). Retrieved 18 August 2012.

Bibliography

Wikimedia Commons has media related to Sikorsky S-76.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Sikorsky_S-76&oldid=533547146"