首页 | 主题 | 图库 | 问答 | 文摘 | 原创 | 百科

历史 | 地理 | 人物 | 艺术 | 体育 | 科学 | 音乐 | 电影 | 信息技术 | 世界遗产

 开放、中立,源自维基百科

Personal tools

Sikorsky S-61

From Wikipedia, the free encyclopedia

  (Redirected from Sikorsky S-61L)
Jump to: navigation, search
S-61L/S-61N

HeliJet's S-61N at Vancouver International Airport

Type Medium-lift transport/airliner helicopter
Manufacturer Sikorsky
Maiden flight March 11 1959
Introduction September 1961
Status Active service
Primary users Canadian Coast Guard
CHC Helicopter
Bristow Helicopters
HeliJet
Number built 119[1]
Developed from SH-3 Sea King
Variants Sikorsky S-61R
Image:Wsa-lightning-complex S61type1-drop ron-blaylock.jpg
A Carson Helicopters Fire King drops on the 2007 WSA Lightning Complex fire.
Image:Wsa-lightning-complex S61type1-drop scott-linn.jpg
A Carson Helicopters Fire King drops on the 2007 WSA Lightning Complex fire.
Image:S61-snorkel.jpeg
An S-61 helitanker uses a snorkel to refill its internal water tanks

The Sikorsky S-61L and S-61N are civil variants of the successful SH-3 Sea King helicopter. They are two of the most widely used airliner and oil rig support helicopters built.[1]

Contents

Design and development

In September 1957, Sikorsky won a US Navy development contract for an amphibious anti-submarine warfare (ASW) helicopter capable of detecting and attacking submarines.[1] The XHSS-2 Sea King prototype flew on March 11 1959. Production deliveries of the HSS-2 (later designated SH-3A) began in September 1961, with the initial production aircraft being powered by by two 930kW (1250shp) General Electric T58-GE-8B turboshafts.

Sikorsky was quick to develop a commercial model of the Sea King.[1] The S-61L first flew on November 2 1961, and was 4ft 3in (1.27m) longer than the HSS-2 in order to carry a substantial payload of freight or passengers. Initial production S-61Ls were powered by two 1350shp (1005kW) GE CT58-140 turboshafts, the civil version of the T58. The S-61L features a modified landing gear without float stabilisers.

Los Angeles Airways was the first civil operator of the S-61[2] introducing them on March 1, 1962 for a purchased price of $650,000 each. [3]

On August 7 1962, the S-61N made its first flight.[1] Otherwise identical to the S-61L, this version is optimized for overwater operations, particularly oil rig support, by retaining the SH-3's floats. Both the S-61L and S-61N were subsequently updated to Mk II standard with improvements including more powerful CT58-110 engines giving better hot and high performance, vibration damping and other detail refinements.

The Payloader, a stripped down version optimised for aerial crane work, was the third civil model of the S-61.[1] The Payloader features the fixed undercarriage of the S-61L, but with an empty weight almost 2000lb (900kg) less than the standard S-61N.

A unique version is the S-61 Shortsky conversion of S-61Ls and Ns by Helipro International.[1] The fuselage is shortened by 50in (1.6m) to increase single engine performance and external payload. The Shortsky conversion first flew in February 1996.

Variants

S-61L 
Non-amphibious civil transport version. It can seat up to 30 passengers (13 Built).
S-61L Mk II 
Improved version of the S-61L helicopter, equipped with cargo bins.
S-61N 
Amphibious civil transport version.
S-61N Mk II 
Improved version of the S-61N helicopter.
S-61 Payloader 
Stripped down machine optimised for aerial crane work; features the fixed undercarriage of the S-61L, but with an empty weight almost 900kg (2000lb) less than the standard S-61N.
S-61 Shortsky 
Shortened conversion of the S-61L and N, designed to increase single engine performance and external payload.

Operators

Flag of Greenland Greenland
Flag of Canada Canada
Flag of the United Kingdom United Kingdom
Flag of the Netherlands Netherlands
Flag of Pakistan Pakistan
Flag of the United States United States
Flag of Ireland Ireland

Former operators are marked by italics

Specifications (S-61N Mk II)

Data from International Directiory of Civil Aircraft[1]

General characteristics

  • Crew: 2 pilots
  • Capacity: up to 30 passengers
  • Length: 58 ft 11 in (17.96 m)
  • Rotor diameter: 62 ft (18.9 m)
  • Height: 17 ft 6 in (5.32 m)
  • Disc area: 3,019 ft² (280.6 m²)
  • Empty weight: 12,336 lb (5,595 kg)
  • Loaded weight: lb (kg)
  • Max takeoff weight: 19,000 lb (8,620 kg)
  • Powerplant:General Electric CT58-140 turboshafts, 1,500 shp (1,120 kW) each

Performance


Accidents

Image:6308-340DisneyLandChopper-R.jpg
N300Y, the S-61L prototype, departing from Disneyland Heliport flight five years prior to accident flight
AD Links