|Zhi-8 Transport / SAR Helicopter
Date:2010-01-12 Source:internet By:globalmil Viewed:
Zhi-8 (Z-8) is a medium transport helicopter developed from the French SA 321 Super Frelon, of which 13 examples were sold to the PLA Navy in 1977~78. At least one of these helicopters was disassembled for survey and reverse-engineering. Development of the Chinese copy of the SA 321, designated Z-8, began in 1976 at the Jingdezhen-based Changhe Aircraft Factory (now Changhe Aircraft Industry Group, CAIG). However, the Z-8 development encountered enormous technical difficulties and the project was suspended in 1979 due to financial reasons.
直-8（Z-8）是一种中型运输直升飞机基于法国SA 321“超黄蜂”发展，在1977~78年13架原型出售给PLA海军。至少这些直升飞机其中一架被分解用于测量和反向-工程。中国的SA 321仿造型，指定为Z-8，1976年在景德镇（Jingdezhen）建立的昌河（Changhe）飞机制造厂（现在昌河飞机工业集团，CAIG）发展，然而，Z-8发展遇到了巨大的技术困难，而且计划在1979年由于财政原因被中止。
In 1985, Changhe resumed the Z-8 programme with its own funding, and the first prototype successfully flew in December 1985. The Z-8 entered the PLA Navy service in 1989 for trial and evaluation, but the helicopter was not certified for design finalisation until 1994. Only a small number (15~20) have been built. The helicopter was mainly deployed by the PLA Navy for transport role from land-based airfields.
Development of an army variant designated Z-8A began in the mid-1990s, and the helicopter was certified for design finalisation in February 1999. After two examples were delivered to the PLA Army Aviation Corps for operational test and evaluation, Changhe began the delivery of the first production batch in November 2002. Currently a small number (4~6) of the Z-8A is operated by the PLA 7th Helicopter Regiment in the Jinan Military Region.
The Z-8A is similar to the basic variant Z-8 in appearance, apart from its Army woodland camouflage colour scheme instead of the naval grey colour of the Z-8. The Z-8A also retained the nose weather radar and the side floating stabilisers on the original Z-8. The helicopter can carry 27 equipped commandos, or 39 soldiers, or 15 stretchers. If necessary, the helicopter could also carry a small-size SUV-type vehicle via its loading ramp. The helicopter is unarmed.
During the 2002 Zhuhai Air Show, Changhe Aircraft Industry Group (CAIG) announced that it was developing a new utility variant Z-8F, which would be powered by three Pratt & Whitney Canada PT6A-67B turboshaft engines for improved performance. The helicopter made its maiden flight in August 2004.
The PLA Air Force introduced the Z-8K as a dedicated search and rescue (SAR) helicopter in 2007. The helicopter appears to be based on the Z-8F design, featuring the Pratt & Whitney Canada PT6A-67B turboshaft engine and redesigned air inlets. As well as having a hydraulic hoist fitted externally above the cabin door, the helicopter also featured an external forward-looking infrared (FLIR) sensor and a search light fitted underneath the cockpit. There are two variants currently in service: Z-8K with a blue-white camouflage scheme operated by the PLAAF 26th Air Division, and Z-8KA with a green colour scheme operated by the PLAAF Airborne Corps.
A shipborne variant designated Z-8J has recently entered service with the PLA Navy. As the original variant Z-8 did not possess the ability to take-off and land on surface vessels, the Z-8J features some modifications in its landing gears to allow shipborne operations. There are two variants currently in service: Z-8JA for shipborne transport and resupply roles, and Z-8JH for the medical evacuation role.
The Z-8 is identical to the SA 321 Super Frelon in appearance, with a six-bladed main rotor mounted above centre of the fuselage. Of the three turboshaft engines, two are mounted side-by-side atop the fuselage forward of main rotor, with the third behind the main rotor. Round air intakes are located above and behind cockpit. Boat-hull type fuselage mounts stabilising floats on either side of the body, which has fixed landing gear and an upswept rear section. The landing gear of the Z-8 is larger in size compared to that of the SA 321. The nose is round with glassed-in cockpit. The tail boom tapers from the main body to the swept-back, tapered fin with a rotor on the left. The single flat is tapered and flat-mounted on the right side of the fin. The army variant Z-8A also features a large rear ramp for fast access by the troops.
Z-8和SA 321“超黄蜂”在外表上相同，在机身上方中心安装六桨叶主旋翼。三台涡轴发动机中，二台安装在主减速器前的机身顶部两侧，第三台在主减速器后。圆形进气口位于座舱后部上方。船-壳型机身两侧安装稳定浮筒，固定起落架和上斜尾段。Z-8的起落架在大小方面与SA 321相比较大些。圆形鼻子连同围玻璃驾驶座舱。尾梁从主机身倾斜渐细，锥形尾翼连同一个左侧安装的尾旋翼。锥形单尾平翼水平安装在尾翼右侧。陆军改型Z-8A为军人快速通过以一个后部斜板为特点。
The Z-8 has a hoist with winch and scoop fitted externally above the starboard side cabin door for rescue missions. For transport missions, the helicopter can carry 27 armed soldiers (maximum 39), or 15 patient litters and a medical staff, or 5,000kg cargo externally on sling.
The Z-8 lacks the ASW equipments and surface search radar found on the original SA 321, nor can it operate from the flight deck of surface vessels. A nose dome in front of the cockpit houses a Chinese indigenous navigation / weather radar.
The basic variant Z-8 has three WZ-6 (Chinese copy of Turboméca 3C III) turboshafts, each rated at 1,512hp (1,128kW). The internal fuel capacity is 3,900 litres. The improved Z-8F will be fitted with three Canada-made Pratt & Whitney PT6A-67B turboshaft engines, each rated at 1,941hp (1,448kW).
基本型Z-8有三台WZ-6（中国仿造的Turboméca 3C III型）涡轴发动机，每台额定1,512 hp（1,128 kW）。机身内燃料能力是3,900升。改良的Z-8F将会配备有三台加拿大制造的普惠PT6A-67B涡轴发动机，每台额定1,941 hp（1,448 kW）。
Flight crew: 2
Main rotor diameter: 18.9m
Weight (empty): 6.86t (Z-8); 7.1t (Z-8F)
Weight (maximum take off): 13t
Engine: 3 x WZ-6 turboshafts, each rated at 1,512hp (Z-8), or 3 x Pratt & Whitney PT6A-67B turboshaft, each rated at 1,941hp
Internal fuel: 3,900 litre
Maximum speed: 248km/h (Z-8); 255km/h (Z-8F)
Service ceiling: 3,100m (Z-8); 4,700m (Z-8F)
Hover ceiling (in ground effect): 1,900m (Z-8); 2,800m (Z-8F)
Range: 700km (with 27 soldiers), or 500km (with 3,000kg payload)
Endurance: 4 hours
Maximum payload: 5,000kg
Typical load: 27 troops or 15 stretchers
飞行组员： 2 名
机长： 23 米
主旋翼直径： 18.9 米
机高： 6.76 米
重量： （空重） 6.86 吨（Z-8）；7.1 吨（Z-8F）；（最大起飞） 13 吨
发动机： 3 x WZ-6 涡轴发动机，每台额定1,512 hp（Z-8），或 3 x 普惠 PT6A-67B 涡轴发动机，每台额定1,941 hp
内部燃料： 3,900 公升
最大速度： 248 km/h（Z-8）；255 km/h（Z-8 F）
升限： 3,100 米（Z-8）；4,700 米（Z-8F）
盘旋升限： （地面效应） 1,900 米（Z-8）；2,800 米（Z-8F）
航程： 700 公里（连同27名军人），或500公里（连同3,000公斤负载）
最大负载： 5,000 公斤
Last update: 2 January 2009
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