Hendrik_2000
Lieutenant General
WZ 16 aka Ardiden 3C. Short spec 1800SHP; 5000hr. I guess with WZ 16 China finally has a powerful and highly efficient Turboshaft engine to power the next iteration of WZ10. Andmost important a new ASW heli that have its on board computer for sonar and Yu 7 torpedo and or YJ9 missile.Longer radius of operation. Totoro, Blackstone take notice
From globalsecurity
WZ16 turboshaft
The WZ16 turboshaft, with a power more than 1,800 shp, is expected to enter mass production in 2014, for the Z15 (AC352) helicopter series. Eurocopter and Avicopter are jointly developing the 15,000-pound-class EC175/AC352. France-based helicopter engine manufacturer Turbomeca is working on a 50-50 basis with China's AVIC Engine on the WZ16 turboshaft. AVIC Engine is working on the compressor and accessory gearbox, while Turbomeca is responsible for the combustor, turbines and control system. The engine is derived from Turbomeca's Ardiden engine. The agreement covers development, production and support. The two companies committed to have the engine certified in China the year before the AC352 is certified. The AC352 was initially to be offered only with Pratt & Whitney Canada PT6C-67Es, like the Eurocopter EC175.
The latest engine added to the Turbomeca (Safran group) range, the Ardiden is designed for medium helicopters in the 5 to 6.5 ton class, both civil and military. The first application for the new Ardiden turboshaft engine was the Indian twin-engine helicopter Dhruv (formerly known as the Advanced Light Helicopter, or ALH), built by Hindustan Aeronautics Ltd. Its simple, modular design makes this a very economical powerplant in terms of total cost of ownership. At the same time, the Ardiden is designed to carry out even the most demanding missions, while retaining its performance under hot/high conditions. The first variant, the Ardiden 1H1 (dubbed Shakti in India) was co-developed and co-produced with HAL for the Dhruv helicopter.
Featuring a very simple architecture, the Ardiden engine is composed of three main modules for easy maintenance: the accessory/reduction gearbox, a gas generator, and a power turbine. It offers a potential time between overhauls of up to 6,000 hours. The development of the Ardiden 3 engine for heavy helicopters drew on experience with the Ardiden 1. The general layout is the same, with a dual centrifugal compressor and a free turbine. The only major difference is that the engine will not have a reduction gearbox. Analysis of the weight budget showed that, in this power class, it's better to manage speed reduction (from 21,000 rpm at the turbine shaft to 300 or 400 rpm for the rotor) via the main transmission unit.
From Safran website
Ardiden
Launched in 2003, the new-generation Ardiden covers a power range of 1,400 - 2,000 shp and is intended for use in five-to-eight ton single and twin-engine helicopters. The engine is particularly well-suited to demanding mission profiles, delivering sustained performance in hot-and-high conditions.
The Ardiden range features a remarkably compact modular architecture. The gas generator includes two centrifugal stages attached to a reverse-flow combustion chamber, a single-stage gas generator turbine and a two-stage power turbine. This design ensures that the engine remains very cost-effective, particularly in terms of maintenance and cost of ownership.
All Ardidens are equipped with the latest-generation, dual-channel Full Authority Digital Engine Control (FADEC). The Ardiden family is divided into two groups: the Ardiden 1, which offers 1,400 shp with growth potential to 1,700 shp, and the Ardiden 3 (in development), covering 1,700 to 2,000 shp.
Today, over 220 Ardiden 1 are in service throughout the world. They are installed in the Druhv, LCH (Light Combat Helicopter) and LUH (Light Utility Helicopter), all built by India's Hindustan Aeronautics Limited.; Russian Helicopters' Ka-62; and the AC352 from China's AVIC Helicopter.
The Ardiden 3C is fitted in the Chinese AC352, jointly developed by Avic Helicopter with Airbus Helicopters. The result of a 50/50 partnership between Safran Helicopter Engines and AVIC Engine, the Ardiden 3C was ground tested in France in November 2013. The engine will be certified by EASA under the designation Ardiden 3C, and by the Civil Aviation Administration of China (CAAC) under the designation WZ16.
The 3C is characterized by excellent reliability, low-cost maintenance (TBO 3,000 hours on entry-into-service and 5,000 hours once mature) and extremely low fuel consumption (at least ten per cent less than other engines in the same power range).
From globalsecurity
WZ16 turboshaft
The WZ16 turboshaft, with a power more than 1,800 shp, is expected to enter mass production in 2014, for the Z15 (AC352) helicopter series. Eurocopter and Avicopter are jointly developing the 15,000-pound-class EC175/AC352. France-based helicopter engine manufacturer Turbomeca is working on a 50-50 basis with China's AVIC Engine on the WZ16 turboshaft. AVIC Engine is working on the compressor and accessory gearbox, while Turbomeca is responsible for the combustor, turbines and control system. The engine is derived from Turbomeca's Ardiden engine. The agreement covers development, production and support. The two companies committed to have the engine certified in China the year before the AC352 is certified. The AC352 was initially to be offered only with Pratt & Whitney Canada PT6C-67Es, like the Eurocopter EC175.
The latest engine added to the Turbomeca (Safran group) range, the Ardiden is designed for medium helicopters in the 5 to 6.5 ton class, both civil and military. The first application for the new Ardiden turboshaft engine was the Indian twin-engine helicopter Dhruv (formerly known as the Advanced Light Helicopter, or ALH), built by Hindustan Aeronautics Ltd. Its simple, modular design makes this a very economical powerplant in terms of total cost of ownership. At the same time, the Ardiden is designed to carry out even the most demanding missions, while retaining its performance under hot/high conditions. The first variant, the Ardiden 1H1 (dubbed Shakti in India) was co-developed and co-produced with HAL for the Dhruv helicopter.
Featuring a very simple architecture, the Ardiden engine is composed of three main modules for easy maintenance: the accessory/reduction gearbox, a gas generator, and a power turbine. It offers a potential time between overhauls of up to 6,000 hours. The development of the Ardiden 3 engine for heavy helicopters drew on experience with the Ardiden 1. The general layout is the same, with a dual centrifugal compressor and a free turbine. The only major difference is that the engine will not have a reduction gearbox. Analysis of the weight budget showed that, in this power class, it's better to manage speed reduction (from 21,000 rpm at the turbine shaft to 300 or 400 rpm for the rotor) via the main transmission unit.
From Safran website
Ardiden
Launched in 2003, the new-generation Ardiden covers a power range of 1,400 - 2,000 shp and is intended for use in five-to-eight ton single and twin-engine helicopters. The engine is particularly well-suited to demanding mission profiles, delivering sustained performance in hot-and-high conditions.
The Ardiden range features a remarkably compact modular architecture. The gas generator includes two centrifugal stages attached to a reverse-flow combustion chamber, a single-stage gas generator turbine and a two-stage power turbine. This design ensures that the engine remains very cost-effective, particularly in terms of maintenance and cost of ownership.
All Ardidens are equipped with the latest-generation, dual-channel Full Authority Digital Engine Control (FADEC). The Ardiden family is divided into two groups: the Ardiden 1, which offers 1,400 shp with growth potential to 1,700 shp, and the Ardiden 3 (in development), covering 1,700 to 2,000 shp.
Today, over 220 Ardiden 1 are in service throughout the world. They are installed in the Druhv, LCH (Light Combat Helicopter) and LUH (Light Utility Helicopter), all built by India's Hindustan Aeronautics Limited.; Russian Helicopters' Ka-62; and the AC352 from China's AVIC Helicopter.
The Ardiden 3C is fitted in the Chinese AC352, jointly developed by Avic Helicopter with Airbus Helicopters. The result of a 50/50 partnership between Safran Helicopter Engines and AVIC Engine, the Ardiden 3C was ground tested in France in November 2013. The engine will be certified by EASA under the designation Ardiden 3C, and by the Civil Aviation Administration of China (CAAC) under the designation WZ16.
The 3C is characterized by excellent reliability, low-cost maintenance (TBO 3,000 hours on entry-into-service and 5,000 hours once mature) and extremely low fuel consumption (at least ten per cent less than other engines in the same power range).
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