Xian WS-15
WS-15 | |
---|---|
Type | Turbofan |
National origin | People's Republic of China |
Manufacturer | Xi'an Aero-Engine Corporation |
Designed by | Shenyang Aeroengine Research Institute |
First run | 2006[1] |
Major applications | Chengdu J-20 |
Status | Under development |
The WS-15 (Chinese: 涡扇-15; pinyin: Wōshàn-15), codename Emei, is a Chinese afterburning turbofan engine designed by the Shenyang Aeroengine Research Institute and manufactured by the Xi'an Aero-Engine Corporation.[1]
The WS-15 is intended to power and enable supercruising on the Chengdu J-20.[2]
Design and development[]
Development of the WS-15 afterburning turbofan engine began in the early 1990s.[1] In 2005, the engine performed successfully on the testbed. An image of the core appeared at the 2006 China International Aviation & Aerospace Exhibition. In 2009, a prototype achieved 160 kilonewtons (36,000 lbf) and a thrust-to-weight ratio of 9.[3] The thrust target was reported as 180 kilonewtons (40,000 lbf) in 2012.[4]
Specifications[]
Data from School of Mechanical Engineering,Shandong University[5][6]
General characteristics
- Type: Afterburning turbofan
- Length: 5.05m
- Diameter: 1.02m
- Dry weight: 1701 kg
Components
- Compressor: axial flow
- Combustors: nickel alloy annular combustion chamber
- Turbine: single-stage high pressure, single-stage low pressure
Performance
- Maximum thrust:
- 105.22 kN (23,654 lbf) (military thrust)
- 161.865–181.37 kN (36,389–40,774 lbf) (afterburner)
- Overall pressure ratio: 28.71
- Air mass flow: 138kg/s
- Turbine inlet temperature: 1,477 °C (2,691 °F)
- Specific fuel consumption:
- 2.02kg/N/h (afterburner)
- 0.665kg/N/h (Intermediate)
- Thrust-to-weight ratio: 9.7-10.87
See also[]
- Shenyang WS-10
- Guizhou WS-13
- WS-20
- CJ-1000A
- List of aircraft engines
- List of Chinese aircraft engines
Comparable engines
References[]
- ^ a b c Fisher, Richard (27 May 2015). "ANALYSIS: Can China break the military aircraft engine bottleneck?". Flightglobal. Retrieved 28 May 2015.
- ^ Chan, Minnie (10 February 2018). "Why China's first stealth fighter was rushed into service with inferior engines". South China Morning Post.
- ^ Fisher, Richard, Jr. (30 December 2009). "October Surprises In Chinese Aerospace". International Assessment and Strategy Center. Archived from the original on August 13, 2015. Retrieved 28 May 2015.
- ^ China Aerospace Propulsion Technology Summit (PDF), Galleon (Shanghai) Consulting, 2012, p. 2, archived from the original (PDF) on 8 December 2013, retrieved 28 May 2015
- ^ 郭培哲 (2016-12-03). "涡扇" (in Simplified Chinese). 山东大学机械工程学院. Archived from the original on 2021-10-02. Retrieved 2021-10-02.
- ^ "聚焦航发控制系统主业,增长提速巩固龙头地位" (PDF) (in Simplified Chinese). 中泰证券. 2021-10-08. p. 25. Retrieved 2021-12-01.
External links[]
- Low-bypass turbofan engines
- 2000s turbofan engines