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The GTRE GTX-35VS Kaveri is an afterburning turbofan being developed by the Gas Turbine Research Establishment (GTRE), a lab under the DRDO in Bangalore.
. GTRE is now running two separate successor engine programmes, the K9+ programme and the K10 programme.
“In recent times, the engine has been able to produce thrust of 82 Kilo Newton but what the IAF and other stake-holders desire is power between 90—95 KN", senior officials told The Hindu. "On using the Kaveri for the LCA, they said the engine would be fitted on the first 40 LCAs to be supplied to the IAF when they come for upgrades to the DRDO in the latter half of the decade." Article further adds that in 2011,50-60 test flights will be carried out to mature the engine in terms of reliability, safety and airworthiness.
- So far, 9 prototypes of Kaveri Engine and 4 prototypes of Kabani (Core) Engine have been developed.
- 2200 hours of test (ground and altitude conditions) has been conducted.
- The following two major milestones have been achieved:
- Successful completion of Official Altitude Testing (OAT) ; and
- Demonstration of First Block of flight of Kaveri Engine in Flying Test Bed (FTB)
Plans are also already under way for derivatives of the Kaveri, including a non-afterburning version for an advanced jet trainer and a high-bypass-ratio turbofan based on the Kaveri core, named as Kabini.
- GTX-35VS Kaveri:
- HAL Tejas (planned for production models)
- Kaveri Engine for LCA
- Name of the Project / Programme -- Kaveri Engine for LCA
- Date of Sanction—30 Mar 1989[18]
- Original Probable Date of Completion (PDC) -- 31 Dec 1996
- Revised PDC—31 Dec 2010[18]
- Technologies / Products developed and status of Projects / Programmes on 3 May 2010—About 1880 hrs on engine test has been completed on various prototypes of Kaveri Engine. A total of eight Kaveri Engines and four core engines have been manufactured, assembled and tested. High Altitude testing on core engine has been completed successfully.[
- Kaveri Engine for LCA
- HAL Advanced Medium Combat Aircraft (conceptual)
- Unmanned Aerial Vehicles
- HAL Tejas (planned for production models)
- Derivatives:
- The Indian government plans to adapt and further develop the Kaveri engine design and technology to create a gas-turbine powerplant for armoured fighting vehicles such as the Arjun tank.
- Kaveri Marine Gas Turbine (KMGT), a recently developed derivative of the GTX-35VS Kaveri engine for ships.
- Indian Railways has expressed interest in utilizing Kaveri to power locomotives
Specification (GTX-35VS Kaveri)
General characteristics
- Type: afterburning turbofan
- Length: 137.4 in (3490 mm)
- Diameter: 35.8 in (910 mm)
- Dry weight: 2,724 lb (1,235 kg) [Goal: 2,100-2450 lb (950-1100 kg)]
- Compressor: two-spool, with low-pressure (LP) and high-pressure (HP) axial compressors:
- LP compressor with 3 fan stages and transonic blading
- HP compressor with 6 stages, including variable inlet guide vanes and first two stators
- Combustors: annular, with dump diffuser and air-blast fuel atomisers
- Turbine: 1 LP stage and 1 HP stage
- Maximum thrust:
- Military thrust (throttled): 11,687 lbf (52.0 kN)
- Full afterburner: 18,210 lbf (81.0 kN)
- Specific fuel consumption:
- Military thrust (throttled): 0.78 lb/(lbf•h) (79.52 kg/(kN·h))
- Full afterburner: 2.03 lb/(lbf•h) (207.00 kg/(kN·h))
- Thrust-to-weight ratio: 7.8:1 (76.0 N/kg)
- Airflow: 172 lb/s (78.0 kg/s)
- Bypass ratio: 0.16:1 (it should be increased to 0.5:1)
- Overall pressure ratio: 21.5:1 [Goal: 27:1]
- LP compressor pressure ratio: 3.4:1 [Goal: 4:1]
- HP compressor pressure ratio: 6.4:1
- Turbine entry temperature: 2,218-2,601 °F (1,214-1,427 °C; 1,487-1,700 K) [Goal: 3,357 °F (1,847 °C; 2,120 K)]
GTRE GTX-35VS Kaveri - Wikipedia, the free encyclopedia