HTFE-25
HTFE-25 turbofan engine from HAL
TypeAfterburning turbofan
National originIndia
ManufacturerHindustan Aeronautics Limited
First run14 December 2015
StatusUnder development[1]
Number built2 (Core engines) 1 Technology demonstrator

The HAL HTFE-25 ("Hindustan Turbo Fan Engine") is a 25 kN turbofan engine under development by Hindustan Aeronautics Limited (HAL).[2] The engine can be used in single engine trainer jets, business jets and UAVs weighing up to 5 tonnes and in twin engine configuration for same weighing up to 9 tonnes. Based on the technical feasibility, the market potential for engine is of 200-250 units.[3]

Two engines have been produced and completed 339 runs as of 2019 out of which 96 runs were conducted in 2018-19. Engine has successfully completed cold starting test at 14 °C with spark igniters and has also achieved 100 per cent max speed with and without IGV modulation.

The company has also initiated the development for integrating afterburner technology on engine. In March 2019, first test with "basic afterburner" configuration was conducted on the engine.[4] Cold weather trials and Hot weather high altitude trials were completed at Leh. Full engine (technology demonstrator) has been built and first run completed successfully. Completion of acceleration trials up to 55% of the speed achieved. [5] HAL aims to have the engine in production by 2030.[6]

Specifications

edit

Data from [7][8]

General characteristics

  • Type: turbofan
  • Length: 1,730 millimetres (68 in)
  • Diameter: 590 millimetres (23 in)
  • Dry weight: 350 kilograms (770 lb)

Components

  • Compressor:

Performance

  • Maximum thrust: 25 kN (2,500 kgf; 5,600 lbf) (dry thrust)
  • Bypass ratio: 0.50
  • Air mass flow: 43 kg/s
  • Turbine inlet temperature: 1450 K
  • Fuel consumption: 0.71 kg/kgf-hr (1.565 lb/lbf-hr)
  • Thrust-to-weight ratio: 7.27

See also

edit

Related development

Comparable engines

Related lists

References

edit
  1. ^ "HAL HAS STARTED THE PREPARATION FOR THE TESTING OF HTFE TURBOFANS". INDIAN DEFENCE NEWS. 14 October 2021. Retrieved 8 November 2021.
  2. ^ Boost for 'Make in India': HAL's 25 kN aero engine completes inaugural run; can be used for trainer aircraft
  3. ^ "Annual Report 2017-18" (PDF). Hindustan Aeronautics Limited. Retrieved October 19, 2019.
  4. ^ "Annual Report 2018-19" (PDF). Hindustan Aeronautics Limited. Retrieved October 19, 2019.
  5. ^ "HAl Annual Report 2021-2022" (PDF).
  6. ^ "HAL Committed to HTFE-25 Engine's 2030 Target Despite Recent Hurdles, Citing Progress in Testing Capabilities". Defence News India. 2025-04-21. Retrieved 2025-04-23.
  7. ^ "Boost for 'Make in India': HAL's 25 kN aero engine completes inaugural run can be used for trainer aircraft". Retrieved 15 July 2018.
  8. ^ @vkthakur (27 July 2019). "HAL has successfully tested the 2nd core of the HTFE-25 at 100% power" (Tweet) – via Twitter.

📚 Artikel Terkait di Wikipedia

Ivchenko-Progress AI-322

(afterburning) Related development Ivchenko-Progress AI-222 Comparable engines HAL HTFE-25 Honeywell/ITEC F124 IHI Corporation XF5 Lotarev DV-2 Rolls-Royce Turbomeca

Ivchenko-Progress AI-222

Ivchenko-Progress AI-322 Progress AI-22 Progress D-27 Comparable engines HAL HTFE-25 Honeywell/ITEC F124 IHI Corporation XF5 Lotarev DV-2 Rolls-Royce Turbomeca

HAL HTSE-1200

200 kW) Specific fuel consumption: ~0.296kg/kW-hr Related development HAL HTFE-25 Comparable engines LHTEC CTS800 MTR390 Pratt & Whitney Canada PT6 Safran

TEI-TF6000

Thrust-to-weight ratio: 6.68 Related development TEI TS1400 Comparable engines HAL HTFE-25 Honeywell/ITEC F124 IHI Corporation XF5 Ivchenko-Progress AI-322 Rolls-Royce

IHI Corporation XF5

Ishikawajima-Harima F3 IHI Corporation F7 IHI Corporation XF9 Comparable engines HAL HTFE-25 Honeywell/ITEC F124 Ivchenko-Progress AI-322 Rolls-Royce Turbomeca Adour

Honeywell/ITEC F124

Thrust-to-weight ratio: 5.3:1 Related development Garrett TFE731 Comparable engines HAL HTFE-25 IHI Corporation XF5 Ivchenko-Progress AI-322 Rolls-Royce Turbomeca Adour

List of aircraft engines

124 mm × 140 mm (4.9 in × 5.5 in) HAL HPE-2 HAL PTAE-7 HAL HJE-2500 HAL HTFE-25 HAL HTSE-1200 HAL HPE-90 HAL P.E.90H HAL HJE-2500 GTRE GTX-35VS Kaveri PTAE-7

Hindustan Aeronautics Limited

can be used in HAL-developed Tejas and AMCA, co-developed with GTRE of (DRDO) and Safran Aircraft Engines (under development) HTFE-25 — a turbofan engine