Abstract
300 DaN itki sınıfında klasik bir turbojet motor performansı ile tamamen yerli bir konsept olan Pars türbojet motorun itki ve yakıt tüketim düzeyleri karşılaştırılmıştır. Pars türbojet motor klasik turbojet motora göre %35 daha az hava ile tüm kompresör basma oranları ve tüm türbin giriş sıcaklıklarında klasik turbojet motoruna göre %5 daha fazla itki ürettiği ve %3 daha iyi özgül impuls’a sahip olduğu ortaya konmaktadır. Bu iyileştirmenin sebebi aynı kompresör basıncı ve türbin giriş sıcaklığında daha fazla iş üretebilen patentli özgün termodinamik çevrimdir. 1’e kadar artan ucuş Mach sayısına göre itki ve yakıt tüketimine bakıldığında ise çok düşük Mach sayıları hariç Pars türbojet motorun klasik türbojet motora göre daha üstün performans sergilediği görülmektedir
References
- Akmandor Ibrahim Sinan, Revolving Outer Body Arc Vane Rotary Compressor or Expander, Pars Makina Ltd. USPTO patent pending, 2015
- Akmandor Ibrahim Sinan, Pivoting Hinged Arc Vane Rotary Compressor or Expander, EP 2 495 396 B1, Pars Makina Patent, European patent Office, issued April 2014
- Akmandor Ibrahim Sinan, "Pivoting, Hinged Arc Vane Rotary Compressor or Expander", US 8,579,615 B2, USPTO issued November 12th, 2013
- Akmandor, Ibrahim Sinan and Erzöz, Nazmi; “Rotary Vane Engine and Thermodynamic Cycle”, US 7,314,035 B2, USPTO issued January 1st 2008
- Jack L. Kerrebrock, Aircraft Engines and Gas Turbines, p54, ISBN 0-262-11064-4, 1977, MIT, Alpine Press Inc., USA Okur, investigation of hinged and spring loaded rolling piston compressors pertaining to a turbo rotary engine', Applied Thermal Engineering, Vol:31 No :6-7, pp.1031-1038, (2011)
Abstract
The thrust and fuel consumption levels of a totally indigenous concept named as Pars turbojet and a conventional turbojet engine in the 300 DaN thrust range have been compared to each other. Compared to this conventional turbojet, Pars turbojet uses 35% less air and produces %5 more thrust with 3% better specific impulse accross all compressor pressure ratios and all turbine inlet temperatures. The reason of this performance improvement is the patented novel thermodynamic cycle that can produce more work for same compressor pressure ratio and turbine inlet temperature. Also when flight Mach number was varied from 0 to 1, Pars turbojet exhibited a performance higher than conventional turbojet except for very low Mach numbers
Keywords
Turbo Vane Engine Turbo-Rotary Engine Rolling Piston Compressor and Turbine Highly Efficient
References
- Akmandor Ibrahim Sinan, Revolving Outer Body Arc Vane Rotary Compressor or Expander, Pars Makina Ltd. USPTO patent pending, 2015
- Akmandor Ibrahim Sinan, Pivoting Hinged Arc Vane Rotary Compressor or Expander, EP 2 495 396 B1, Pars Makina Patent, European patent Office, issued April 2014
- Akmandor Ibrahim Sinan, "Pivoting, Hinged Arc Vane Rotary Compressor or Expander", US 8,579,615 B2, USPTO issued November 12th, 2013
- Akmandor, Ibrahim Sinan and Erzöz, Nazmi; “Rotary Vane Engine and Thermodynamic Cycle”, US 7,314,035 B2, USPTO issued January 1st 2008
- Jack L. Kerrebrock, Aircraft Engines and Gas Turbines, p54, ISBN 0-262-11064-4, 1977, MIT, Alpine Press Inc., USA Okur, investigation of hinged and spring loaded rolling piston compressors pertaining to a turbo rotary engine', Applied Thermal Engineering, Vol:31 No :6-7, pp.1031-1038, (2011)
Details
| Other ID | JA98SN79FS |
|---|---|
| Journal Section | Research Article |
| Authors | |
| Publication Date | March 1, 2017 |
| Published in Issue | Year 2017 Volume: 2 Issue: 1 |