Technologies Developed

 
 
  • Improved Tandoor Oven,  patent No:1292/DEL/2004 (D P Mishra,)

  • Recuperative Vortex LPG Burner, IPA No: 3197/DEL/2005 (D P Mishra)

  • Heat Recuperating Microcombustor, IPA No:2257/DEL/2009 (D P Mishra, and S J Swarup)

  • Low emission energy efficient gas burner,  IPA No: 2347/DEL/2009 (D P Mishra)

  • Two-fluid Atomizer,   IPA NO: 1551/DEL/2013 (D. P. Mishra & Manisha B P)

  • Hydrogen Gas Burner and Method of Combustion in Hydrogen Burner, 2013, IPA NO: 2545/DEL/2013 (D. P. Mishra)

  • Estimation of inertia tensor and center of gravity of a vehicle on a three axis platform,

  • Patent Application No.  2365/DEL/2007  Dated: 13-11-2007 (Sanjeev K. Gupta, A. Kushari, C. S. Upadhyay and C. Venkatesan)

  • Profile measurement machine, Patent Application No. 1656/DEL/2007  Dated: 03-08-2007 (Sanjeev K. Gupta, A. Kushari, C. S. Upadhyay and C. Venkatesan)

  • Piston based resister, Patent Application No.1886/Del/2007 Dated:06-09-2007(Sanjeev K. Gupta, A. Kushari, C. S. Upadhyay and C. Venkatesan)

  • A Twin- Fluid Internally Mixed Swirl Atomizer (A. Kushari, M. S. Rawat)

  • Profile measuring Machine: Patent Application No. 1656/DEL/2007  Dated: 03-08-2007 (Sanjeev K. Gupta, A. Kushari, C. S. Upadhyay and C. Venkatesan)

  • Piston based resister: Patent Application No.1886/Del/2007 Dated:06-09-2007(Sanjeev K. Gupta, A. Kushari, C. S. Upadhyay and C. Venkatesan)

  • Estimation of inertia tensor and centre of gravity of a vehicle on the three axis platform: Patent Application No.  2365/DEL/2007  Dated: 13-11-2007 (Sanjeev K. Gupta, A. Kushari, C. S. Upadhyay and C. Venkatesan)

  • An Arrangement for jet engine to reduce noise     Patent Application No: 3603/DEL/2011 Dated: 12-12-2011 (A. Kushari,  Mukul Atri (Student,AE), Sriram Ganesan (Student, AE)

Technology Transferred to Industry

  • A comprehensive analysis code for prediction of helicopter blade loads and flight dynamics, fully developed and validated at IIT Kanpur, had been transferred to HAL and is being used to study general steady maneuvering flight.

 

 

 
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