Harsh Vinayak - Meriden CT, US Bruce D. Hansen - Shelton CT, US Edward J. Karedes - Cheshire CT, US Clark V. Cooper - Glastonbury CT, US Lawrence M. Zunski - Seymour CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B23P015/14
US Classification:
2989335, 29893, 298933, 74462, 451 47
Abstract:
A method for improving acoustic and vibrational properties of gears includes determining the transmission errors of intermeshing gears due to stiffness variations in the gear teeth, performing Gear Tooth Topological (GTT) modifications to compensate for the errors, and isotropically processing the gears to produce an ultra-smooth surface finish. Additional errors from isotropic processing, machining, loading, thermal effects and/or load sharing may be summed with the errors from the stiffness variations and used for the GTT modifications. The teachings of the present invention may reduce noise by as much as 13 to 15 dB.
Yuriy Gmirya - Woodbridge CT, US Harsh Vinayak - Meriden CT, US David Andrew Binney - Beacon Falls CT, US Lawrence Mark Zunski - Seymour CT, US Vincent F. Millea - Stratford CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
F16H 57/00
US Classification:
74410, 74423, 74664
Abstract:
A split torque gearbox having multiple input shafts. Each input shaft is connected to two face gears. Each face gear is connected to two quill shafts, one is coaxially mounted and the second is not coaxially mounted. Of the two quill shafts, one is positioned on a first side of an output stage and a second quill shaft is located on a second side of the output stage and the quill shafts are connected thereto. The output stage is connected to a main shaft.
Variable Speed Gearbox With An Independently Variable Speed Tail Rotor System For A Rotary Wing Aircraft
A gearbox of a rotary-wing aircraft includes at least one variable speed system which optimizes the main rotor speed for different flight regimes such as a hover flight profile and a high speed cruise flight profile for any rotary wing aircraft while maintaining an independently variable tail rotor speed.
Variable Speed Gearbox With An Independently Variable Speed Tail Rotor System For A Rotary Wing Aircraft
Nicholas D. Lappos - Stratford CT, US Edward Karedes - Cheshire CT, US Harsh Vinayak - Meriden CT, US Yuriy Gmirya - Woodbridge CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B64C 27/04
US Classification:
244 1711, 244 1719, 244 1723, 244 60
Abstract:
A gearbox of a rotary-wing aircraft includes at least one variable speed system which optimizes the main rotor speed for different flight regimes such as a hover flight profile and a high speed cruise flight profile for any rotary wing aircraft while maintaining an independently variable tail rotor speed.
Method For Processing Alloys Via Plasma (Ion) Nitriding
Clark VanTine Cooper - Glastonbury CT, US Krassimir G. Marchev - Sudbury MA, US Bill C. Giessen - Cambridge MA, US Raymond C. Benn - Madison CT, US Edward H. Bittner - Madison CT, US Harsh Vinayak - Meriden CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
C23C 8/24 C23C 8/48 C23C 22/00
US Classification:
148238, 148317
Abstract:
A surface processing method and power transmission component includes transforming a surface region of a metal alloy into a hardened surface region at a temperature that is less than a heat treating temperature of the metal alloy. The metal alloy includes about 11. 1 wt % Ni, about 13. 4 wt % Co, about 3. 0 wt % Cr, about 0. 2 wt % C, and about 1. 2 wt % Mo which reacts with the C to form a metal carbide precipitate of the form MC. The surface processing temperature, vacuum pressure, precursor gas flow and ratio, and time of processing are controlled to provide a desirable hardened surface region having a gradual transition in nitrogen concentration.
Load Sharing Gear For High Torque, Split-Path Transmissions
Yuriy Gmirya - Woodbridge CT, US Harsh Vinayak - Meriden CT, US
International Classification:
F16H055/18
US Classification:
074/410000, 074/409000
Abstract:
A gear adapted to provide load sharing in a torque split transmission module wherein at least one spring element is disposed in combination with a torque driving shaft at one end thereof and in combination with a ring of torque transmitting gear teeth at the other end thereof. The spring element is radially stiff to center the ring of gear teeth about the shaft and is torsionally soft to permit relative rotational displacement between the gear teeth and the shaft. The spring element is substantially disc shaped and includes a plurality of recurved radial spokes. More specifically, the spokes project radially outboard from a first mounting ring, define a 180 degree bend proximal to the gear teeth, and extend inwardly toward a second mounting ring. A pair of spring elements may be used wherein the first mounting ring of each spring element connects to shaft flange and the second mounting ring mounts to an inboard end of a radial flange of the gear teeth. Furthermore, each of the pair of spring elements is disposed on either side of the radial flange to balance the spring force about a medial plane defined by the ring of gear teeth. A manufacturing method for fabricating the spring element is also disclosed.
Clark Cooper - Glastonbury CT, US Charles Isabelle - Barkhamsted CT, US Harsh Vinayak - Meriden CT, US Jules Kish - Milford CT, US Robin Miller - Ellington CT, US Glenn Levasseur - Colchester CT, US Edward Karedes - Cheshire CT, US Anthony Chory - Trumbull CT, US Stephen Sammataro - Madison CT, US Michael Mullen - Cheshire CT, US Bruce Hansen - Shelton CT, US Mark Davis - Vernon CT, US
International Classification:
F16H057/08
US Classification:
074462000
Abstract:
A transmission provides for the application of higher design allowables in bending, pitting, and scoring, as enabled by surface-engineering (SE) processes such as isotropic superfinishing and Me-DLC coating to effect increases in the power density of transmission systems.
Method For Processing Alloys Via High-Current Density Ion Implantation
Clark Cooper - Glastonbury CT, US Raymond Benn - Madison CT, US Edward Bittner - Madison CT, US Harsh Vinayak - Meriden CT, US
International Classification:
C23C 8/24
US Classification:
148220000, 148222000, 148230000, 148239000
Abstract:
A surface processing method and power transmission component includes transforming by high current density ion implantation (high intensity plasma ion processing) a surface region of a metal alloy into a hardened surface region at a temperature that is less than a heat treating temperature of the metal alloy. The metal alloy includes between 1.5 wt % and 15 wt % Ni, between 5 wt % and 30 wt % Co, up to 1.0 wt % carbon, and up to 15 wt % of a carbide-forming element, such as molybdenum, chromium, tungsten, vanadium or combinations thereof, that can react with carbon to form metal carbide precipitates of the form MC. The surface processing temperature, vacuum pressure, precursor gas flow and ratio, and time of processing are controlled to provide a desirable hardened surface region having a gradual transition in nitrogen concentration. A vapor deposition process deposits an amorphous hydrogenated carbon coating on the hardened surface region of the metal alloy. An intermediate coating between the coating and the hardened surface region promotes adhesion between the coating and hardened surface region.
NIIT Technologies Windsor, CT Jan 2012 to May 2012 Analyst, Team LeadSenior Software Engineer Aug 2010 to Dec 2011NIIT Technologies New Delhi, Delhi Jul 2007 to Jul 2010 Software Engineer
Education:
Carnegie Mellon University Silicon Valley, CA Aug 2013 to 2000 Master of Science in Software ManagementJaypee Institute of Information Technology University Noida, Uttar Pradesh Jul 2003 to Apr 2007 Bachelor of Technology in Computer Science and EngineeringCarnegie Institute of Technology
Quixey Mountain View, CA Aug 2014 to Dec 2014 Product Management InternCarnegie Mellon University
Sep 2013 to Dec 2014 Research AssistantCarnegie Mellon University Mountain View, CA May 2014 to Aug 2014 Project Management InternNIIT Technologies Windsor, CT Jan 2012 to May 2012 Tech Analyst, Team LeadNIIT Technologies Ltd
Aug 2010 to Dec 2011 Senior Software EngineerNIIT Technologies Ltd New Delhi, Delhi Jul 2007 to Jul 2010 Software Engineer
Education:
Carnegie Mellon University Silicon Valley, CA Aug 2013 to Dec 2014 Master of Science in Software ManagementJaypee Institute of Information Technology University Noida, Uttar Pradesh Jul 2003 to Apr 2007 Bachelor of Technology in Computer Science and Engineering
hi5 Profile page for Harsh Vinayak (Noida,India). Harsh Vinayak is . Harsh Vinayak has 12 friends and 1 photos. Join hi5 and become friends with Harsh ...
Googleplus
Harsh Vinayak
Youtube
Back to Classroom: Harsh Vinayak
Harsh Vinayak, Senior VP, NTT Data on things that startups must keep i...