JOHN CHRISTIAN JASANY
Pilots at Compton Rd, Cincinnati, OH
License number
Ohio A3951564
Issued Date
Oct 2016
Expiration Date
Apr 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
265 Compton Rd, Cincinnati, OH 45215
Professional information
High-Emissivity Infrared Coating Applications For Use In Hirss Applications
US Patent:
7313909, Jan 1, 2008
Filed:
Oct 25, 2004
Appl. No.:
10/972552
Inventors:
Andrew Jay Skoog - West Chester OH, US
Jane Ann Murphy - Middletown OH, US
John Michael Jasany - Cincinnati OH, US
Aaron Dennis Gastrich - Loveland OH, US
Timothy Lance Manning - Cincinnati OH, US
Jane Ann Murphy - Middletown OH, US
John Michael Jasany - Cincinnati OH, US
Aaron Dennis Gastrich - Loveland OH, US
Timothy Lance Manning - Cincinnati OH, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 7/08
US Classification:
60 395
Abstract:
A high emissivity (Hi-E) coating for use on the exhaust baffles of HIRSS systems. HIRSS systems were developed to reduce the infrared (IR) signature of helicopter engines. Increasing operating temperatures of helicopter engines have made the HIRSS systems less effective. An infrared coating applied over selected portions of the HIRSS reduces the IR of the system. The Hi-E coating comprises, in weight percent, 30-80% refractory oxide pigment, 5-20% binder, 1-15% potassium oxide, optionally up to about 15% glass-forming material and the balance refractory oxide powder. When applied to provide a surface finish of 1100Rmicroinches or coarser, the coated HIRSS has a significantly reduced hemispherical reflectance in the IR frequency range.
High Reflectivity Infrared Coating Applications For Use In Hirss Applications
US Patent:
2009031, Dec 24, 2009
Filed:
May 2, 2007
Appl. No.:
11/743303
Inventors:
Andrew Jay SKOOG - West Chester OH, US
Jane Ann MURPHY - Franklin OH, US
John Michael JASANY - Cincinnati OH, US
Mariah Dawn SENTER - Mason OH, US
Jane Ann MURPHY - Franklin OH, US
John Michael JASANY - Cincinnati OH, US
Mariah Dawn SENTER - Mason OH, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
F02C 7/24
US Classification:
415177
Abstract:
The present invention is a hover infrared suppression system for a gas turbine engine comprising a hover infrared suppression system having an upstream first stage, a second stage downstream of the first stage and a third stage downstream of the second stage, the engine operating at a temperature sufficient to cause the hover infrared suppression system to emit infrared radiation. The present invention further comprises a high reflectivity coating applied over a preselected area of at least one of the stages of the hover infrared suppression system to reduce the infrared radiation emitted from the engine, the high reflectivity coating being fired after application.
High Reflectivity Infrared Coating Applications For Use In Hirss Applications
US Patent:
2006008, Apr 27, 2006
Filed:
Oct 25, 2004
Appl. No.:
10/972553
Inventors:
Andrew Skoog - West Chester OH, US
Jane Murphy - Middletown OH, US
John Jasany - Cincinnati OH, US
Mariah Senter - Mason OH, US
Jane Murphy - Middletown OH, US
John Jasany - Cincinnati OH, US
Mariah Senter - Mason OH, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
B32B 15/00, B32B 15/01, B05D 1/02, B05D 1/28, B05D 3/02, B05D 3/00
US Classification:
428670000, 428655000, 428660000, 428668000, 427429000, 427421100, 427372200, 427299000
Abstract:
The present invention is a hover infrared suppression system for a gas turbine engine comprising a hover infrared suppression system having an upstream first stage, a second stage downstream of the first stage and a third stage downstream of the second stage, the engine operating at a temperature sufficient to cause the hover infrared suppression system to emit infrared radiation. The present invention further comprises a high reflectivity coating applied over a preselected area of at least one of the stages of the hover infrared suppression system to reduce the infrared radiation emitted from the engine, the high reflectivity coating being fired after application.
Method And Apparatus For Suppressing Infrared Signatures
US Patent:
2005026, Dec 8, 2005
Filed:
Jun 8, 2004
Appl. No.:
10/862994
Inventors:
William Steyer - Topsfield MA, US
Christopher Kieffer - Revere MA, US
John Jasany - Cincinnati OH, US
Jacob Hoffman - Ipswich MA, US
Christopher Kieffer - Revere MA, US
John Jasany - Cincinnati OH, US
Jacob Hoffman - Ipswich MA, US
International Classification:
F02K001/38
US Classification:
060204000, 060262000, 060039500
Abstract:
An infrared signature suppression system for reducing infrared radiation emitted by a vehicle. The system includes an elongate duct mounted on the vehicle having a hollow interior extending along an axial centerline between an upstream end and a downstream end for transporting exhaust gas emitted by the vehicle, and a baffle positioned in the hollow interior of the duct between the upstream end and the downstream end. At least a portion of at least one of the duct and the baffle includes an emissivity coating for reducing infrared radiation emitted by the vehicle.
One-Piece Baffle Infrared Suppressor Apparatus And Method
US Patent:
7607305, Oct 27, 2009
Filed:
Aug 3, 2005
Appl. No.:
11/196218
Inventors:
William Steyer - Topsfield MA, US
Christopher Marlow Kieffer - Revere MA, US
John Michael Jasany - Cincinnati OH, US
Christopher Marlow Kieffer - Revere MA, US
John Michael Jasany - Cincinnati OH, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02K 1/00
US Classification:
60770, 60 395, 23926517
Abstract:
A method for suppressing infrared radiation from an aircraft engine includes directing hot exhaust from the aircraft engine into a lobed mixer of a single baffle infrared suppressor having a single baffle assembly to generate alternating flows of hot exhaust gas and cold air. The method further includes directing the alternating flows of hot exhaust gas and cold air towards the single baffle assembly to mix the hot exhaust gas with the cold air.