JARY EUGENE ENGELS
Pilots at 71 Dr, Peoria, AZ
License number
Arizona A0547565
Issued Date
Jan 2017
Expiration Date
Jul 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
13369 N 71St Dr, Peoria, AZ 85381
Professional information
Method And Apparatus For Gesture Recognition
US Patent:
2012011, May 3, 2012
Filed:
Oct 29, 2010
Appl. No.:
12/915452
Inventors:
Robert W. Sparks - San Diego CA, US
Jary Engels - Peoria AZ, US
John Woltkamp - Fountain Hills AZ, US
Jary Engels - Peoria AZ, US
John Woltkamp - Fountain Hills AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
G06F 3/01, G06F 3/041
US Classification:
715863, 345173
Abstract:
A touchscreen device is configured to display a number of user interface elements in accordance with a menu hierarchy. Upon receipt of a predetermined touchscreen gesture (e.g., the circular motion of a manipulator) the menu hierarchy is bypassed and the user is given immediate control over a selected function, for example, a tuning function such as audio volume, screen contrast, and the like.
Head-Down Aircraft Attitude Display And Method For Displaying Schematic And Terrain Data Symbology
US Patent:
7218245, May 15, 2007
Filed:
Jan 13, 2005
Appl. No.:
11/034582
Inventors:
Ivan S. Wyatt - Scottsdale AZ, US
Thomas M. Leard - Carefree AZ, US
Jary E. Engels - Peoria AZ, US
Thomas M. Leard - Carefree AZ, US
Jary E. Engels - Peoria AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G01C 23/00
US Classification:
340973, 340979, 345619
Abstract:
Methods and apparatus are provided for displaying terrain data symbology for an aircraft. The apparatus is a heads-down display for an aircraft having a monitor configured to generate a display and a processor coupled to the display. The display has a centerline. The processor is configured to align the centerline of the display with a track of the aircraft, and generate on the display a first symbol corresponding to a terrain and a second symbol corresponding to an attitude of the aircraft. The processor is further configured to position the first symbol and the second symbol with reference to the track of the aircraft.
System And Methods For Rendering Taxiway And Runway Signage In A Synthetic Display Of An Airport Field
US Patent:
2011019, Aug 11, 2011
Filed:
Feb 9, 2010
Appl. No.:
12/702950
Inventors:
Thea L. Feyereisen - Hudson WI, US
Troy Nichols - Peoria AZ, US
John G. Suddreth - Cave Creek AZ, US
Ivan Sandy Wyatt - Scottsdale AZ, US
Jary Engels - Peoria AZ, US
Gang He - Morristown NJ, US
Troy Nichols - Peoria AZ, US
John G. Suddreth - Cave Creek AZ, US
Ivan Sandy Wyatt - Scottsdale AZ, US
Jary Engels - Peoria AZ, US
Gang He - Morristown NJ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
G06G 7/76, G06F 19/00
US Classification:
701120
Abstract:
A system and methods of displaying airport field features on a flight deck display element of an aircraft are provided. The flight deck display system obtains geographic position data and heading data for the aircraft, accesses airport feature data associated with synthetic graphical representations of an airport field, and renders a dynamic synthetic display of the airport field on the flight deck display element. The dynamic synthetic display is rendered in accordance with the geographic position data, the heading data, and the airport feature data. In certain embodiments the synthetic display includes graphical representations of taxiways/runways, along with signage that is conformally rendered on the exposed taxiway surfaces. Display characteristics of the signage may be influenced by the actual physical and/or temporal proximity of the aircraft relative to reference locations on the airport field. In some embodiments, the taxiway/runway signage includes dynamic directional indicators corresponding to the intended directions of travel on the taxiways/runways. Moreover, the taxiway/runway signage can be dynamically rendered in a forward-facing manner at all times on the flight deck display element.
System And Method For Increasing Visibility Of Critical Flight Information On Aircraft Displays
US Patent:
7834779, Nov 16, 2010
Filed:
Jun 29, 2005
Appl. No.:
11/170498
Inventors:
Gang He - Morristown NJ, US
Thea L. Feyereisen - Hudson WI, US
Aaron J. Gannon - Anthem AZ, US
Blake W. Wilson - Peoria AZ, US
Jary E. Engels - Peoria AZ, US
Ivan S Wyatt - Scottsdale AZ, US
Thea L. Feyereisen - Hudson WI, US
Aaron J. Gannon - Anthem AZ, US
Blake W. Wilson - Peoria AZ, US
Jary E. Engels - Peoria AZ, US
Ivan S Wyatt - Scottsdale AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G01C 23/00
US Classification:
340973, 340974, 701 14
Abstract:
System and method increase the visibility of critical flight information on electronic displays. An aircraft display system includes a processing unit, a flight management system, a navigation system, a database for storing target data and terrain data, a graphics display generator, and a visual display. The flight management system and/or the navigation system provide real-time aircraft operational and flight control information. The processing unit directs the graphics display generator to generate graphic control signals for the visual display, which increase the transparency of a segment of a zero pitch reference line in the vicinity of a flight path marker on the display.
Airspace Awareness Enhancement System And Method
US Patent:
8554393, Oct 8, 2013
Filed:
Sep 25, 2009
Appl. No.:
12/566942
Inventors:
Gang He - Morristown NJ, US
Jary Engels - Peoria AZ, US
Jary Engels - Peoria AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G06F 7/70
US Classification:
701 14
Abstract:
A display system and method for an aircraft renders various airspaces and associated airspace types on an aircraft display device. An image is selectively rendering on the aircraft display device that includes at least an airspace boundary graphic representative of at least a portion of the boundary for the airspace, and a textual airspace type designation label representative of the airspace type of the airspace.
Apparatus And Method For Display And Functionality Of A Vehicle Display System Cursor Control Device
US Patent:
8519997, Aug 27, 2013
Filed:
Sep 23, 2008
Appl. No.:
12/235769
Inventors:
John F. Suddreth - Cave Creek AZ, US
Gang He - Morristown NJ, US
Kenneth M. Leiphon - Phoenix AZ, US
Ivan Sandy Wyatt - Scottsdale AZ, US
Jary E. Engels - Peoria AZ, US
Thea L. Feyereisen - Hudson WI, US
Gang He - Morristown NJ, US
Kenneth M. Leiphon - Phoenix AZ, US
Ivan Sandy Wyatt - Scottsdale AZ, US
Jary E. Engels - Peoria AZ, US
Thea L. Feyereisen - Hudson WI, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G06T 15/00
US Classification:
345419, 715700
Abstract:
A display system for use on a vehicle is presented. The display system comprises a cursor control device, at least one electronic display for displaying a first image comprising a three-dimensional conformal view of a terrain and a first movable cursor, and a processor that is coupled to the cursor control device and the at least one electronic display. The processor is configured to move the first movable cursor on the first image in response to input from the cursor control device and to determine a latitude and longitude that correspond to the position of the first movable cursor.
Low Speed Range Indicator
US Patent:
2004021, Oct 21, 2004
Filed:
Apr 2, 2003
Appl. No.:
10/406692
Inventors:
John Gaidelis - Glendale AZ, US
Thomas Frazier - Scottsdale AZ, US
Jary Engels - Peoria AZ, US
Thomas Leard - Carefree AZ, US
Clarence Nygaard - Glendale AZ, US
Robert Odgers - Litchfield Park AZ, US
David Tunheim - Scottsdale AZ, US
Ivan Wyatt - Scottsdale AZ, US
Thomas Frazier - Scottsdale AZ, US
Jary Engels - Peoria AZ, US
Thomas Leard - Carefree AZ, US
Clarence Nygaard - Glendale AZ, US
Robert Odgers - Litchfield Park AZ, US
David Tunheim - Scottsdale AZ, US
Ivan Wyatt - Scottsdale AZ, US
International Classification:
G06F007/00
US Classification:
701/004000
Abstract:
In an aircraft flight instrument display system having a display screen for displaying flight information, an airspeed indicator is displayed in a vertical tape format, and has a low speed range indicator with a low speed range identified on the airspeed indicator by highlighting the low speed range, and has at least a settable indicator within the low speed range indicating a critical airspeed. The low speed range indicator and the critical airspeed indicator are both set with only manual inputs.
Dynamic Primary Flight Displays For Unusual Attitude Conditions
US Patent:
7403133, Jul 22, 2008
Filed:
Oct 13, 2005
Appl. No.:
11/250124
Inventors:
Gang He - Morristown NJ, US
Ivan S Wyatt - Scottsdale AZ, US
Jary E. Engels - Peoria AZ, US
Thea L. Feyereisen - Hudson WI, US
Aaron J. Gannon - Anthem AZ, US
Blake W. Wilson - Peoria AZ, US
Ivan S Wyatt - Scottsdale AZ, US
Jary E. Engels - Peoria AZ, US
Thea L. Feyereisen - Hudson WI, US
Aaron J. Gannon - Anthem AZ, US
Blake W. Wilson - Peoria AZ, US
Assignee:
Honeywell International, Inc. - Morristown NJ
International Classification:
G01C 21/00
US Classification:
340974, 340975, 701 4
Abstract:
Embodiments of the present invention provide a method of dynamically transitioning into a distinct display format during unusual attitude conditions. In one embodiment, the method includes collecting attitude data, comparing current attitude to a first set attitude angle, and fading a distinct display format into a display for unusual attitude conditions when current attitude is at least equal to the first set attitude angle.
Altimeter Setting Display And Storage System And Method
US Patent:
7873446, Jan 18, 2011
Filed:
Feb 13, 2007
Appl. No.:
11/706671
Inventors:
Christopher J. Shehi - Glendale AZ, US
Jary E. Engels - Peoria AZ, US
Jary E. Engels - Peoria AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G06F 17/00
US Classification:
701 4, 701 9, 345 7, 340977
Abstract:
A system and method for storing altimeter setting values on an aircraft display includes simultaneously rendering an altimeter and an active altimeter setting field, and selectively rendering a standby altimeter setting field simultaneously with the altimeter and the active altimeter setting field. An active altimeter setting value is rendered in the active altimeter setting field, and a stored altimeter setting value may be rendered in the standby altimeter setting field. Preferably, the stored altimeter setting value is selectively rendered in the standby altimeter setting field when the standby altimeter setting field is simultaneously rendered with the altimeter and the active altimeter setting field.
System And Method For Rendering A Sky Veil On A Vehicle Display
US Patent:
2013014, Jun 13, 2013
Filed:
Dec 7, 2011
Appl. No.:
13/313859
Inventors:
Vivek Jain - Panchkula, IN
David A. Wright - Phoenix AZ, US
Jason F. Harvey - Glendale AZ, US
Jary Engels - Peoria AZ, US
David A. Wright - Phoenix AZ, US
Jason F. Harvey - Glendale AZ, US
Jary Engels - Peoria AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G09G 5/02, G09G 5/00
US Classification:
345589, 345629
Abstract:
Methods and systems are provided for improving pilot situational awareness during brown-over-brown display situations. An image is rendered, on a display, that includes one of, or both, rendered terrain and rendered sky. A sky veil is at least selectively rendered on a portion of the display. The sky veil, when rendered, is rendered at least partially transparent and in a manner that portions of the sky veil that overlap with rendered sky are not discernable, and rendered terrain is viewable through portions of the sky veil that overlap with terrain.