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Lorren J Stiles

from Mount Juliet, TN
Age ~75
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Also known as:
Stiles Lorren
Phone and address:
204 Camille Victoria Ct, Mount Juliet, TN 37122
(772) 287-8399
Related to:
Louise StilesElizabeth Stiles, 81
Connected to:
Alane M Stiles, 74Alerie Stiles, 38Amber Stiles, 43Bailey Stiles, 32Baird B Stiles, 61Belinda A Stiles, 59Brian S Stiles, 49Candy Stiles, 64Carl A Stiles, 42Charles E Stiles, 54

Lorren Stiles Phones & Addresses

  • 204 Camille Victoria Ct, Mount Juliet, TN 37122 (772) 287-8399
  • Lebanon, TN
  • 3906 San Clemente Ct, Palm City, FL 34990 (561) 287-8399 (772) 287-8399
  • Roxbury, CT
  • Medford, NJ
  • 3906 SW San Clemente Ct, Palm City, FL 34990 (772) 287-8399

Work

Position: Professional/Technical

Education

Degree: High school graduate or higher

Professional Records

License Records

Lorren Stiles

Address:
3906 SW San Clemente Ct, Palm City, FL 34990
License #:
A1834328
Category:
Airmen

Business Records

Name / Title
Company / Classification
Phones & Addresses
Lorren Stiles
Director
TIBURON PROPERTY OWNERS ASSOCIATION, INC
1047 SW Tiburon Way, Palm City, FL 34990
PO Box 572, Palm City, FL 34991
1074 SW Tiburon Way, Palm City, FL 34990
3906 SW San Clemente Ct, Palm City, FL 34990

Publications

Us Patents

Integrated Hover Display With Augmented Approach To Hover Symbology Cueing For Degraded Visual Environmental Conditions

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US Patent:
7091881, Aug 15, 2006
Filed:
Apr 21, 2005
Appl. No.:
11/111473
Inventors:
John H. Judge - Woodbury CT, US
John J. Occhiato - Derby CT, US
Lorren Stiles - Palm City FL, US
Vineet Sahasrabudhe - Hamden CT, US
Margaret A. MacIsaac - Woodbury CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
G01C 21/00
US Classification:
340979, 340946, 340967, 340973, 340974, 701 14
Abstract:
A flight control system includes a primary flight display having a hover display which facilitates operations in DVE conditions. The hover display includes a radar altitude display, heading drift symbology and lateral drift symbology which assists pilots in the detection of drift, which is common in DVE situations and to provide the pilot with a salient cue pertinent to the approach to hover and landing.

Technical Design Concepts To Improve Helicopter Obstacle Avoidance And Operations In “Brownout” Conditions

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US Patent:
7106217, Sep 12, 2006
Filed:
Mar 31, 2004
Appl. No.:
10/816218
Inventors:
John H. Judge - Woodbury CT, US
John J. Occhiato - Derby CT, US
Lorren Stiles - Palm City FL, US
Vineet Sahasrabudhe - Hamden CT, US
Margaret A. MacIsaac - Woodbury CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
G01C 23/00
US Classification:
340973, 340970, 701 14
Abstract:
A method for flying in a degraded visual environment comprising the steps of collecting environmental data, processing the data and fusing the data together into a combined input output. The output is fed into a head down display, head mounted or heads up display and, preferably to a fly-by-wire vertical take-off and landing capable vehicle wherein the fly-by-wire system makes automatic adjustments to the helicopter.

Full Authority Fly-By-Wire Pedal System

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US Patent:
7644893, Jan 12, 2010
Filed:
Feb 15, 2006
Appl. No.:
11/354687
Inventors:
Bruce Boczar - Seymour CT, US
Lorren Stiles - Palm City FL, US
Peter T. Witiak - Shelton CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B64C 19/02
US Classification:
244235, 244220
Abstract:
A pedal system particularly tailored to a Fly-By-Wire (FBW) flight control system includes a double gradient linkage assembly. The double gradient linkage assembly includes a damper system and a spring system that improves yaw axis (azimuth) control of the aircraft. Control is only required when a change in the yaw axis state is demanded. Since only minimal displacement inputs to such a FBW flight control system is required, the travel of the pedals are exceeding compact, such that pilot workload is significantly reduced through the reduction in the frequency and magnitude of aircraft control inputs.

Surface Contact Override Landing Scheme For A Fbw Rotary-Wing Aircraft

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US Patent:
7742846, Jun 22, 2010
Filed:
Jun 2, 2006
Appl. No.:
11/446464
Inventors:
Todd M. Fanciullo - Tucson AZ, US
Paul Morphy - Williamsville NY, US
Lorren Stiles - Palm City FL, US
Alex Faynberg - Cheshire CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
G05D 1/00
US Classification:
701 4, 701 2, 701 3, 701 8, 701 9, 701 11, 244 11, 244 13, 244 1711, 244 1723, 244175, 340 52, 340945, 340961, 340963, 340970, 342 29, 342 30, 342 34, 342 36
Abstract:
A method of transitioning from a complex response flight state to a ground operation control state. Pilot intent is determined through collective position information to control the transition. An independent cockpit switch activates an emergency surface contact transition function for use with a fly-by-wire (FBW) flight control system. Once the surface contact transition function is active, FBW control laws transition from a fully augmented flight state, through an augmentation deactivation state and into the surface contact state.

Full Authority Fly-By-Wire Pedal System

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US Patent:
7806372, Oct 5, 2010
Filed:
Dec 1, 2009
Appl. No.:
12/628269
Inventors:
Bruce Boczar - Seymour CT, US
Lorren Stiles - Palm City FL, US
Peter T. Witiak - Shelton CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B64C 13/46
B64C 19/02
US Classification:
244223, 244220, 244235
Abstract:
A pedal system particularly tailored to a Fly-By-Wire (FBW) flight control system includes a double gradient linkage assembly. The double gradient linkage assembly includes a damper system and a spring system that improves yaw axis (azimuth) control of the aircraft. Control is only required when a change in the yaw axis state is demanded. Since only minimal displacement inputs to such a FBW flight control system is required, the travel of the pedals are exceeding compact, such that pilot workload is significantly reduced through the reduction in the frequency and magnitude of aircraft control inputs.

Full Authority Fly-By-Wire Pedal System

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US Patent:
7874526, Jan 25, 2011
Filed:
Dec 1, 2009
Appl. No.:
12/628266
Inventors:
Bruce Boczar - Seymour CT, US
Lorren Stiles - Palm City FL, US
Peter T. Witiak - Shelton CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
B64C 19/02
G05G 1/30
US Classification:
244235, 244220, 74512, 74560, 74562
Abstract:
A pedal system particularly tailored to a Fly-By-Wire (FBW) flight control system includes a double gradient linkage assembly. The double gradient linkage assembly includes a damper system and a spring system that improves yaw axis (azimuth) control of the aircraft. Control is only required when a change in the yaw axis state is demanded. Since only minimal displacement inputs to such a FBW flight control system is required, the travel of the pedals are exceeding compact, such that pilot workload is significantly reduced through the reduction in the frequency and magnitude of aircraft control inputs.

Integrated Hover Display With Radar Altitude Predictor For Indicating Height Above Ground

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US Patent:
20060238377, Oct 26, 2006
Filed:
Jun 20, 2006
Appl. No.:
11/471087
Inventors:
Lorren Stiles - Palm City FL, US
Margaret MacIsaac - Woodbury CT, US
International Classification:
G01C 21/00
US Classification:
340979000
Abstract:
A flight control system includes a primary flight display having a hover display which facilitates operations in DVE conditions. The hover display includes a radar altitude display, heading drift symbology and lateral drift symbology which assists pilots in the detection of drift, which is common in DVE situations and to provide the pilot with a salient cue pertinent to the approach to hover and landing.

Methods And Systems Involving Viewing Angles In Aircraft Displays

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US Patent:
20110254706, Oct 20, 2011
Filed:
Feb 4, 2011
Appl. No.:
13/021028
Inventors:
Margaret M. Lampazzi - Woodbury CT, US
Lorren Stiles - Palm City FL, US
Jena D. Salvetti - Owens Cross Roads AL, US
Gang He - Morristown NJ, US
Assignee:
SIKORSKY AIRCRAFT CORPORATION - Stratford CT
International Classification:
G01C 23/00
US Classification:
340975
Abstract:
A method and system for presenting environmental data including receiving environmental data from a sensor, processing the data to generate a graphical representation of the environment, wherein the view point of the graphical representation of the environment is a distance (d) and an angle (θ) relative to a point in an aircraft, and presenting the graphical representation of the environment to a user on a display.
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Lorren J Stiles from Mount Juliet, TN, age ~75 Get Report