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Dennis D Olcott

from Castle Pines, CO
Age ~56
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Also known as:
Dennis Duane Olcott, Dennis Olson
Phone and address:
6761 Catarata Pl, Castle Rock, CO 80108
Related to:
Richard M OlcottJay D Olcott, 53Brian Olcott, 27Edward W Glines, 58Casey J Burback, 56Robert J ColemanSheri J Olcott, 58Haley J Olcott, 29Eddy W Glines, 58Coleman Z Aleisha, 52Dianna Olcott, 60Harold D Coleman, 85Carolee P Coleman, 80Karen C Coleman, 81Sheri ColemanTravis Coleman, 51
Connected to:
Ashley E Olcott, 40Eric A Olcott, 43Henry E Olcott, 76Ivy O Olcott, 96Judy D Olcott, 79Kelly J Olcott, 52Marie H Olcott, 98Marla B Olcott, 58Roger J Olcott, 68Roy H Olcott, 33

Dennis Olcott Phones & Addresses

  • 6761 Catarata Pl, Castle Rock, CO 80108
  • Castle Pines, CO
  • Dillon, CO
  • 550 Camelia Ct, Vero Beach, FL 32963 (772) 231-5235 (772) 234-2568
  • 1245 Spanish Lace Ln, Vero Beach, FL 32963 (772) 231-5235
  • Lone Tree, CO
  • Littleton, CO
  • Hurst, TX
  • Lone Tree, CO
  • Provo, UT
  • Tehachapi, CA
  • Montrose, CO

Professional Records

License Records

Dennis D Olcott

Address:
Castle Rock, CO
License #:
260483-2202 - Active
Category:
Engineer/Land Surveyor
Issued Date:
Nov 14, 1995
Expiration Date:
Mar 31, 2017
Type:
Professional Engineer

Dennis Duane Olcott

Address:
6761 Catarata Pl, Castle Pines, CO 80108
License #:
46412 - Active
Issued Date:
Jun 1, 2012
Renew Date:
Nov 1, 2015
Expiration Date:
Oct 31, 2017
Type:
Professional Engineer

Dennis Duane Olcott

Address:
6761 Catarata Pl, Castle Pines, CO 80108
License #:
A2518473
Category:
Airmen

Business Records

Name / Title
Company / Classification
Phones & Addresses
Dennis Olcott
Principal
Mountain Aircraft LLC
Mfg Aircraft · Nonclassifiable Establishments
6761 Catarata Pl, Castle Rock, CO 80108
Dennis Olcott
Managing Partner
Answer Engineering, Llp
Engineering Services
19751 E Mainstreet, Parker, CO 80138
(303) 379-9943
Dennis Olcott
President, Vice President
Vero Beach High School Xc Boosters, Inc
Elementary/Secondary School
1707 16 St, Vero Beach, FL 32960
225 Ocean Way, Vero Beach, FL 32963
716 24 Sq, Vero Beach, FL 32962
Dennis Olcott
Chief Engineer, Senior Vice-President
Adamworks, LLC
Mfg Plastic Products Engineering Services
7367 S Revere Pkwy, Englewood, CO 80112
7367 S Revere Pkwy, Centennial, CO 80112
(303) 200-6655

Publications

Us Patents

Aircraft

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US Patent:
D500729, Jan 11, 2005
Filed:
Feb 25, 2004
Appl. No.:
29/200138
Inventors:
Joe Wilding - Elizabeth CO, US
Dennis D. Olcott - Lone Tree CO, US
Greg Cole - Bend OR, US
Assignee:
Adam Aircraft Industries - Englewood CO
International Classification:
1299
US Classification:
D12319

Aircraft

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US Patent:
D500981, Jan 18, 2005
Filed:
Feb 25, 2004
Appl. No.:
29/200129
Inventors:
Joe Wilding - Elizabeth CO, US
Dennis D. Olcott - Lone Tree CO, US
Greg Cole - Bend OR, US
Assignee:
Adam Aircraft Industries - Englewood CO
International Classification:
1299
US Classification:
D12319

Hybrid Composite-Metal Energy Absorbing Seat

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US Patent:
6896324, May 24, 2005
Filed:
Apr 21, 2003
Appl. No.:
10/420566
Inventors:
Matthew H. Kull - Parker CO, US
Dennis D. Olcott - Lone Tree CO, US
Sharon M. Wilson - Colorado Springs CO, US
Assignee:
Adam Aircraft Industries - Englewood CO
International Classification:
B60N002/42
A47C007/02
US Classification:
2972161, 29721613, 29745218, 29745219, 2974522, 29745255
Abstract:
A hybrid composite-metal energy absorbing seat is described. According to one embodiment, an aircraft seat includes a seat base assembly and a seat back assembly. The seat base assembly includes multiple rigid metal seat base side frame elements joined by a lower seat pan, an energy absorbing element placed on the lower seat pan to deform and absorb downward energy in a crash, and a contoured seat pan whose sides extend past the seat base side frame elements and deform to absorb downward energy in a crash. The seat back assembly is attached to the seat base assembly and includes multiple rigid metal seat back side frame elements joined by a contoured composite seat back. The rigid metal seat back side frame elements absorb forward crash load energy by permanently deforming during a severe forward crash load. The contoured composite seat back provides design/aesthetic flexibility.

Hybrid Composite-Metal Energy Absorbing Seat

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US Patent:
7083230, Aug 1, 2006
Filed:
Mar 3, 2005
Appl. No.:
11/072904
Inventors:
Matthew H. Kull - Parker CO, US
Dennis D. Olcott - Lone Tree CO, US
Sharon M. Wilson - Colorado Springs CO, US
Assignee:
Adam Aircraft Industries - Englewood CO
International Classification:
B60N 2/42
A47C 7/02
US Classification:
2972161, 29721613, 29745218, 29745219, 2974522, 29745255
Abstract:
A hybrid composite-metal energy absorbing seat is described. According to one embodiment, an aircraft seat includes a seat base assembly and a seat back assembly. The seat base assembly includes multiple rigid metal seat base side frame elements joined by a lower seat pan, an energy absorbing element placed on the lower seat pan to deform and absorb downward energy in a crash, and a contoured seat pan whose sides extend past the seat base side frame elements and deform to absorb downward energy in a crash. The seat back assembly is attached to the seat base assembly and includes multiple rigid metal seat back side frame elements joined by a contoured composite seat back. The rigid metal seat back side frame elements absorb forward crash load energy by permanently deforming during a severe forward crash load. The contoured composite seat back provides design/aesthetic flexibility.

Methods For Manufacturing Composite Aircraft, Parts And A Family Of Composite Aircraft

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US Patent:
7478780, Jan 20, 2009
Filed:
Oct 14, 2005
Appl. No.:
11/249502
Inventors:
Joseph Ray Wilding - Elizabeth CO, US
Dennis D. Olcott - Lone Tree CO, US
Assignee:
AAI Acquisition, Inc. - Englewood CO
International Classification:
B64C 1/00
US Classification:
244119, 156242, 156245, 264219
Abstract:
The invention relates to systems and methods for manufacturing composite parts for aircraft. In one innovative aspect, a system and method for adjusting a location of a center of gravity of an aircraft relative to a center of lift of a wing of the aircraft is disclosed, wherein a modular spar tunnel mold is provided and configured to be detachably fixed at a plurality of selected locations within a main mold for a fuselage portion of the aircraft. In another innovative aspect, a movable detail or mold is used for manufacturing complex composite parts for an aircraft. In yet another innovative aspect, a movable detail is used to fabricate a common feature for a plurality of different parts for one or more aircraft or a family of aircraft of similar design.

Modular Spar Tunnel

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US Patent:
20040217235, Nov 4, 2004
Filed:
Apr 15, 2003
Appl. No.:
10/414390
Inventors:
Joseph Wilding - Elizabeth CO, US
Dennis Olcott - Lone Tree CO, US
International Classification:
B64C001/06
US Classification:
244/119000, 156/189000, 264/219000
Abstract:
A system and method for adjusting a location of a center of gravity of an aircraft relative to a center of lift of a wing of the aircraft. In one innovative aspect, a modular spar tunnel mold is provided and configured to be detachably fixed at a selected location within a main mold for a fuselage portion of the aircraft.

Vtol Aircraft

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US Patent:
20160214710, Jul 28, 2016
Filed:
May 7, 2015
Appl. No.:
14/706407
Inventors:
- Greenwood Village CO, US
Dennis D. Olcott - Castle Pines CO, US
International Classification:
B64C 27/28
B64C 27/26
B64C 9/00
B64C 29/00
Abstract:
A vertical takeoff and landing aircraft includes a pair of ducted lift/thrust fans that are rotatably movable between a first vertical lift position and a second horizontal thrust position. The lift/thrust fans are disposed within curvilinear fan recesses formed within leading edge portions of the aircraft's wings. A downwardly exhausting, ducted lift fan is disposed within the aircraft's fuselage, aft of the aircraft's pitch axis. A power plant, disposed within the fuselage, is coupled with the lift/thrust fans and the lift fan by a transmission system. The lift/thrust fans and lift fan are positioned with respect to one another to be triangulated about the aircraft's center of gravity and the aircraft's center of lift.
Control profile
Dennis D Olcott from Castle Pines, CO, age ~56 Get Report