John Dovey resumes & CV records
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John Dovey
John Dovey
John V Dovey, Age 5810539 Palatine Ave, Seattle, WA 98133
John Dovey Phones & Addresses
10539 Palatine Ave, Seattle, WA 98133 (206) 364-3374 (206) 547-8993
11539 Palatine Ave, Seattle, WA 98133 (206) 364-3374
11551 Greenwood Ave, Seattle, WA 98133 (206) 364-3374
Renton, WA
Bellevue, WA
Choctaw, OK
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John Dovey
John Dovey was the co-owner of the Boston Doves of the National League with his bother George Dovey from 1907 through 1909, and later sole principal owner ...
Us Patents
Aircraft Trailing Edge Devices, Including Devices Having Forwardly Positioned Hinge Lines, And Associated Methods
US Patent:
7708231, May 4, 2010
Filed:
Nov 21, 2005
Appl. No.:
11/284113
Inventors:
Douglas S. Lacy - Bothell WA, US
Jan A. Kordel - Redmond WA, US
John V. Dovey - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
Seiya Sakurai - Seattle WA, US
Neal V. Huynh - Bellevue WA, US
Jan A. Kordel - Redmond WA, US
John V. Dovey - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
Seiya Sakurai - Seattle WA, US
Neal V. Huynh - Bellevue WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 9/18
US Classification:
244211
Abstract:
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
Trailing Edge Device Catchers And Associated Systems And Methods
US Patent:
7766282, Aug 3, 2010
Filed:
Dec 11, 2007
Appl. No.:
12/001414
Inventors:
Jan A. Kordel - Sandringham, AU
Seiya Sakurai - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
John V. Dovey - Seattle WA, US
Seiya Sakurai - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
John V. Dovey - Seattle WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 3/50
US Classification:
244215, 244201, 244213, 244217, 244212
Abstract:
Trailing edge device catchers and associated systems and methods are disclosed. A system in accordance with one embodiment includes a wing having a wing support, a trailing edge device carried by and movable relative to the wing and having a device support, and a coupling connected between the wing and the trailing edge device. The coupling can include a pivot joint that includes a pivot element aligned along a pivot axis and connected between the wing support and the device support. The coupling can further include an actuator coupled between the wing and the trailing edge device, with the actuator having a first position in which the trailing edge device is stowed, and a second position in which the trailing edge device is deployed, with an air flow gap located between the wing and the trailing edge device when the trailing edge device is in the second position. A cam track is carried by one of the wing and the trailing edge device and has opposing cam track surfaces fixed relative to each other. A cam is carried by the other of the wing and trailing edge device and is positioned within the cam track between the opposing cam track surfaces.
Aircraft Trailing Edge Devices, Including Devices Having Forwardly Positioned Hinge Lines, And Associated Methods
US Patent:
8038103, Oct 18, 2011
Filed:
Jul 2, 2009
Appl. No.:
12/497493
Inventors:
Douglas S. Lacy - Bothell WA, US
Jan A. Kordel - Sandringham, AU
John V. Dovey - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
Seiya Sakurai - Seattle WA, US
Neal V. Huynh - Bellevue WA, US
Jan A. Kordel - Sandringham, AU
John V. Dovey - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
Seiya Sakurai - Seattle WA, US
Neal V. Huynh - Bellevue WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 9/18
US Classification:
244211
Abstract:
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
Aircraft Trailing Edge Devices, Including Devices Having Forwardly Positioned Hinge Lines, And Associated Methods
US Patent:
8567726, Oct 29, 2013
Filed:
Oct 3, 2011
Appl. No.:
13/252011
Inventors:
Douglas S. Lacy - Bothell WA, US
Jan A. Kordel - Sandringham, AU
John V. Dovey - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
Seiya Sakurai - Seattle WA, US
Neal V. Huynh - Bellevue WA, US
Jan A. Kordel - Sandringham, AU
John V. Dovey - Seattle WA, US
Michael A. Balzer - Kirkland WA, US
Seiya Sakurai - Seattle WA, US
Neal V. Huynh - Bellevue WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 9/18
US Classification:
244211
Abstract:
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
Jam Resistant And Intruder-Proof Flight Deck Door
US Patent:
2003018, Oct 9, 2003
Filed:
Sep 24, 2002
Appl. No.:
10/253571
Inventors:
John Dovey - Seattle WA, US
Scott Kube - Everett WA, US
John Pechacek - Colleyville TX, US
Rolando Taguinod - Renton WA, US
Scott Kube - Everett WA, US
John Pechacek - Colleyville TX, US
Rolando Taguinod - Renton WA, US
International Classification:
B64D011/00
B64D013/00
B64D013/00
US Classification:
244/118500
Abstract:
A multi-section aircraft door includes a sliding joint permitting a lower door section displacement into the flight deck area. The door includes an upper door section having a lower edge. The lower edge is connectably joined to an upper member of a two-member sliding joint. The upper member slidably joins to a sliding joint lower member. The sliding joint lower member is connectably joined to a lower door section upper edge. The upper member and the lower member of the two-member sliding joint include paired apertured embossments. A frangible pin slidably mates in each apertured embossment pair. A lever and cam form a frangible pin removal assembly. The lever is held in a normally upright position by either a spring device or a clevis and pin assembly. A rotating clasp or a ball detente system can also replace the frangible pin/apertured embossment and cam/lever.
Ballistic Resistant Flight Deck Door And Method Of Making Same
US Patent:
2003018, Oct 9, 2003
Filed:
Jan 3, 2003
Appl. No.:
10/336592
Inventors:
Michael Cloud - Snohomish WA, US
John Dovey - Seattle WA, US
James Kunda - Snohomish WA, US
John Dovey - Seattle WA, US
James Kunda - Snohomish WA, US
International Classification:
B64D011/00
B64D013/00
B64D013/00
US Classification:
244/118500
Abstract:
A flight deck door for an aircraft that is both ballistic resistant and intruder proof. The flight deck door includes a laminated ballistic resistant material which can also provide intruder resistant properties. The ballistic resistant or armor material can be laminated onto a core to provide additional rigidity to the flight deck door. The core also increases the rigidity of the flight deck door and increases intruder resistance. Also sound dampening layers may be added to the door.
Seal, Aircraft Including The Seal, And Methods Therefor
US Patent:
2020037, Dec 3, 2020
Filed:
May 30, 2019
Appl. No.:
16/426724
Inventors:
- Chicago IL, US
John V. DOVEY - Seattle WA, US
John V. DOVEY - Seattle WA, US
International Classification:
F16J 15/02
B64C 3/50
B33Y 80/00
B64C 3/50
B33Y 80/00
Abstract:
A seal for sealing a space between a first structure and second structure. The seal includes a seal base configured to couple with the first structure so as to form a respective seal with the first structure, a resilient lattice body coupled to the seal base, and a cover. The cover includes an inner surface coupled to the resilient lattice body in an opposing relationship relative to the seal base so that the cover moves towards and away from the seal base in a biasing direction of the resilient lattice body, and a bulbous outer surface configured to engage the second structure so as to form a respective seal with the second structure.
Slat End Seal And Method For Manufacturing The Same
US Patent:
2020011, Apr 16, 2020
Filed:
Oct 15, 2018
Appl. No.:
16/160002
Inventors:
- Chicago IL, US
John Dovey - Seattle WA, US
John Dovey - Seattle WA, US
International Classification:
B64C 9/24
B64C 7/00
B64C 7/00
Abstract:
The present disclosure provides a slat end seal for use with a slat of an aircraft. The slat end seal includes a shell having a first surface, a second surface opposite the first surface, and a sidewall extending from the first surface. The shell includes a plurality of through holes in the first surface of the shell. The slat end seal also includes a lattice structure coupled to the first surface of the shell and configured to compress in response to a force applied to the second surface of the shell. The lattice structure includes a plurality of supports defining a plurality of interstitial voids between the plurality of supports. The lattice structure also includes at least one through hole aligned with at least one through hole of the plurality of through holes in the first surface of the shell.
Public records
Vehicle Records
John Dovey
Address:
10539 Palatine Ave N, Seattle, WA 98133
Phone:
(206) 364-3374
VIN:
4T1BE46K77U028256
Make:
TOYOTA
Model:
CAMRY
Year:
2007
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