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Sergey D Barmichev

from Kirkland, WA
Age ~72
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Also known as:
Serge D Barmichev, Serge Barmich
Phone and address:
14416 87Th Ave NE, Kirkland, WA 98034
(425) 381-7190
Related to:
Paul SestonMeagan L Kuniega, 28Yelena N Barmichev, 68Elena Barmichev, 68Natalie Seaton, 47
Connected to:
Victoria A Barmichael, 61Jeffrey A Barminko, 39Louise R Barmish, 69Scott E Barmmer, 57Jeanine M Barmonde, 55Andrew Barmore, 90Chad W Barmore, 55Douglas S Barmore, 51Duane L Barmore, 80Franklin D Barmore, 37

Sergey Barmichev Phones & Addresses

  • 14416 87Th Ave NE, Kirkland, WA 98034 (425) 381-7190
  • Bothell, WA
  • Bellevue, WA
  • Kiona, WA
  • 12025 100Th Ave NE APT 7B, Kirkland, WA 98034

Resumes

Resumes

Sergey Barmichev Photo 1

Engineer-Scientist

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Location:
Seattle, WA
Industry:
Aviation & Aerospace
Work:
Boeing
engineer-scientist
Education:
Leningrad State University named after A.S. Pushkin 1975 - 1989
Skills:
Microsoft Office
Project Management
Management
Program Management
Engineering
Leadership
Microsoft Excel
Aerospace
Manufacturing
Sergey Barmichev Photo 2

Engineer

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Location:
Kirkland, WA
Work:
Boieng
Engineer

Publications

Us Patents

Composite Seat Back Structure For A Lightweight Aircraft Seat Assembly

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US Patent:
8016361, Sep 13, 2011
Filed:
Apr 1, 2010
Appl. No.:
12/752381
Inventors:
Max U. Kismarton - Renton WA, US
Sergey Barmichev - Bothell WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B60N 2/68
US Classification:
2974522, 29745218, 29745219
Abstract:
An aircraft passenger seat configured in accordance with an embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat includes one or more lightweight composite support legs, a lightweight composite seat pan, and a lightweight composite seat back structure. The support legs are coupled to the seat pan, which is in turn coupled to the seat back structure. The support legs utilize composite frame elements that are formed as continuous compression molded composite extrusions. The seat pan includes composite fore and aft cross beams that are also formed as continuous compression molded composite extrusions. The aft cross beam includes a rear flange that serves as a flexible “hinge” for the seat back structure. The seat can leverage producible and relatively inexpensive composite manufacturing techniques such that the seat can be economically produced for use as an economy class seat.

Synthetic Aisle Configuration For An Aircraft

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US Patent:
8220741, Jul 17, 2012
Filed:
Jun 27, 2008
Appl. No.:
12/147731
Inventors:
Sergey D. Barmichev - Bothell WA, US
David W. Eckert - Marysville WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64D 11/06
US Classification:
2441186, 105319
Abstract:
A method may be present for configuring an aircraft. A design may be identified for the aircraft. A passenger area may be configured using a set of synthetic aisles to meet a desired passenger density for the design.

Fuselage Mounted Landing Gear

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US Patent:
8523107, Sep 3, 2013
Filed:
Mar 12, 2010
Appl. No.:
12/722848
Inventors:
James Jason Salmon - Kirkland WA, US
Sergey D. Barmichev - Bothell WA, US
Michael Allan Long - Freeland WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 25/10
US Classification:
244102A, 244102 R
Abstract:
A landing gear for an aircraft. The landing gear may have a wheel/truck assembly, an oleo strut/support frame for supporting the wheel/truck assembly, and a retraction assembly attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a deployed position and a retracted position. The retraction assembly may have a pivoting trunnion brace attached to the oleo strut/support frame and to a fuselage of the aircraft for positioning the wheel/truck assembly, the oleo strut/support frame and the retraction assembly at least substantially fully within the fuselage of the aircraft in the retracted position.

Low Profile Cargo Handling System

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US Patent:
8561946, Oct 22, 2013
Filed:
Oct 15, 2010
Appl. No.:
12/905581
Inventors:
Sergey D. Barmichev - Bothell WA, US
Harry Wilbert Slusher - Fountain Valley CA, US
Gary Peter Seagrave - Everett WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 1/20
US Classification:
2441181, 2441371, 414679
Abstract:
Different advantageous embodiments provide a method and apparatus to increase a clearance of a cargo area of an aircraft. The apparatus and method may comprise an aircraft with a cargo area. A tray system may have a plurality of segment trays with each segment tray positioned between a plurality of floor beams located underneath a surface of the floor of the cargo area. A plurality of rollers in the tray system may be configured to allow an object to be moved across the cargo area.

Advanced Performance Refueling Boom

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US Patent:
8596580, Dec 3, 2013
Filed:
Sep 27, 2010
Appl. No.:
12/891394
Inventors:
Sergey D. Barmichev - Bothell WA, US
Harry Wilbert Slusher - Fountain Valley CA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64D 39/00
US Classification:
244135A, 244 1 TD, 244135 R
Abstract:
Apparatuses, systems, and methods described herein provide for a refueling boom having vertical control surfaces extending primarily downward below the horizontal control surfaces out of the auxiliary power unit (APU) exhaust and airframe-induced turbulent flow fields, while reducing the torque moments applied to the boom beam and increasing control authority. According to one aspect of the disclosure provided herein, a refueling boom includes a boom beam, at least one horizontal control surface, and a pair of vertical control surfaces. The vertical control surfaces are positioned on opposing ends of the horizontal control surfaces and each include an upper portion and a longer lower portion projecting downward below the horizontal control surface. Aspects further improve the aerodynamic characteristics of the boom beam, reducing the drag associated with the refueling boom.

Composite Seat Back Structure For A Lightweight Aircraft Seat Assembly

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US Patent:
20080150342, Jun 26, 2008
Filed:
Dec 22, 2006
Appl. No.:
11/614980
Inventors:
Max U. Kismarton - Renton WA, US
Sergey Barmichev - Bothell WA, US
International Classification:
A47C 7/02
US Classification:
29745218
Abstract:
An aircraft passenger seat configured in accordance with an embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat includes one or more lightweight composite support legs, a lightweight composite seat pan, and a lightweight composite seat back structure. The support legs are coupled to the seat pan, which is in turn coupled to the seat back structure. The support legs utilize composite frame elements that are formed as continuous compression molded composite extrusions. The seat pan includes composite fore and aft cross beams that are also formed as continuous compression molded composite extrusions. The aft cross beam includes a rear flange that serves as a flexible “hinge” for the seat back structure. The seat can leverage producible and relatively inexpensive composite manufacturing techniques such that the seat can be economically produced for use as an economy class seat.

Flexible Shape Low Volume Autoclave

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US Patent:
20080308224, Dec 18, 2008
Filed:
Jun 12, 2007
Appl. No.:
11/761744
Inventors:
Sergey D. Barmichev - Bothell WA, US
Max U. Kismarton - Renton WA, US
Stephen T. Brown - Everett WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B29C 65/02
US Classification:
156285, 156382
Abstract:
Techniques and apparatus for providing a flexible shape low volume autoclave are disclosed. In one embodiment, an autoclave includes an elongated pressure vessel that is sealed on both ends and has a circumferential joint between a first portion and a second portion. The autoclave further includes the portions defining an interior configured for accepting an elongated part, the joint being configured to create an angle between the portions and further creating an opening with a seal, the opening facilitating an insertion of the part into the interior, and the seal enabling pressurization of the interior.

Low Volume Autoclave Having Configurable Shape

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US Patent:
20120073745, Mar 29, 2012
Filed:
Feb 26, 2011
Appl. No.:
13/035932
Inventors:
SERGEY BARMICHEV - Bothell WA, US
KEVIN MATTHEW RETZ - Bothell WA, US
International Classification:
B29C 70/44
B29C 35/02
US Classification:
156285, 156382
Abstract:
An autoclave may be reconfigured to accommodate differently shaped parts by relatively rotating portions of the autoclave.
Control profile
Sergey D Barmichev from Kirkland, WA, age ~72 Get Report