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Song C Chiou

from Irvine, CA
Age ~66

Song Chiou Phones & Addresses

  • 15292 Moulins Cir, Irvine, CA 92604 (562) 286-3057
  • 12235 Waterbrook Dr, Rch Cucamonga, CA 91739
  • Rancho Cucamonga, CA
  • 12226 Meadow Dr, Artesia, CA 90701 (562) 924-2248
  • 17013 Betty Ave, Cerritos, CA 90703 (562) 404-0469 (562) 924-2248
  • Corona, CA
  • Anaheim, CA
  • 17013 Betty Ave, Cerritos, CA 90703

Work

Position: Professional/Technical

Education

Degree: Associate degree or higher

Business Records

Name / Title
Company / Classification
Phones & Addresses
Song Chiou
Director of Engineering
Goodrich Corporation
Mfg Aircraft Components and Parts · Aircraft Engine and Engine Parts Manufacturing
8200 Arlington Ave, Riverside, CA 92503
(951) 351-5400, (951) 351-5000, (909) 351-5400

Publications

Us Patents

Linear Acoustic Liner

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US Patent:
7921966, Apr 12, 2011
Filed:
Aug 13, 2008
Appl. No.:
12/190805
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
E04B 1/84
B64D 33/02
E04B 1/82
B64D 33/00
US Classification:
181292, 181288, 181214, 244538
Abstract:
A linear acoustic liner for an aircraft includes a cellular core having a first surface and an opposed second surface. A substantially imperforate back skin covers the first surface, and a perforate face skin covers the second surface of the core. The perforate face skin includes an outer face skin layer having a first plurality of spaced openings, an inner face skin layer having a second plurality of spaced openings, and a porous layer disposed between the outer face skin layer and the inner face skin layer. Each of the first plurality of spaced openings are substantially aligned with one of the second plurality of spaced openings.

Linear Acoustic Liner

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US Patent:
8196704, Jun 12, 2012
Filed:
Mar 14, 2011
Appl. No.:
13/047408
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
E04B 1/84
B64D 33/02
E04B 1/82
B64D 33/00
US Classification:
181292, 181288, 181214, 181296, 244 53 B
Abstract:
A linear acoustic liner for an aircraft includes a cellular core having a first surface and an opposed second surface. A substantially imperforate back skin covers the first surface, and a perforate face skin covers the second surface of the core. The perforate face skin includes an outer face skin layer having a first plurality of spaced openings, an inner face skin layer having a second plurality of spaced openings, and a porous layer disposed between the outer face skin layer and the inner face skin layer. Each of the first plurality of spaced openings are substantially aligned with one of the second plurality of spaced openings.

Low Density Lightning Strike Protection For Use In Airplanes

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US Patent:
20090227162, Sep 10, 2009
Filed:
Mar 9, 2007
Appl. No.:
12/282305
Inventors:
Teresa M. Kruckenberg - La Mesa CA, US
Valerie A. Hill - Villa Rica GA, US
Anthony Michael Mazany - Amelia Island FL, US
Eloise Young - Moreland Hills OH, US
Song Chiou - Cerritos CA, US
Assignee:
Goodrich Corporation - Charlotte NC
Rohr, Inc. - Chula Vista CA
International Classification:
B32B 5/16
D03D 9/00
B32B 27/04
H01B 1/24
B32B 27/12
B82B 1/00
B82B 3/00
US Classification:
442 1, 428338, 442117, 252511, 977751, 977752, 977762, 977775, 977773, 977902
Abstract:
Surface films, paints, or primers can be used in preparing aircraft structural composites that may be exposed to lightning strikes. Methods for making and using these films, paints or primers are also disclosed. The surface film can include a thermoset resin or polymer, e.g., an epoxy resin and/or a thermoplastic polymer, which can be cured, bonded, or painted on the composite structure. Low-density electrically conductive materials are disclosed, such as carbon nanofiber, copper powder, metal coated microspheres, metal-coated carbon nanotubes, single wall carbon nanotubes, graphite nanoplatelets and the like, that can be uniformly dispersed throughout or on the film. Low density conductive materials can include metal screens, optionally in combination with carbon nanofibers.

Acoustic Barrel For Aircraft Engine Nacelle Including Crack And Delamination Stoppers

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US Patent:
20100122868, May 20, 2010
Filed:
Nov 14, 2008
Appl. No.:
12/271189
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
International Classification:
F02K 1/82
B29C 65/48
US Classification:
181213, 156182
Abstract:
An acoustic inner barrel for an aircraft engine nacelle inlet is constructed from a composite material and is formed as a single, 360-degree annular segment. The barrel includes an inner skin, an outer skin, a cellular core disposed between the inner skin and the outer skin, and at least one crack and delamination stopper extending radially from the inner skin to the outer skin.

Crack And Delamination Stoppers For Aircraft Propulsion System Components

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US Patent:
20120291416, Nov 22, 2012
Filed:
May 11, 2012
Appl. No.:
13/470049
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
B64D 33/04
F02K 3/04
US Classification:
602262, 23926511
Abstract:
An inner fixed structure of a thrust reverser includes an inner skin, an outer skin, a cellular core disposed between the inner skin and the outer skin, and at least one crack and delamination stopper extending radially between the inner skin and the outer skin.

Thrust Reverser-Integrated Track Beam And Inner Fixed Structure

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US Patent:
20140030087, Jan 30, 2014
Filed:
Jul 24, 2013
Appl. No.:
13/949976
Inventors:
Song Chiou - Cerritos CA, US
Michael J. Layland - Bonita CA, US
Claude Hubert - Riverside CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
F02C 7/20
US Classification:
4152131
Abstract:
A panel for a nacelle structure that surrounds a jet engine core includes a longitudinally extending, generally semicircular center region, an upper bifurcation region, a lower bifurcation region, a hinge beam region extending from the upper bifurcation region and configured to receive an upper thrust reverser track guide, and a latch beam region extending from the lower bifurcation region and configured to receive a lower thrust reverser track guide. A bypass duct is formed in a space between the panel and the nacelle structure. A hinge beam structure and latch beam structure are integrally formed with the panel. An inner skin layer extends continuously across a bond panel surface generally facing the engine core and an outer skin layer extends continuously across a bond panel surface generally facing the bypass duct, the inner and outer skin layers extending across the center region, upper and lower bifurcation regions, hinge beam region, and latch beam region. The outer skin layer may have an acoustic treatment, such as being perforated in at least the center region and the upper and lower bifurcation regions. In this way, a separate hinge beam and latch beam are not used, and therefore there is no need to couple the panel to the respective beams.

Acoustic Liner And Method Of Forming An Acoustic Liner

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US Patent:
20220349363, Nov 3, 2022
Filed:
Jul 18, 2022
Appl. No.:
17/867140
Inventors:
- Chula Vista CA, US
Peter J. Walsh - Wethersfield CT, US
Danielle L. Grolman - Holden MA, US
Craig Aaron Reimann - Vernon CT, US
Thomas P. Filburn - Granby CT, US
Song Chiou - Irvine CA, US
Jeong-Woo Kim - Glastonbury CT, US
Jeffrey M. Mendoza - Manchester CT, US
International Classification:
F02K 1/82
F23M 20/00
F02C 7/045
G10K 11/168
Abstract:
An acoustic liner includes a first face sheet, a second face sheet spaced from the first face sheet, and a plurality of sidewalls extending between the first face sheet and the second face sheet. The plurality of sidewalls defines a plurality of cells. Each cell of the plurality of cells defines a cavity between the first face sheet and the second face sheet. A bulk absorber is disposed within at least one cell of the plurality of cells. The bulk absorber further defines the cavity of the at least one cell of the plurality of cells. The first face sheet defines a plurality of apertures extending through a thickness of the first face sheet. Each aperture of the plurality of apertures is aligned with a respective cell of the plurality of cells.

Acoustic Liner And Method Of Forming An Acoustic Liner

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US Patent:
20200217272, Jul 9, 2020
Filed:
Jan 4, 2019
Appl. No.:
16/240360
Inventors:
- Chula Vista CA, US
Peter J. Walsh - Wethersfield CT, US
Danielle L. Grolman - Holden MA, US
Craig Aaron Reimann - Vernon CT, US
Thomas P. Filburn - Granby CT, US
Song Chiou - Irvine CA, US
Jeong-Woo Kim - Glastonbury CT, US
Jeffrey M. Mendoza - Manchester CT, US
International Classification:
F02K 1/82
G10K 11/168
F02C 7/045
F23M 20/00
Abstract:
An acoustic liner includes a first face sheet, a second face sheet spaced from the first face sheet, and a plurality of sidewalls extending between the first face sheet and the second face sheet. The plurality of sidewalls defines a plurality of cells. Each cell of the plurality of cells defines a cavity between the first face sheet and the second face sheet. A bulk absorber is disposed within at least one cell of the plurality of cells. The bulk absorber further defines the cavity of the at least one cell of the plurality of cells. The first face sheet defines a plurality of apertures extending through a thickness of the first face sheet. Each aperture of the plurality of apertures is aligned with a respective cell of the plurality of cells.
Song C Chiou from Irvine, CA, age ~66 Get Report