Adrian R Allan

age ~56

from Walpole, MA

Also known as:
  • Robert A Allan
  • Allan R Allan
  • Robert R Allan
  • Andrew R Allan
  • Bob R Allan
  • Adrian R Allen
  • Rob Allan
  • Wendy Allan
  • Allan Adrian
  • Allan Robert

Adrian Allan Phones & Addresses

  • Walpole, MA
  • 1645 Windsong Dr, Phoenix, AZ 85045 • 6025493085
  • 2939 Amber Ridge Way, Phoenix, AZ 85048 • 4807048468 • 4807048024
  • Cincinnati, OH
  • Chandler, AZ
  • 2939 E Amber Ridge Way, Phoenix, AZ 85048

Us Patents

  • Vane Radial Mounting Apparatus

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  • US Patent:
    6843638, Jan 18, 2005
  • Filed:
    Dec 10, 2002
  • Appl. No.:
    10/316542
  • Inventors:
    Mario A. Hidalgo - Phoenix AZ, US
    Adrian R. Allan - Chandler AZ, US
    Louis D. Cruse - Scottsdale AZ, US
  • Assignee:
    Honeywell International Inc. - Morristown NJ
  • International Classification:
    F01D 102
  • US Classification:
    4152093, 415189
  • Abstract:
    A variable geometry vane for use in a turbine engine. The vane can be radially mounted in a shroud ring while outside the turbine engine. The shroud and vane assembly can then be mounted to an engine hub without disassembly of the shroud, eliminating the need for a split ring shroud. Once located surrounding the hub, vanes are slid radially inward until a radially inward vane button engages a hole within the hub. Vanes are locked in place using clips slid into slots within the shroud. The clips are retained in place using an adjacent engine part bolted to the face of the shroud. Once in place within the engine, vanes are attached to a control arm for airflow adjustment.
  • Variable Turbine Cooling Flow System

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  • US Patent:
    6931859, Aug 23, 2005
  • Filed:
    Dec 17, 2003
  • Appl. No.:
    10/739754
  • Inventors:
    Peter L. Morgan - Tempe AZ, US
    William J. Howe - Chandler AZ, US
    Mark C. Morris - Phoenix AZ, US
    Adrian R. Allan - Chandler AZ, US
    Donald L. Palmer - Cave Creek AZ, US
  • Assignee:
    Honeywell International Inc. - Morristown NJ
  • International Classification:
    F02C007/12
  • US Classification:
    60782, 60785, 137494
  • Abstract:
    Cooling air to the blades and disks of a gas turbine may be modulated to provide a variable turbine cooling flow. A bellows may be extended by providing a high pressure compressor discharge flow to an interior of the bellows. The bellows may be compressed when the interior of the bellows communicates with ambient pressure air. The extension/compression of the bellows moves an arm over orifices in a cooling air flow path. The pressure inside of the bellows is metered to move the arm over at least one orifice, thereby restricting cooling air flow when the engine is running at low power. The pressure inside of the bellows is metered to move the arm to uncover all of the slots to provide maximum cooling flow when the engine is running at high power. The resulting variable cooling flow system results in less need for cooling air at low powers, thus reducing engine fuel consumption.
  • Compliant Mounting System For Turbine Shrouds

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  • US Patent:
    7195452, Mar 27, 2007
  • Filed:
    Sep 27, 2004
  • Appl. No.:
    10/950750
  • Inventors:
    Adrian R. Allan - Phoenix AZ, US
    James L. Hadder - Scottsdale AZ, US
    George E. Zurmehly - Phoenix AZ, US
  • Assignee:
    Honeywell International, Inc. - Morristown NJ
  • International Classification:
    F01D 11/08
    F01D 25/26
  • US Classification:
    415135, 415318, 4151733, 4152131, 4152141, 29446, 29452, 298892, 2988922, 248675
  • Abstract:
    The mounting of low expansion full ring shrouds in a turbine engine requires radial compliance to limit the stresses experienced by the shroud due to thermal growth differences between the shroud and its support. A method provides radial compliance with no looseness in a mounting system. The mounting system also allows for axial motion of the shroud, should such motion be needed or desired. The lack of looseness in the mounting system results in an ability to achieve smaller tip clearances and thus better engine performance.
  • Cooled Component With A Featured Surface And Related Manufacturing Method

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  • US Patent:
    8109735, Feb 7, 2012
  • Filed:
    Nov 13, 2008
  • Appl. No.:
    12/270372
  • Inventors:
    Raymond Gage - Phoenix AZ, US
    Adrian Allan - Phoenix AZ, US
  • Assignee:
    Honeywell International Inc. - Morristown NJ
  • International Classification:
    F04D 29/38
  • US Classification:
    416241R
  • Abstract:
    An improved type of cooled component is disclosed. The cooled components, such as turbine airfoils and combustors, have a base metal structural member, including a metal sheet or blank, with a featured surface. The features, such as fins, pins, and other protrusions, as well as divots, indentions, slots, channels, and holes, are formed by lithographic processes. The protrusions can be formed from a different material than the metal sheet or blank, preferably one with superior heat-conductive or oxidation properties. A related method of manufacturing is also disclosed.
  • Laminated Finger Seal With Stress Reduction

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  • US Patent:
    20030025274, Feb 6, 2003
  • Filed:
    Aug 2, 2001
  • Appl. No.:
    09/922126
  • Inventors:
    Adrian Allan - Chandler AZ, US
    Arun Kumar - Chandler AZ, US
    Gulshan Arora - Mesa AZ, US
  • Assignee:
    Honeywell International, Inc. - Morristown NJ
  • International Classification:
    F01D011/02
  • US Classification:
    277/355000
  • Abstract:
    A finger seal for use between a housing and a combustor liner to inhibit air passage therebetween. The finger seal has at least two annular diaphragm members partitioned into a generally continuous inner diameter portion and a segmented outer diameter portion. The segments are finger elements spaced uniformly apart forming gaps therebetween and extend radially outward terminating in a foot portion. A keyhole is formed at the terminus end of the gaps to reduce fatigue and stress of the finger elements. The diaphragm members are laminated together, oriented such that adjacent fingers of one laminate block the gaps of the other, and inserted between a pair of spacers and endplates to be attached at their inner diameter portion. The finger seal is attached circumferentially around the housing and assembled into the combustor liner with the foot portion sealing against the combustor liner interior wall.
  • Laminated Finger Seal With Ceramic Composition

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  • US Patent:
    20030111797, Jun 19, 2003
  • Filed:
    Dec 19, 2001
  • Appl. No.:
    10/027573
  • Inventors:
    Vincent Chung - Tempe AZ, US
    Arun Kumar - Chandler AZ, US
    Bjoern Schenk - Phoenix AZ, US
    Adrian Allan - Chandler AZ, US
  • Assignee:
    Honeywell International, Inc. - Morristown NJ
  • International Classification:
    F16J015/44
  • US Classification:
    277/355000
  • Abstract:
    A ceramic finger seal for use between a housing and a combustor liner to inhibit air passage therebetween and for use in fluid sealing between a rotating shaft and a housing circumscribing the rotating shaft. The ceramic finger seal has at least two annular diaphragm members constructed of two or more diaphragm segments bonded end to end by ceramic cement or other high temperature joining compounds. The diaphragm members may be partitioned into a generally continuous inner diameter portion and a segmented outer diameter portion or the reverse thereof. The segmented portion includes finger elements spaced uniformly apart forming gaps therebetween and extend radially outward or inward terminating in a foot portion. A keyhole is formed at the terminus end of the gaps to minimize crack initiation of the finger elements. The diaphragm members are laminated together, oriented such that adjacent fingers of one laminate block the gaps of the other, and inserted between a pair of spacers and endplates to be attached at their continuous diameter portion. The ceramic finger seal may be attached circumferentially around the housing and assembled into the combustor liner with the foot portion sealing against the combustor liner interior wall. The rolled edge on the finger is formed by laser cutting to prevent gouging of the combustor liner surface.
  • Bonded Assemblies And Methods For Improving Bond Strength Of A Joint

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  • US Patent:
    20110059290, Mar 10, 2011
  • Filed:
    Sep 8, 2009
  • Appl. No.:
    12/555633
  • Inventors:
    Raymond Gage - Phoenix AZ, US
    Adrian Allan - Phoenix AZ, US
  • Assignee:
    HONEYWELL INTERNATIONAL INC. - Morristown NJ
  • International Classification:
    B32B 3/06
    B32B 37/14
  • US Classification:
    428 99, 156 91
  • Abstract:
    Bonded assemblies and methods for improving the bond strength of a joint are provided. The joint may be formed between bonding surfaces of a first and a second component. The first component has a bonding surface adapted to be bonded to a bonding surface of a second component. A plurality of features may be formed in at least one of the bonding surfaces. The bonding surfaces are bonded together to form the joint. A bonding material layer between the bonding surfaces may form the joint or the first and second components may be co-cured to form the joint. A chemical and mechanical bond between the bonding surfaces is formed with the plurality of features forming the mechanical bond and increasing the bond area of the chemical bond. The features may be openings and/or protrusions such as holes, slots, and bosses.

Isbn (Books And Publications)

Redbrick University Revisited: The Autobiography Of `bruce Truscot'

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Author
Adrian R. Allan

ISBN #
0853232598

Redbrick University Revisited: The Autobiography Of `bruce Truscot'

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Author
Adrian R. Allan

ISBN #
0853233977

Googleplus

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Facebook

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Adrian Allan Bilgera

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Adrian Allan Uy Pantale

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Adrian Allan Caraos

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Adrian Allan Alejandria A...

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Adrian Allan Guevarra

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Adrian Allan Y. Berdin

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Myspace

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Adrian Allan

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Locality:
Sydney, New South Wales
Gender:
Male
Birthday:
1955
Adrian Allan Photo 18

Adrian Allan

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Locality:
Mandurah, Western Australia
Gender:
Male
Birthday:
1952
Adrian Allan Photo 19

adrian allan

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Locality:
Philippines
Gender:
Male
Birthday:
1946
Adrian Allan Photo 20

adrian allan

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Locality:
Philippines
Gender:
Male
Birthday:
1937
Adrian Allan Photo 21

Adrian Allan

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Locality:
Philippines
Gender:
Male
Birthday:
1938

Youtube

Alex Belfield - Bernie Keiths statement.

Thank you for your patience. All is explained in the video. I hope you...

  • Duration:
    12m 19s

Just when you think you heard it all. The mon...

Adrian allen Mumpsimus Sponsor me and my channel but only if you...

  • Duration:
    8m 32s

Alex Belfield - Perception Vs Reality.

  • Duration:
    12m 10s

Alex Belfield - The Truth.

Alex Belfield's first stalking victim, tells the truth about his exper...

  • Duration:
    3m 49s

Alex Belfield - More home truths.

Ahead of tomorrow's video, I thought you'd like to know what further r...

  • Duration:
    1m 13s

Adrian Allan and John Heaton discuss Paul McC...

An in-depth discussion about the life and work of Paul McCartney in th...

  • Duration:
    1h 26m 42s

Other Social Networks

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Adrian Allan's Page Comp...

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Network:
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Adrian Allan's Page on Composers' Forum. ... Started this discussion. Last reply by Adrian Allan Mar 27. 6 Replies 0 Likes ...

Flickr


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