Lanchao D Lin

age ~66

from Dayton, OH

Also known as:
  • Lan Chao Lin
  • Lancho Lin
  • Lin D Lanchao
Phone and address:
1245 Spring Ash Dr, Dayton, OH 45458
9378862371

Lanchao Lin Phones & Addresses

  • 1245 Spring Ash Dr, Dayton, OH 45458 • 9378862371
  • 36 Seminary Ave, Dayton, OH 45403
  • Centerville, OH
  • Allen Park, MI
  • 1245 Spring Ash Dr, Centerville, OH 45458

Work

  • Company:
    Ge aviation
  • Position:
    Engineer

Education

  • Degree:
    Associate degree or higher

Resumes

Lanchao Lin Photo 1

Engineer

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Location:
Dayton, OH
Work:
Ge Aviation
Engineer

Us Patents

  • Finned Heat Exchanger

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  • US Patent:
    6397931, Jun 4, 2002
  • Filed:
    Feb 27, 2001
  • Appl. No.:
    09/793785
  • Inventors:
    Lanchao Lin - Beavercreek OH
    John E. Leland - Kettering OH
    Richard J. Harris - Dayton OH
  • Assignee:
    The United States of America as represented by the Secretary of the Air Force - Washington DC
  • International Classification:
    H05K 720
  • US Classification:
    165 803, 165 804, 165185, 165 81
  • Abstract:
    A finned heat exchanger is disclosed. The heat exchanger includes a unitary fin array with a multiplicity of fin banks. Each of the fin banks include a plurality of raised, folded fins for heat transfer. The fin banks extend in a transverse direction and are spaced apart in a longitudinal direction. The fin banks are retained within the fin array by looped expansion turns. The fin array is mounted on a dielectric substrate base. A closed flow channel for directing a flow of coolant is created by adding a cap to the substrate base.
  • Passive Thermal Spreader And Method

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  • US Patent:
    6679316, Jan 20, 2004
  • Filed:
    Oct 2, 2000
  • Appl. No.:
    09/677720
  • Inventors:
    Lanchao Lin - Beavercreek OH
    John E. Leland - Kettering OH
  • Assignee:
    The United States of America as represented by the Secretary of the Air Force - Washington DC
  • International Classification:
    F28D 1500
  • US Classification:
    16510426, 165170, 16510433
  • Abstract:
    A passive thermal spreader and method of fabrication are disclosed. The passive thermal spreader includes a heat transfer plate formed from laminated plates including an internal sealed thermosyphon defined within the interface of the plates. The preferred embodiment of the passive thermal spreader selected to illustrate the invention includes a pair of distinct thermosyphons defined within the interface of three laminated, stacked plates. Each thermosyphon includes a plurality of channels arranged boustrophedonically. Each of the channels includes an elongate straight portion and an end turn portion for connection to the adjacent channel elongate straight portion. Each elongate straight portion includes a channel divider. The channel divider directly contributes to the high performance of the thermal spreader of the present invention by assisting the transport of the working fluid.
  • Cooling Of Electromechanical Actuator With Phase Change Material And Thermosyphons Containing Working Fluid

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  • US Patent:
    62948539, Sep 25, 2001
  • Filed:
    Nov 2, 2000
  • Appl. No.:
    9/704947
  • Inventors:
    Lanchao Lin - Beavercreek OH
    John E. Leland - Kettering OH
    Rengasamy Ponnappan - Dayton OH
  • Assignee:
    The United States of America as represented by the Secretary of the Air
    Force - Washington DC
  • International Classification:
    H02K 900
    H02K 919
  • US Classification:
    310 57
  • Abstract:
    A passively cooled electromechanical actuator is disclosed. The passively cooled electromechanical actuator includes a rotor having an output shaft rotatably received within a stator. A pair of inner supports connect the stator to a pair of mounting platforms. The mounting platforms are attached to the inner surfaces of an aircraft wing and are in thermal communication therewith. A pair of closed, capillary tube thermosyphons containing a working fluid are in thermal communication with the stator, the inner supports and the mounting platforms. During operation, the thermosyphons receive heat from the stator and transport it to the mounting platforms whereupon it is convected or radiated to the atmosphere from the aircraft wings. The inner supports have a phase change material received within for providing temporary thermal energy storage during transient conditions.
  • Ram Air Turbine System

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  • US Patent:
    20170057655, Mar 2, 2017
  • Filed:
    Sep 2, 2015
  • Appl. No.:
    14/843718
  • Inventors:
    - Grand Rapids MI, US
    Xiaochuan JIA - Centerville OH, US
    Lanchao LIN - Dayton OH, US
  • International Classification:
    B64D 41/00
    F01D 15/10
    F01D 25/12
    F01D 5/18
  • Abstract:
    A ram air turbine system includes a rotatable shaft, a housing having a body defining an interior, a generator located within the interior and having a stator and a rotor, and a turbine having a first set of blades operably coupled with the rotatable shaft and configured such that airstream passing through the first set of blades rotates the shaft.

Youtube

[alaplaya] - Land of Chaos - online (LOCO)- T...

In the context of alaplayas 2nd anniversary, they have published the f...

  • Category:
    Gaming
  • Uploaded:
    14 Jul, 2009
  • Duration:
    2m 3s

Ma ln Xun inh Hi

tit mc ma ln m mn cho mng Xun inh Hc do cc anh em trong Tripode B thc ...

  • Category:
    People & Blogs
  • Uploaded:
    26 Feb, 2007
  • Duration:
    4m 39s

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