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Marion Oneil Duggans

from Daytona Beach, FL
Age ~71

Marion Duggans Phones & Addresses

  • 525 Wallace St, Daytona Beach, FL 32114 (386) 253-2629 (386) 947-9367
  • 527 Wallace St, Daytona Beach, FL 32114 (386) 253-2629
  • Port Orange, FL
  • 2111 Brandywine Rd, West Palm Bch, FL 33409 (561) 683-3729
  • 4200 Community Dr, West Palm Beach, FL 33409 (561) 683-3729
  • 4200 Community Dr APT 409, West Palm Beach, FL 33409 (561) 683-3729
  • 203 Wedgewood Plaza Dr, West Palm Beach, FL 33404 (561) 845-0815
  • 1016 Indian Trace Cir, West Palm Beach, FL 33407 (561) 845-0815
  • Riviera Beach, FL
  • Boynton Beach, FL

Resumes

Resumes

Marion Duggans Photo 1

Cad Design And Drafter

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Location:
West Palm Beach, FL
Work:
Alstom Power
Cad Design and Drafter
Marion Duggans Photo 2

Designer And Drafter, Steam Turbine

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Location:
Daytona Beach, FL
Industry:
Oil & Energy
Work:

Designer and Drafter, Steam Turbine

Mitsubishi Power Systems Americas
Designer and Drafter, Steam Turbine Engineering
Marion Duggans Photo 3

Marion Duggans

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Location:
West Palm Beach, FL
Industry:
Mechanical Or Industrial Engineering
Marion Duggans Photo 4

Cad Design/Drafter At Alstom Power

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Position:
cad design/drafter at Alstom Power
Location:
West Palm Beach, Florida Area
Industry:
Oil & Energy
Work:
Alstom Power
cad design/drafter

Publications

Us Patents

Hot Gas Duct And Duct Splitter Arrangement

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US Patent:
20080222874, Sep 18, 2008
Filed:
Mar 13, 2007
Appl. No.:
11/685503
Inventors:
Orestes J. Maurell - West Palm Beach FL, US
Russell Bond Jones - Jupiter FL, US
Marion Duggans - West Palm Beach FL, US
Sejko Kolev - Birr, CH
Assignee:
ALSTOM TECHNOLOGY LTD. - Baden
International Classification:
B23P 25/00
US Classification:
29458, 2940208, 415178
Abstract:
A hot gas duct, such as a combustion casing in a gas turbine engine, includes a duct splitter held within the hot gas duct in at least three, preferably four, locations spaced around a peripheral edge of the duct splitter. At least one, preferably two, of the holding locations each comprise a generally cylindrical mounting that projects through a wall of the hot gas duct to engage an edge portion of the duct splitter by means of a slot formed in a circular face of the mounting. Mutually contacting surfaces of the slot and the duct splitter comprise hard face coatings to combat wear due to vibration and differential thermal expansion and contraction. The mountings have cooling holes that penetrate the mounting, so that coolant can flow through the mountings and into the interior of the hot gas duct to cool the mountings and the hard face coatings.

Thermal Machine

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US Patent:
20110113785, May 19, 2011
Filed:
Aug 9, 2010
Appl. No.:
12/852788
Inventors:
Remigi TSCHUOR - Windisch, CH
Russell Bond JONES - Jupiter FL, US
Marion Oneil DUGGANS - West Palm Beach FL, US
Assignee:
ALSTOM TECHNOLOGY LTD - Baden
International Classification:
F02C 1/00
B23P 17/00
US Classification:
60752, 29888
Abstract:
A thermal machine is provided, in particular a gas turbine, which includes an annular combustion chamber which is bounded on the outside by an outer shell and an inner shell. The outer shell and the inner shell are each split on a separating plane into an upper half and a lower half, which are mechanically interlocked by welding one to the other on the separating plane. Increased mechanical robustness and a longer life of the combustion chamber are achieved in that an additional mechanical interlock is provided on the separating planes in order to absorb tensile and shear forces acting on the separating planes.

Gas Turbine

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US Patent:
20110135451, Jun 9, 2011
Filed:
Aug 16, 2010
Appl. No.:
12/857131
Inventors:
Remigi TSCHUOR - Windisch, CH
Russell Bond JONES - Jupiter FL, US
Luis J. RODRIGUEZ - West Palm Beach FL, US
Hartmut HAEHNLE - Kuessaberg, DE
Marion Oneil DUGGANS - Daytona Beach FL, US
Assignee:
ALSTOM TECHNOLOGY LTD - Baden
International Classification:
F01D 11/00
F01D 5/08
US Classification:
4151701, 415180
Abstract:
A gas turbine includes a turbine section; an annular combustor disposed upstream of the turbine section and configured to discharge a hot gas flow on an outlet side to the turbine section; an outer shell delimiting the combustor and splittable at a parting plane; a plenum enclosing the outer shell; a rotor; a turbine vane carrier encompassing the rotor; a plurality of stator vanes disposed on the vane carrier, and at least two sealing segments forming a ring, each of the at least two sealing segments having an inner edge and a head and a foot section and being movably mounted on the inner edge by the foot section to the outer shell and by the head section to the turbine vane carrier so as to mechanically connect the combustor to the turbine vane carrier.
Marion Oneil Duggans from Daytona Beach, FL, age ~71 Get Report