MY6800109A - Method of repairing a metallic hull for buoyant vessel - Google Patents

Method of repairing a metallic hull for buoyant vessel

Info

Publication number
MY6800109A
MY6800109A MY1968109A MY6800109A MY6800109A MY 6800109 A MY6800109 A MY 6800109A MY 1968109 A MY1968109 A MY 1968109A MY 6800109 A MY6800109 A MY 6800109A MY 6800109 A MY6800109 A MY 6800109A
Authority
MY
Malaysia
Prior art keywords
repairing
buoyant vessel
metallic hull
hull
metallic
Prior art date
Application number
MY1968109A
Original Assignee
Alfred Alphonse Yee
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alfred Alphonse Yee filed Critical Alfred Alphonse Yee
Publication of MY6800109A publication Critical patent/MY6800109A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
MY1968109A 1964-12-02 1968-12-31 Method of repairing a metallic hull for buoyant vessel MY6800109A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB49101/64A GB1034260A (en) 1964-12-02 1964-12-02 Aerofoil-shaped blade for use in a fluid flow machine

Publications (1)

Publication Number Publication Date
MY6800109A true MY6800109A (en) 1968-12-31

Family

ID=10451151

Family Applications (1)

Application Number Title Priority Date Filing Date
MY1968109A MY6800109A (en) 1964-12-02 1968-12-31 Method of repairing a metallic hull for buoyant vessel

Country Status (5)

Country Link
US (1) US3353351A (en)
DE (2) DE1280618B (en)
FR (1) FR1454951A (en)
GB (2) GB1034260A (en)
MY (1) MY6800109A (en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3412979A (en) * 1965-12-10 1968-11-26 Rolls Royce Aerofoil-shaped blade for use in a fluid flow machine such as a turbine
US3726604A (en) * 1971-10-13 1973-04-10 Gen Motors Corp Cooled jet flap vane
US4989404A (en) * 1988-12-12 1991-02-05 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US5220794A (en) * 1988-12-12 1993-06-22 Sundstrand Corporation Improved fuel injector for a gas turbine engine
US4967562A (en) * 1988-12-12 1990-11-06 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US4967563A (en) * 1988-12-12 1990-11-06 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US5027603A (en) * 1988-12-28 1991-07-02 Sundstrand Corporation Turbine engine with start injector
US5241818A (en) * 1989-07-13 1993-09-07 Sundstrand Corporation Fuel injector for a gas turbine engine
US5239818A (en) * 1992-03-30 1993-08-31 General Electric Company Dilution pole combustor and method
DE4309131A1 (en) * 1993-03-22 1994-09-29 Abb Management Ag Method and appliance for influencing the wake in furnace fittings
DE4336143C2 (en) * 1993-10-22 1995-11-16 Erich Wuerzinger Cooling process for turbomachinery
DE19651881A1 (en) * 1996-12-13 1998-06-18 Asea Brown Boveri Combustion chamber with integrated guide vanes
DE50107283D1 (en) * 2001-06-18 2005-10-06 Siemens Ag Gas turbine with a compressor for air
US7070386B2 (en) 2004-06-25 2006-07-04 United Technologies Corporation Airfoil insert with castellated end
WO2006053825A1 (en) * 2004-11-16 2006-05-26 Alstom Technology Ltd Gas turbine system and associated combustion chamber
US8713909B2 (en) * 2009-03-04 2014-05-06 United Technologies Corporation Elimination of unfavorable outflow margin
US9169733B2 (en) 2013-03-20 2015-10-27 General Electric Company Turbine airfoil assembly
US10711702B2 (en) * 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
US10578028B2 (en) 2015-08-18 2020-03-03 General Electric Company Compressor bleed auxiliary turbine
US20200182068A1 (en) * 2018-12-05 2020-06-11 United Technologies Corporation Axial flow cooling scheme with structural rib for a gas turbine engine
US10822963B2 (en) 2018-12-05 2020-11-03 Raytheon Technologies Corporation Axial flow cooling scheme with castable structural rib for a gas turbine engine
US11603766B1 (en) 2022-05-04 2023-03-14 Pratt & Whitney Canada Corp. Turbine stator vanes having inserts and splitter plates

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641040A (en) * 1948-01-02 1953-06-09 Esther C Goddard Means for cooling turbine blades by air
US2858100A (en) * 1952-02-01 1958-10-28 Stalker Dev Company Blade structure for turbines and the like
GB753224A (en) * 1953-04-13 1956-07-18 Rolls Royce Improvements in or relating to blading for turbines or compressors
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
US2920866A (en) * 1954-12-20 1960-01-12 A V Roe Canada Ltd Hollow air cooled sheet metal turbine blade
FR1177035A (en) * 1957-05-28 1959-04-20 Snecma Method and device for cooling machine parts
GB854135A (en) * 1958-03-05 1960-11-16 Rolls Royce Improvements in or relating to combustion equipment
DE1204021B (en) * 1959-04-27 1965-10-28 Rolls Royce Blade for axial flow machines, especially gas turbines
GB898368A (en) * 1959-06-23 1962-06-06 Rolls Royce Improved combustion chamber
US3242674A (en) * 1961-05-05 1966-03-29 Lucas Industries Ltd Liquid fuel combustion apparatus
GB938247A (en) * 1962-03-26 1963-10-02 Rolls Royce Gas turbine engine having cooled turbine blading

Also Published As

Publication number Publication date
DE1280618B (en) 1968-10-17
DE1476892B2 (en) 1970-11-12
US3353351A (en) 1967-11-21
FR1454951A (en) 1966-02-11
DE1476892A1 (en) 1970-07-16
GB1068280A (en) 1967-05-10
GB1034260A (en) 1966-06-29

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