Reduced stress internal manifold heat shield attachment
AssigneePratt & Whitney Canada Corp.
InventorsJason Fish, Bhawan B. Patel, Saeid Oskooei
Life of this patent
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Abstract
A fuel manifold assembly for a gas turbine engine fuel system comprises a fuel manifold at least partly enclosed by a heat shield, the internal manifold being made of a first material having a first coefficient of thermal expansion, and the heat shield being made of a second material having a second coefficient of thermal expansion that is lower than the first coefficient of thermal expansion.
Claims8
A fuel manifold assembly for a gas turbine engine comprising a fuel manifold at least partly enclosed by a heat shield, the fuel manifold being made entirely of a first material and the heat shield being made entirely of a second material that is different from the first material, said first material having a first coefficient of thermal expansion and said second material having a second coefficient of thermal expansion that is lower than the first coefficient of thermal expansion such that the heat shield expands less than the fuel manifold when exposed to the same temperature, wherein differential thermal growth between the internal manifold and the heat shield at engine operating temperatures is reduced.
A method of reducing thermally-generated stress at a joint between a fuel manifold and a heat shield of a fuel manifold assembly in a gas turbine engine, the method comprising:
- selecting a first material having a first coefficient of thermal expansion for the fuel manifold;
- and selecting a second material having a second coefficient of thermal expansion for the heat shield, the second coefficient of thermal expansion being lower than the first coefficient of thermal expansion;
- and permitting the heat shield to expand less than the fuel manifold when exposed to the same temperature, which reduces differential thermal growth between the internal manifold and the heat shield at engine operating temperatures and thereby reduces thermally-generated stress at the joint between the fuel manifold and the heat shield.
A fuel injection system for gas turbine engine including a compressor, a combustor and a turbine, comprising:
- an annular internal fuel manifold disposed adjacent the combustor within a surrounding engine casing, the fuel manifold having at least one fuel conveying passage therein in fluid flow communication with a plurality of fuel injection nozzles disposed along the fuel manifold and adapted to spray fuel into the combustor, and a fuel inlet connected to the fuel manifold and providing fuel flow to the fuel conveying passage, the fuel manifold being made entirely of a first material having a first coefficient of thermal expansion;
- and
- an annular heat shield at least partially covering the fuel manifold about the circumference thereof and fastened thereto by at least one circumferentially extending joint, the heat shield being made of a second material having a second coefficient of thermal expansion that is lower than the first coefficient of thermal expansion, such that the heat shield expands less than the fuel manifold when exposed to the same temperature and wherein differential thermal growth between the fuel manifold and the heat shield at engine operating temperatures is reduced.
Dependencies are inferred from the claim text.