Power transmission arrangement
First Claim
1. A power transmission arrangement for a gas turbine engine having in axial flow series a first stage compressor, a second stage compressor, a first stage turbine and a second stage turbine, a first main shaft connecting the first stage turbine to the second stage compressor so that the first stage turbine drives the second stage compressor during operation of the engine, and a second main shaft connecting the second stage turbine to the first stage compressor so that the second stage turbine drives the first stage compressor during operation of the engine, said power transmission arrangement comprising:
- a first power transmission member connectable to the first main shaft;
a second power transmission member connectable to the second main shaft;
a third power transmission member; and
a coupling assembly having a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft via the first power transmission member, and having a selectable decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the second main shaft to the third transmission member via the second transmission member.
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Accused Products
Abstract
A power transmission arrangement comprises a first power transmission member connectable to a first main shaft of an engine. The arrangement also includes a second power transmission member connectable to a second main shaft of the engine and to a third power transmission member. A coupling assembly is provided which has a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft of the engine via the first power transmission member. The coupling assembly has a decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the main shaft of the engine to the third power transmission member via the second power transmission member.
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Citations
43 Claims
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1. A power transmission arrangement for a gas turbine engine having in axial flow series a first stage compressor, a second stage compressor, a first stage turbine and a second stage turbine, a first main shaft connecting the first stage turbine to the second stage compressor so that the first stage turbine drives the second stage compressor during operation of the engine, and a second main shaft connecting the second stage turbine to the first stage compressor so that the second stage turbine drives the first stage compressor during operation of the engine, said power transmission arrangement comprising:
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a first power transmission member connectable to the first main shaft; a second power transmission member connectable to the second main shaft; a third power transmission member; and a coupling assembly having a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft via the first power transmission member, and having a selectable decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the second main shaft to the third transmission member via the second transmission member. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28)
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29. A power transmission arrangement for a gas turbine engine, said gas turbine engine comprising:
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an intermediate pressure compressor; a high pressure compressor; a high pressure turbine; an intermediate pressure turbine; a first main shaft connecting said high pressure compressor and said high pressure turbine; a second main shaft connecting said intermediate pressure compressor and said intermediate pressure turbine; and a power transmission arrangement arranged between said intermediate compressor and said high pressure compressor, said power transmission comprising; a coupling assembly; a first power transmission shaft connected to said first main shaft; a second power transmission shaft connected to said second main shaft; and a third power transmission member, wherein said second power transmission shaft is arranged within said first power transmission shaft, and wherein said first and second power transmission shafts are selectively coupled to, and decoupled from, each other by said coupling assembly to allow power to be transmitted from the third power transmission member via the power transmission arrangement to the first main shaft when the first and second power transmission shafts are selectively coupled and to allow power to be transmitted to the third power transmission member via the power transmission arrangement from the second main shaft when the first and second power transmission shafts are selectively decoupled. - View Dependent Claims (30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43)
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Specification