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公开(公告)号:US1038534A
公开(公告)日:1912-09-17
申请号:US1911654004
申请日:1911-10-11
发明人: DAKE CHARLES W
CPC分类号: F01D1/12
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公开(公告)号:US1035544A
公开(公告)日:1912-08-13
申请号:US1911604085
申请日:1911-01-23
发明人: DAKE WILFORD W
CPC分类号: F01D1/12
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公开(公告)号:US951373A
公开(公告)日:1910-03-08
申请号:US1909478759
申请日:1909-02-19
申请人: KEMBLE THOMAS S
发明人: KEMBLE THOMAS S
CPC分类号: F01D1/12
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公开(公告)号:US923146A
公开(公告)日:1909-06-01
申请号:US1903163713
申请日:1903-06-30
申请人: GEN ELECTRIC
发明人: CURTIS CHARLES G
CPC分类号: F01D1/12
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公开(公告)号:US888181A
公开(公告)日:1908-05-19
申请号:US1907387991
申请日:1907-08-10
申请人: LINDNER FRANK H
发明人: LINDNER FRANK H
CPC分类号: F01D1/12
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公开(公告)号:US846896A
公开(公告)日:1907-03-12
申请号:US1906328400
申请日:1906-07-30
申请人: BECKER NICOLAUS
发明人: BECKER NICOLAUS
CPC分类号: F01D1/12
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公开(公告)号:US788097A
公开(公告)日:1905-04-25
申请号:US1903168732
申请日:1903-08-08
发明人: EHRHART RAYMOND N
CPC分类号: F01D1/12
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公开(公告)号:US733722A
公开(公告)日:1903-07-14
申请号:US1902110861
申请日:1902-06-09
申请人: LOUNT SAMUEL
发明人: LOUNT SAMUEL
CPC分类号: F01D1/12
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公开(公告)号:US09995216B1
公开(公告)日:2018-06-12
申请号:US15688521
申请日:2017-08-28
申请人: Mustafa Rez , Bassel Rez
发明人: Mustafa Rez , Bassel Rez
IPC分类号: F02C3/073 , F02C3/16 , F02C5/04 , F01D1/32 , F02C3/045 , F02C3/067 , F02K3/072 , F02C7/08 , F02C7/10
CPC分类号: F02C3/073 , F01D1/12 , F01D1/32 , F02C3/045 , F02C3/067 , F02C3/16 , F02C3/165 , F02C5/04 , F02C7/08 , F02C7/10 , F02K3/072
摘要: A disc turbine engine includes a multi disc engine in which each disc engine includes a turbine blade, and low-pressure compressor blade, a high-pressure compressor blade and a bearing that runs the disc engine freely around a shaft. Each disc engine has its own cooling system, the compressor's blades act as cooling fins for the turbine blade, and air bleeding from the high-pressure compressor to the lower pressure compressor through a hollow turbine blade. Cooling the nozzle is by attaching the nozzle to the guide fan and by air bleeding through the hollow body. There is no stator in between the disc engine and no large shaft is required because the power produced by each turbine blade is consumed by its own compressor. The weight and cost of this engine will be less than other engines at the same thrust output.
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