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821 条记录 (耗时 0.014 秒)

    PROPULSION SYSTEM FOR AN AIRCRAFT
    3.
    发明公开
    PROPULSION SYSTEM FOR AN AIRCRAFT 审中-公开

    公开(公告)号：EP3406526A2

    公开(公告)日：2018-11-28

    申请号：EP18173393.2

    申请日：2018-05-21

    申请人： General Electric Company

    发明人： BARONE, Dominic ,  GEMIN, Paul Robert

    IPC分类号： B64D27/24 ,  B64D35/02 ,  B64D27/02

    CPC分类号： B64D27/24 ,  B64D27/10 ,  B64D27/16 ,  B64D35/02 ,  B64D2027/026 ,  B64D2221/00 ,  F01D15/10 ,  F02C3/04 ,  F05D2220/323 ,  Y02T50/64

    摘要： A propulsion system 50, 350 for an aircraft 10 includes an electric generator 56, 356 mechanically driven by a combustion engine, with the electric generator 56, 356 configured to generate alternating current electrical power. The propulsion system 50, 350 additionally includes a power bus 58, 356 electrically connected to the electric generator 56, 356 and configured to receive and transmit the alternating current electrical power generated by the electric generator 56, 356. Additionally, the propulsion system 50, 350 includes, an electric propulsor assembly comprising an electric motor 360 and a propulsor drivingly connected to the electric motor 360, the electric motor 360 electrically coupled to the power bus 58, 356 for the receiving alternating current electrical power from the power bus 58, 356.

    SCHAUFELGITTERPLATTFORM
    5.
    发明公开
    SCHAUFELGITTERPLATTFORM 审中-公开

    公开(公告)号：EP3401504A1

    公开(公告)日：2018-11-14

    申请号：EP17170495.0

    申请日：2017-05-10

    申请人： MTU Aero Engines AG

    发明人： Maatouk, Fadi ,  Brettschneider, Markus ,  Mahle, Inga

    IPC分类号： F01D5/14 ,  F01D9/04

    CPC分类号： F01D5/145 ,  F01D5/143 ,  F01D9/04 ,  F01D9/041 ,  F05D2220/323 ,  F05D2240/11 ,  F05D2240/80

    摘要： Offenbart wird ein Schaufelgittersegment (110, 120, 130, 140, 150) eines Schaufelgitters für eine Strömungsmaschine, das eine Plattform (10) mit einer Plattformoberfläche sowie mindestens zwei Schaufelblätter (20, 30) umfasst. Die Plattformoberfläche weist eine an das erste Schaufelblatt heranreichende Vertiefung (111, 121, 131, 141, 151) auf, welche die Druckseite (21) des ersten Schaufelblattes stromab von 80% der axialen Gitterbreite (g) stromab Anströmkanten (23, 33) berührt und die Druckseite (21) des ersten Schaufelblattes bis zu maximal 80% der axialen Gitterbreite (g) stromab Anströmkanten (23, 33) berührt. Mindestens ein tiefster Punkt (112, 122) der Vertiefung liegt wenigstens 90% der axialen Gitterbreite (g) stromab der Anströmkanten (23, 33).
    Offenbart sind ferner ein Schaufelgitter, ein Schaufelkanal, eine Plattform, eine Strömungsmaschine und ein Flugzeugtriebwerk.

    FLUGGASTURBINE MIT VARIABLER AUSTRITTSDÜSE EINES NEBENSTROMKANALS
    8.
    发明公开
    FLUGGASTURBINE MIT VARIABLER AUSTRITTSDÜSE EINES NEBENSTROMKANALS 审中-公开

    公开(公告)号：EP3387244A1

    公开(公告)日：2018-10-17

    申请号：EP16805124.1

    申请日：2016-12-01

    申请人： Rolls-Royce Deutschland Ltd & Co KG

    发明人： KÖPF, Frank Uwe

    IPC分类号： F02K1/08

    CPC分类号： F02K1/08 ,  B64D27/16 ,  B64D31/06 ,  F05D2220/323

    摘要： The invention relates to an aircraft gas turbine, comprising a core engine (10) and a bypass flow channel (25), which bypasses the core engine and which forms an outlet nozzle (31) together with a casing (29) of the core engine (10) and together with a radially outer housing wall (30), characterized in that a ring element (32), which can be displaced in the axial direction, is arranged in the region of the outlet nozzle (31), wherein a ring channel (33) that can be varied by the displacement of the ring element (32) is formed between the casing (29) of the core engine (10) and the ring element (32).

    VANE COOLING SYSTEM
    9.
    发明公开
    VANE COOLING SYSTEM 审中-公开

    公开(公告)号：EP3385505A1

    公开(公告)日：2018-10-10

    申请号：EP18160511.4

    申请日：2018-03-07

    申请人： Rolls-Royce plc

    发明人： Pitt, Simon

    IPC分类号： F01D9/02 ,  F01D9/06 ,  F01D25/12

    CPC分类号： F01D25/12 ,  F01D9/02 ,  F01D9/023 ,  F01D9/041 ,  F01D9/06 ,  F01D9/065 ,  F05D2220/32 ,  F05D2220/323 ,  F05D2240/12 ,  F05D2260/201 ,  Y02T50/675

    摘要： A vane cooling system for a gas turbine engine comprises a vane (21) arranged on a stator and having a chamber (23) extending continuously from a radially inner end to a radially outer end of the vane. The vane (21) has; a radially inner inlet (24) and a radially outer inlet (25), a first cooling fluid feed (39) in communication with the radially inner inlet (24) and a second cooling fluid feed (28) in communication with the radially outer inlet (25), The first cooling fluid feed (39) has a higher pressure than the second cooling feed (28). A flow adjustment device (30) is arranged for adjusting a flow of the second cooling fluid feed into the radially outer inlet (25).

    VANE STRUT POSITIONING AND SECURING SYSTEMS
    10.
    发明授权
    VANE STRUT POSITIONING AND SECURING SYSTEMS 有权

    公开(公告)号：EP3093442B1

    公开(公告)日：2018-10-10

    申请号：EP16160455.8

    申请日：2016-03-15

    申请人： United Technologies Corporation

    发明人： DIBENEDETTO, Enzo ,  BINTZ, Matthew E.

    IPC分类号： F01D9/04 ,  F01D17/16

    CPC分类号： F01D17/14 ,  F01D9/02 ,  F01D9/042 ,  F01D17/162 ,  F05D2220/323 ,  F05D2230/60

    摘要： A strut-flap vane system for a turbomachine includes a vane strut (211) comprising an airfoil portion (211 b) and a strut mount (211a) extending in a radially outward direction from the airfoil portion. The strut mount forms a hollow semi-cylinder and includes threading (211 c) on an outer diameter thereof. The system includes an aft mount portion or portions (201) defining a hollow semi-cylinder configured to form a strut cylinder (203) with the strut mount such that the aft mount portion can be disposed in contact with the strut mount to form the strut cylinder. The strut cylinder defines a cylinder opening (205) and the aft mount portion includes threading (201 c) on an outer diameter thereof that aligns with the threading of the strut mount to allow a strut spanner nut (207) to mesh with both the strut mount and the mount portion. Furthermore, a method of assembling is disclosed.