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公开(公告)号:EP4386664A1
公开(公告)日:2024-06-19
申请号:EP23211548.5
申请日:2023-11-22
申请人: Rolls-Royce plc
发明人: Mulloth, Akhil
IPC分类号: G06T7/00
CPC分类号: G06T7/001
摘要: There is disclosed a method of identifying non-conformance of a manufactured component, the method comprising: performing a volumetric scan to generate a 3-dimensional (3D) image of a volume of space containing the component, the 3D image comprising a plurality of voxels, each voxel representing a sub-volume within the volume of space and assigned a voxel value relating to properties of the material in the sub-volume; generating a component histogram giving the frequency of each voxel value within the volume of space; and comparing the component histogram to a template histogram, and identifying differences between the component histogram and the template histogram, and based on the comparison, determining whether there is a defect in the component.
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公开(公告)号:EP4386193A1
公开(公告)日:2024-06-19
申请号:EP23212942.9
申请日:2023-11-29
申请人: Rolls-Royce plc
IPC分类号: F02K3/115
CPC分类号: F02K3/115
摘要: A thermal management system (100) for a gas turbine engine (10) includes a plurality of inlet and outlet vanes (104, 106) extending from a bypass inner wall (110) towards an outer cowl (120), a plurality of first removable shims (144), a plurality of second removable shims (146), and a third removable shim (148). Each first removable shim (144) extends between and engages the outer cowl (120) and a corresponding inlet vane (104). Each second removable shim (146) extends between and engages the outer cowl (120) and a corresponding outlet vane (106). The third removable shim (148) extends between and engages a heat exchanger (108) and the outer cowl (120). Each of the plurality of first removable shims (144), each of the plurality of second removable shims (146), and the third removable shim (148) is removable for positionally adjusting the outer cowl (120) relative to the bypass inner wall (110).
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公开(公告)号:EP4116562B1
公开(公告)日:2024-06-19
申请号:EP22177422.7
申请日:2022-06-07
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公开(公告)号:EP4382725A1
公开(公告)日:2024-06-12
申请号:EP23208832.8
申请日:2023-11-09
申请人: Rolls-Royce plc
发明人: Harrison, John
CPC分类号: F01D5/027 , F04D29/662 , G01M1/36 , F05D2260/9620130101 , F16F15/32 , F04D29/321 , F04D19/02
摘要: Disclosed is a gas turbine engine rotor balancing apparatus comprising: a rotor configured to rotate about a rotor axis; a substantially annular balancing mass configured to encircle the rotor; and a mass adjustment apparatus for adjusting the position of the balancing mass relative to the rotor.
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公开(公告)号:EP4382257A1
公开(公告)日:2024-06-12
申请号:EP23208838.5
申请日:2023-11-09
申请人: Rolls-Royce plc
发明人: Harrison, Liam , Norton, Andrew
摘要: A section of a continuum arm robot comprising a pair of pivot points at a first and second end of the joint, the section further having a first and second connecting rod connected to the section and joining at the centre of the section, the connecting rods has a plurality of gear teeth at the peripheral ends of the connecting rod that intermesh at a central point on the section.
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公开(公告)号:EP3362268B1
公开(公告)日:2024-05-29
申请号:EP16784246.7
申请日:2016-10-13
CPC分类号: B29C70/38 , G06F30/20 , G06F2113/2620200101 , G06F2113/2420200101
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公开(公告)号:EP4368811A1
公开(公告)日:2024-05-15
申请号:EP23202990.0
申请日:2023-10-11
申请人: Rolls-Royce plc
CPC分类号: F01D5/147 , F01D5/16 , F01D9/065 , F05D2230/3020130101 , F05D2230/3120130101 , F05D2240/12720130101 , F05D2250/2020130101 , F05D2250/7220130101 , F05D2260/2214120130101 , F05D2260/9620130101
摘要: A tie (130) for a component (100) includes a body (132) including an elongate portion (146) and an arch (150) disposed adjacent to the elongate portion (146). The arch (150) includes first and second middle surfaces (156, 162) extending between a pair of first and second outer curved surfaces (154, 160), respectively. The body (132) defines a minimum cross-sectional plane (140) perpendicular to a longitudinal axis (X-X') and passing through the elongate portion (146). The body (132) further includes a minimum tie width (148) at the minimum cross-sectional plane (140) along a second transverse axis (Z-Z'). The minimum tie width (148) is greater than each of a first minimum arch width (158) of the first middle surface (156) and a second minimum arch width (164) of the second middle surface (162) by a width factor greater than or equal to 3 to less than or equal to 10.
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公开(公告)号:EP4366105A1
公开(公告)日:2024-05-08
申请号:EP23201123.9
申请日:2023-10-02
申请人: Rolls-Royce plc
发明人: Trainer, David , Sweet, Mark , Incerpi, Gian , Stevens, Jonathan
摘要: The disclosure relates to an electrical power system with current fault protection provided by current limiting diodes (CLDs). Example embodiments include an electrical power system (600) comprising: an electrical machine (601); an AC:DC power electronics converter (602) connected to receive an input AC supply from the electrical machine (601) and provide an output DC supply across first and second output terminals (603a, 603b); a DC bus (604) connected to first and second output terminals (603a, 603b) of the AC:DC power electronics converter (602); a load (605) connected across the DC bus (604); a first circuit breaker switch (S1) and a first current limiting diode (CLD1) connected in series between the AC:DC power electronics converter (602) and the DC bus (604); and a second circuit breaker switch (S2) and a second current limiting diode (CLD2) connected in series between the DC bus (604) and the load (605), wherein the first current limiting diode (CLD1) is configured to limit current to a higher level than the second current limiting diode (CLD2).
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公开(公告)号:EP4339513A3
公开(公告)日:2024-05-08
申请号:EP23185270.8
申请日:2023-07-13
申请人: Rolls-Royce plc
发明人: Witham, Frederic
IPC分类号: F23R3/28
CPC分类号: F23R3/283 , F23R2900/0001220130101 , F23R2900/0304220130101 , F23R3/002 , F23R3/60
摘要: The present disclosure relates to a combustor assembly 16 for a gas turbine engine 10, the combustor assembly 16 comprising: a combustor wall 30 defining a combustion chamber 25 and comprising an opening periphery 33, the opening periphery 33 defining a first opening 32; a sealing element 34 comprising an annular body 35, the annular body 35 extending around a sealing element axis S and extending through the first opening 32, the sealing element 34 further comprising a flange 38 extending radially outward from the annular body 35 with respect to the axis S to a distal surface 58, the flange 38 slidingly coupling the sealing element 34 and the combustor wall 30 and forming a seal or first partial seal between the sealing element 34 and the combustor wall 30, the annular body comprising an outer surface 37 and an inner surface 36, the inner surface 36 defining a second opening 49 configured to receive a fuel nozzle 40, wherein a first total clearance D1, D2 between the outer surface 37 and the opening periphery 33 in a first direction A is greater than a second total clearance d1, d2 between the outer surface 37 and the opening periphery 33 in a second direction B perpendicular to the first direction A such that the sealing element 34 is able to slide relative to the combustor wall 30 by a greater extent in the first direction A than in the second direction B.
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40.
公开(公告)号:EP3938186B1
公开(公告)日:2024-05-08
申请号:EP20708092.0
申请日:2020-03-03
CPC分类号: B27F7/13 , B29C70/24 , B29C2793/004520130101 , B29C70/545
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