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公开(公告)号：EP4442579A1
公开(公告)日：2024-10-09
申请号：EP24164680.1
申请日：2024-03-19
IPC分类号： B64F5/10
摘要： A robotic manufacturing system includes a track extending along a length of a component of a partially manufactured item, wherein the component has a non-constant longitudinal shape, the track being supported independently of the partially manufactured item. The system includes a jointed member having an elongated arcuate shape, a mount longitudinally movable along the track and configured to receive the jointed member in an articulating manner, and an end effector movably mounted on the jointed member. The jointed member is movable along a portion of the component length in a radial position sympathetic to the non-constant component longitudinal shape. The jointed member is longitudinally movable relative to the mount along its elongated arcuate shape such that the jointed member will move in an arc spaced from and around an outer component surface. A portion of the end effector is movable along a length of the jointed member.
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公开(公告)号：EP4180334B1
公开(公告)日：2024-10-09
申请号：EP22205880.2
申请日：2022-11-07
IPC分类号： B64D41/00
CPC分类号： B64D2013/061120130101 , B64D2041/00520130101 , B64D41/00 , Y02T90/40
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公开(公告)号：EP4438470A1
公开(公告)日：2024-10-02
申请号：EP23165763.6
申请日：2023-03-31
发明人： Hoffmann, Lars , Gössing, Rolf , Hamm, Martin
IPC分类号： B64C13/42 , F04B23/04 , F04B49/06 , F15B11/17 , F04B49/00 , F04B49/20 , F15B20/00 , B64D45/00
CPC分类号： B64C13/42 , F04B23/04 , F04B49/06 , F15B11/17 , F15B2211/2051520130101 , F15B2211/665120130101 , F15B2211/63320130101 , F15B2211/875720130101 , F15B20/004 , F15B2211/2057620130101 , F04B49/007 , F04B2203/0220130101 , B64D2221/0020130101 , B64D2045/008520130101 , F04B17/03 , F04B2203/020820130101
摘要： In order to increase availability of hydraulic power from different electric power sources, the invention provides an apparatus (22) and a method for hydraulically powering at least one consumer (14) of a hydraulic system (12) of an aircraft (10), the hydraulic system (12) comprising:
a first electrical power source (A) and a first electrically driven motor pump (MPU1) electrically powered by the first electrical power source (A),
a second electrical power source (B) and a second electrically driven motor pump (MPU2) electrically powered by the second electrical power source (B),
and a hydraulic power generation control (26) which controls a supply of electrical energy from the first and second electrical power sources (A, B) to the first and second motor pumps (MPU1, MPU2). The invention proposes to determine the actual available electrical power (APA, APB) of each of the first and second electrical power sources (A, B) and to set a load factor (UPA, UPB) of each motor pump (MPU1, MPU2) in order to share a load to generate hydraulic power demanded from the at least one consumer (14) between the first and second motor pumps (MPU1, MPU2), wherein each load factor is set depending from the actual available electrical power (APA, APB).-
公开(公告)号：EP4438225A2
公开(公告)日：2024-10-02
申请号：EP24163660.4
申请日：2024-03-14
发明人： FADLOVICH, Chace , DAVIS, Eric
CPC分类号： B23Q2210/00620130101 , B23Q1/4876 , B23Q1/525 , B23Q5/20
摘要： An apparatus for performing operations on a part, and in particular on the fuselage of an aircraft. The apparatus utilizes a spool with a cable wound therearound to move end effectors. The ends of the cable are fixed to an arched beam. Thus, rotation of the spool either moves the beam or moves the spool. The apparatus moves along rails that may be mounted to a fixed structure like floors or walls.
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公开(公告)号：EP4438224A1
公开(公告)日：2024-10-02
申请号：EP24163967.3
申请日：2024-03-15
发明人： FADLOVICH, Chace , POSPISIL, Eric , BERRY, Joseph , GRIMSTAD, Mike , WOOGERD, Michael , GARCIA AMADO, Juan Francisco
CPC分类号： B23Q1/012 , B23Q2210/00620130101 , B64F5/10
摘要： An apparatus for performing operations on a part, and in particular on the fuselage of an aircraft. The apparatus utilizes movable arches which carry an and effector and which move along a track fixed to a structure. Additional, fixed arches are positioned at specific longitudinal positions and when the movable arches are aligned with the fixed arches, the end effector may move from the movable arch to the fixed arch.
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公开(公告)号：EP4299971B1
公开(公告)日：2024-09-18
申请号：EP22181308.2
申请日：2022-06-27
IPC分类号： F17C9/00
CPC分类号： F17C9/00 , F17C2221/01220130101 , F17C2223/016120130101 , F17C2223/03320130101 , F17C2223/04620130101 , F17C2225/03520130101 , F17C2227/013520130101 , F17C2227/014220130101 , F17C2227/033920130101 , F17C2227/038820130101 , F17C2265/06620130101 , F17C2223/016920130101 , F17C2225/016920130101 , F17C2221/03220130101 , F17C2221/03520130101 , F17C2225/016120130101 , F17C2227/010720130101 , F17C2227/011420130101 , F17C2227/03620130101 , F17C2250/04320130101 , F17C2260/05620130101 , F17C2270/018920130101 , F17C2270/018420130101
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公开(公告)号：EP4424591A1
公开(公告)日：2024-09-04
申请号：EP23159111.6
申请日：2023-02-28
发明人： Andreani, Luc
IPC分类号： B64C9/02
摘要： In order to improve the attachments of aircraft components (16) to an aircraft wing (14) with regard to simple design and better load distribution, the invention provides an aircraft component support arrangement (46) for connecting the aircraft component (16) to an aircraft wing (14), including a component support (38) and an attachment device (48) for attaching the component support (38) to a wing structure (62), the attachment device (48) comprising:
a first to third connection means (60.1, 60.2, 60.3) for connecting the component support (38) to the wing structure (62), the first to third connection means (60.1, 60.2, 60.3) each comprising a floating bearing (66.1, 66.2, 66.3) permitting linear movement in direction of a first to third axis (68.1, 68.2, 68.3), respectively, and angular rotation about a central point in two orthogonal directions, wherein the first to third connection means (60.1, 60.2, 60.3) are spaced apart from each other in two dimensions to connect the component support (38) at three different locations to the wing structure (62) and wherein at least one of the first to third axes (68.1, 68.2, 68.3) has a different orientation to the others of the first to third axes (68.1, 68.2, 68.3).-
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公开(公告)号：EP4417062A1
公开(公告)日：2024-08-21
申请号：EP23156492.3
申请日：2023-02-14
CPC分类号： C21D1/18 , F25D31/00 , A47J2027/00620130101
摘要： A method (100) for automatically processing a subject material (200) and a corresponding automatic processing apparatus (10) for carrying out the method is provided. The method (100) comprises processing (101) a processing medium (19) within a processing medium reservoir (11) to predefined conditions, holding (102) the processing medium (19) within the processing medium reservoir (11) at the predefined conditions, arranging (103) the subject material (200) to be tempered relative to a processing container (12), such that the subject material (200) at least partially is located within the processing container (12), and starting (104) a tempering cycle. The method then comprises continuously transporting (105), via a pump (13), the processing medium (19), during a processing time, from the processing medium reservoir (11) into the processing container (12), wherein the processing medium (19) enters the processing container (12) via an inlet opening (16) and exits the processing container (12) by overflowing via an outlet opening (17), such that a fixed processing medium level (22) is present within the processing container (12) during the processing cycle, and removing (107) the processing medium (19) from the processing container (12) back into the processing medium reservoir (11) via the inlet opening (16) when the processing time is reached. The automatic processing process may, e.g., be a tempering process, or a galvanization process, or another process for treating a subject material (200) with a processing medium.
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