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公开(公告)号：US11505321B2
公开(公告)日：2022-11-22
申请号：US16901155
申请日：2020-06-15
Applicant: THE BOEING COMPANY
Inventor： Alexander J. Matsuoka , Colin R. Kreiger
Abstract: An apparatus for securing a raceway assembly within an aircraft, which includes a clip assembly associated with the raceway assembly, which secures the raceway assembly to a seat rail. The apparatus further includes a floor panel positioned in overlying relationship to the raceway assembly and the clip assembly.
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Patent Agency Ranking
公开(公告)号：US11362494B2
公开(公告)日：2022-06-14
申请号：US16459531
申请日：2019-07-01
Applicant: The Boeing Company
Inventor： Colin R. Kreiger , Alexander J. Matsuoka , Derrick B. Pruitt , Michael E. Frick , Gregory A. Tubbs
Abstract: There is provided a raceway cover assembly for installing conductive element(s) in an aircraft. The raceway cover assembly includes a raceway cover for removable coupling to a raceway. The raceway is configured for attachment to a sidewall assembly for use in a cabin of the aircraft. The raceway cover includes a first cover side, a second cover side, and retaining element(s) disposed on the first cover side. The raceway cover assembly further includes the conductive element(s) coupled and retained to the first cover side, with the retaining element(s), to form the raceway cover assembly. The conductive element(s) and the raceway cover are assembled together at a location off of the aircraft, prior to installing the raceway cover assembly with the one or more conductive elements in the aircraft, which allows for routing of the one or more conductive elements in the raceway cover at the location off of the aircraft.
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公开(公告)号：US20210387730A1
公开(公告)日：2021-12-16
申请号：US16901155
申请日：2020-06-15
Applicant: THE BOEING COMPANY
Inventor： Alexander J. Matsuoka , Colin R. Kreiger
Abstract: An apparatus for securing a raceway assembly within an aircraft, which includes a clip assembly associated with the raceway assembly, which secures the raceway assembly to a seat rail. The apparatus further includes a floor panel positioned in overlying relationship to the raceway assembly and the clip assembly.
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4.发明授权公开(公告)号：US10992120B2
公开(公告)日：2021-04-27
申请号：US16459499
申请日：2019-07-01
Applicant: The Boeing Company
Inventor： Colin R. Kreiger , Gregory A. Tubbs , Alexander J. Matsuoka , Michael E. Frick , Ryan P. Rogers , Jackson L. Fadely , Derrick B. Pruitt
Abstract: There is provided a sidewall closeout area assembly for an aircraft. The assembly includes a raceway with a first end to attach to a sidewall assembly, a second end to attach to aircraft floor structure(s), and a raceway body with first access opening(s) providing access to one or more of, a crown area and an underfloor area, for conductive elements routed along the raceway. The assembly further includes a raceway cover removably coupled to the raceway and having second access opening(s) providing access to the cabin and to an overfloor area in the cabin for the conductive elements. The assembly further includes a closeout area formed between the raceway body and the raceway cover, to house and protect the conductive elements. The assembly facilitates accessibility to the conductive elements, and provides a routing path for the conductive elements that does not need to be reconfigured for different aircraft cabin layouts.
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公开(公告)号：US20210006051A1
公开(公告)日：2021-01-07
申请号：US16459531
申请日：2019-07-01
Applicant: The Boeing Company
Inventor： Colin R. Kreiger , Alexander J. Matsuoka , Derrick B. Pruitt , Michael E. Frick , Gregory A. Tubbs
Abstract: There is provided a raceway cover assembly for installing conductive element(s) in an aircraft. The raceway cover assembly includes a raceway cover for removable coupling to a raceway. The raceway is configured for attachment to a sidewall assembly for use in a cabin of the aircraft. The raceway cover includes a first cover side, a second cover side, and retaining element(s) disposed on the first cover side. The raceway cover assembly further includes the conductive element(s) coupled and retained to the first cover side, with the retaining element(s), to form the raceway cover assembly. The conductive element(s) and the raceway cover are assembled together at a location off of the aircraft, prior to installing the raceway cover assembly with the one or more conductive elements in the aircraft, which allows for routing of the one or more conductive elements in the raceway cover at the location off of the aircraft.
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6.发明申请公开(公告)号：US20210006050A1
公开(公告)日：2021-01-07
申请号：US16459499
申请日：2019-07-01
Applicant: The Boeing Company
Inventor： Colin R. Kreiger , Gregory A. Tubbs , Alexander J. Matsuoka , Michael E. Frick , Ryan P. Rogers , Jackson L. Fadely , Derrick B. Pruitt
Abstract: There is provided a sidewall closeout area assembly for an aircraft. The assembly includes a raceway with a first end to attach to a sidewall assembly, a second end to attach to aircraft floor structure(s), and a raceway body with first access opening(s) providing access to one or more of, a crown area and an underfloor area, for conductive elements routed along the raceway. The assembly further includes a raceway cover removably coupled to the raceway and having second access opening(s) providing access to the cabin and to an overfloor area in the cabin for the conductive elements. The assembly further includes a closeout area formed between the raceway body and the raceway cover, to house and protect the conductive elements. The assembly facilitates accessibility to the conductive elements, and provides a routing path for the conductive elements that does not need to be reconfigured for different aircraft cabin layouts.
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