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公开(公告)号：US12103660B2
公开(公告)日：2024-10-01
申请号：US18163765
申请日：2023-02-02
Applicant: Textron Aviation Inc.
Inventor： Michael John Seibel , Jamie L. Taber , Sidney Aloysius Mohr
CPC classification number: B64C1/24 , A47B5/04 , A47B31/06 , B64D9/00 , H01F7/0252 , Y10T403/32319
Abstract: A table is incorporated into an aircraft staircase design. The table can be deployed when the stairs are stowed inside the aircraft cabin area. The table is upwardly biased such that when it is released from a locking mechanism the table flips up to horizontal.
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公开(公告)号：US11919643B2
公开(公告)日：2024-03-05
申请号：US16421207
申请日：2019-05-23
Applicant: Rockwell Collins, Inc.
Inventor： Travis J. Vaninetti , Justin C. Christenson , Jefferey M. McKee
CPC classification number: B64D11/0007 , A47B31/04 , A47B31/06 , B64D11/0023 , B64D2011/0038
Abstract: A self-deploying counter for an aircraft monument is disclosed. In embodiments, the monument is installable adjacent to a cabin space within an aircraft passenger cabin (e.g., on either side of an exit door) and the self-deploying counter includes a partition door capable of being pivoted between a default closed position and an open position extending into the cabin space. The self-deploying counter has a horizontal top surface and an undersurface. When the partition door is deployed, the counter pivots in concert with the door's deployment, the fully deployed position corresponding to the open position of the partition door.
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公开(公告)号：US10059241B2
公开(公告)日：2018-08-28
申请号：US15651505
申请日：2017-07-17
Applicant: Winnebago Industries, Inc.
Inventor： Steven Jergenson
CPC classification number: B60N3/001 , A47B1/10 , A47B5/04 , A47B5/06 , A47B31/04 , A47B31/06 , A47B83/045 , A47B2200/0063 , B60P3/36
Abstract: A table system includes a cabinet housing, a slide frame positioned within the cabinet housing, an adjustable table assembly including a table support frame slideably coupled to the slide frame, and a pivot system. The pivot system includes a support mast and a sliding component. The sliding component is coupled to the support mast such that the sliding component is configured to slide up the support mast such that the adjustable table assembly pivots around a pivot point between an extended position and a folded position.
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公开(公告)号：US20180208320A1
公开(公告)日：2018-07-26
申请号：US15928203
申请日：2018-03-22
Applicant: THE BOEING COMPANY
Inventor： Thomas Joseph Moran
CPC classification number: B64D13/00 , A47B31/06 , A47B2031/002 , B62B2202/67 , B62B2204/00 , B62B2204/04 , B64D11/0007 , B64D11/04 , B64D2013/0629
Abstract: A galley cart includes walls defining an interior cavity extending between a front and a rear of the galley cart and the interior cavity extending between a top end and a bottom end. A supply port is provided in flow communication with the interior cavity at or near either the top end or the bottom end of the cart. A return port is provided in flow communication with the interior cavity that is adjacent the supply port at or near the top end or the bottom end of the cart. A barrier is positioned between the supply port and the return port within the interior cavity of the cart to define a supply chamber and a return chamber to control airflow through the interior cavity.
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公开(公告)号：US09957050B2
公开(公告)日：2018-05-01
申请号：US14716357
申请日：2015-05-19
Applicant: THE BOEING COMPANY
Inventor： Thomas Joseph Moran
CPC classification number: B64D13/00 , A47B31/06 , A47B2031/002 , B62B2202/67 , B62B2204/00 , B62B2204/04 , B64D11/0007 , B64D11/04 , B64D2013/0629
Abstract: A galley cart includes walls defining an interior cavity extending between a front and a rear of the galley cart and the interior cavity extending between a top end and a bottom end. A supply port is provided in flow communication with the interior cavity at or near either the top end or the bottom end of the cart. A return port is provided in flow communication with the interior cavity that is adjacent the supply port at or near the top end or the bottom end of the cart. A barrier is positioned between the supply port and the return port within the interior cavity of the cart to define a supply chamber and a return chamber to control airflow through the interior cavity.
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公开(公告)号：US09889935B2
公开(公告)日：2018-02-13
申请号：US14302648
申请日：2014-06-12
Applicant: B/E AEROSPACE, INC.
Inventor： Peter John Leslie Burd
CPC classification number: B64D11/04 , A47B31/06 , A47B2031/002 , B62B3/004 , B62B2202/67 , E06B7/16 , Y02T50/46
Abstract: An aircraft galley cart bay door includes a door main structure having an inwardly facing peripheral inner edge with an inner surface, and a surface seal on the inner surface of the inwardly facing peripheral inner edge of the inner wall. A substantial majority of the main structure of the door is formed from a high strength molded carbon fiber composite material. The door main structure may optionally define a recess, and insulation material can be disposed in the recess defined by the main structure of the door.
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公开(公告)号：US20180027960A1
公开(公告)日：2018-02-01
申请号：US15660963
申请日：2017-07-27
Inventor： WOLFGANG DRESSLER , SEMSI HAJREDINAJ
Abstract: A habitable motor vehicle includes an interior, an ambience around the vehicle, an opening between the interior and ambience, a door which closes the opening, an insect protection device fastened to the vehicle, a table, and a fastening device which is releasably fastens the table to the vehicle. The insect protection device has an insect protection screen which at least partly closes the opening. The fastening device has coupling members comprising a table coupling member arranged on the table, and a vehicle coupling member arranged on a side of the motor vehicle in a region of the opening. The table and vehicle coupling members are releasably coupled to each other. The table extends from the opening laterally into the ambience when the coupling members are coupled. An intermediate space is formed between the table and the interior having the insect protection screen arranged therein when the coupling members are coupled.
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公开(公告)号：US09695619B2
公开(公告)日：2017-07-04
申请号：US15136813
申请日：2016-04-22
Applicant: B/E Aerospace, Inc.
Inventor： Peter John Leslie Burd
IPC: E05C3/06 , E05C19/00 , E05C1/10 , E05C3/14 , B64D11/04 , E05C19/04 , A47B31/06 , E05C1/00 , E05C19/02 , E05B13/00 , B64D11/00 , E05C3/16
CPC classification number: E05C1/10 , A47B31/06 , B64D11/0007 , B64D11/04 , E05B13/004 , E05C1/002 , E05C3/14 , E05C3/16 , E05C19/009 , E05C19/028 , E05C19/04 , Y02T50/46 , Y10T292/108
Abstract: A galley cart bay door latch system serves to secure catering or galley carts, as are used on commercial aircraft, within the aircraft's galley. The system relies on two substantially horizontally disposed latch levers to secure the galley door which in turn restrains a galley cart in position within the galley. The ends of the latch levers are received in a recess formed in the door to secure the door. Raising the latch lever releases the door and positively pushes the door outwardly. The latching configuration allows the doors to be slammed shut without the need to further manipulate the latch levers.
