公开(公告)号：CA2996029A1

公开(公告)日：2017-04-06

申请号：CA2996029

申请日：2016-03-30

Applicant: C&D ZODIAC INC

Inventor： SAVIAN SCOTT ,  SCOLEY IAN GEOFFREY ,  LONG ERIC

IPC: A47K17/02 ,  B64D11/02 ,  E03C1/322

Abstract: A toilet module attachment assembly that includes a retainer member that is adapted to be secured to a wall. The retainer member includes a wall attachment flange and a press fit portion extending generally inwardly from the wall attachment flange. When the retainer member is secured to a wall a channel is defined between the wall and the press fit portion. The attachment assembly also includes a seal member that includes a bulge portion that is received in the channel of the retainer member.

公开(公告)号：CA2943779C

公开(公告)日：2017-01-17

申请号：CA2943779

申请日：2013-02-13

Applicant: C&D ZODIAC INC

Inventor： SAVIAN SCOTT ,  KEARSEY STEPHEN

IPC: B64D11/00 ,  B60R7/00 ,  B64D9/00

Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated, with the first side panel and the bucket, and a second pivot mechanism operatively associated, with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along and are rotatable about a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

公开(公告)号：CA2898647C

公开(公告)日：2016-11-08

申请号：CA2898647

申请日：2014-02-13

Applicant: C&D ZODIAC INC

Inventor： SAVIAN SCOTT ,  KEARSEY STEPHEN ,  WILLIAMS COREY

IPC: B64D11/00 ,  B60R5/00 ,  B64C1/22

Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

公开(公告)号：CA2978623A1

公开(公告)日：2016-09-09

申请号：CA2978623

申请日：2016-03-02

Applicant: C&D ZODIAC INC

Inventor： SAVIAN SCOTT ,  SHETTY SANDESH ,  SANDBERG ROY BENJAMIN

IPC: B60N2/00 ,  B64D11/06 ,  G06F17/50

Abstract: A computerized system for determining the design layout of an aircraft. The system includes an input module configured to receive a first input data indicating a first value of a first parameter, a first feature database that includes a plurality of feature settings, a feature search module configured to search the first feature database and select a feature setting based on the first value of the first parameter, a central database that includes a plurality of rules governing a design layout of a fuselage, and an optimizing module in communication with the central database and configured to generate an optimal design layout based on the selected feature setting.

公开(公告)号：CA2963324A1

公开(公告)日：2016-05-06

申请号：CA2963324

申请日：2015-10-27

Applicant: C&D ZODIAC INC

Inventor： KEARSEY STEPHEN ,  LONG ERIC ,  SAVIAN SCOTT

IPC: B64D11/00

Abstract: A latch system that includes a paddle button assembly having a button that is movable between a home position and an actuation position, a first latch assembly that includes a first striker assembly and a first hook assembly, and a first cable that extends between the paddle button assembly and the first latch assembly. Movement of the button from the home position to the actuation position moves the first cable, thereby disengaging the first hook assembly and the first striker assembly.

公开(公告)号：CA2860094C

公开(公告)日：2016-03-29

申请号：CA2860094

申请日：2013-02-13

Applicant: C&D ZODIAC INC

Inventor： SAVIAN SCOTT

IPC: B64D11/00 ,  B64D47/02 ,  F21S8/10

Abstract: A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and. a panel positioned above and connected, to the PSU pod. The PSU pod includes at least first and second reading lights positioned, within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.

公开(公告)号：CA2898647A1

公开(公告)日：2014-08-21

申请号：CA2898647

申请日：2014-02-13

Applicant: C & D ZODIAC INC

Inventor： SAVIAN SCOTT ,  KEARSEY STEPHEN ,  WILLIAMS COREY

IPC: B64D11/00 ,  B64C1/22

Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

公开(公告)号：CA2860094A1

公开(公告)日：2013-08-22

申请号：CA2860094

申请日：2013-02-13

Applicant: C & D ZODIAC INC

Inventor： SAVIAN SCOTT

IPC: G05F1/00

Abstract: A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and. a panel positioned above and connected, to the PSU pod. The PSU pod includes at least first and second reading lights positioned, within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.