The Boeing Company

Harper Engineering Company

Other

Theboeing Company

Richard J LaConte

David Chadwell

Larry C Smith

Michael O Nebeker

James J Johnson

Peter J Arnold

William C Quan

Chad D Schmitz

Mitchell J Piorkowski

David S Melberg

Shannon J Kupfer

Allan B Lewis

Scott P Kube

Tony D Autrey

James J Hanay

Jai W Eller

Ryan Funk

Brian Henderson

A stowage bin assembly includes a bin bucket assembly having a bin bucket which includes at least one sidewall, the at least one sidewall including a notch and the at least one sidewall having an interior surface. The stowage bin assembly also includes at least one hinge assembly. The at least one hinge assembly includes a housing which is received in the notch, the housing having an interior surface, wherein the interior surface of the housing is substantially flush with the interior surface of the at least one sidewall when the housing of the at least one hinge assembly is received in the notch. The stowage bin assembly also includes a stowage bin door pivotably coupled to the bin bucket assembly via the at least one hinge assembly, the stowage bin door moveable between an open position and a closed position. Related components, assemblies, and devices are also provided.

Integrated stowage bin assembly

A stowage bin cover assembly coupleable to a stowage bin is provided. The stowage bin cover assembly includes a stowage bin cover coupleable to the stowage bin, the stowage bin cover including a first groove; and an anti-slip strip coupleably received in the first groove. The anti-slip strip can be positioned and oriented to project above an uppermost outer surface of the first groove such that the anti-slip strip will frictionally engage a payload received in the stowage bin, the frictional engagement resisting movement of the payload. Related methods are also provided.

Overhead storage compartment cover assembly and methods to use same

A method for use when retrofitting a panel of a storage compartment having a mechanical latch assembly with an electric latch assembly includes removing the mechanical latch assembly from the panel of the storage compartment; and preparing the panel of the storage compartment to receive a potted insert. The preparation may include defining and marking a location to receive the potted insert. The method may include removing a portion of the panel to define a potted insert cavity and inserting the potted insert through the potted insert cavity of the panel. The method may also include applying at least one of a potting compound and an adhesive to bond the potted insert to the panel and coupling a portion of the electric latch assembly to the potted insert.

Methods for installation of potted inserts having a latch mechanism

A method of preparing a finished panel and latch combination, wherein the panel and latch mounting combination are seamless and attractive.

Method of fabricating potted panel latch system

A method of preparing and a finished panel and latch combination, wherein the panel and latch mounting combination are seamless and attractive.

Potted panel latch system

A latch assembly includes at least one latch unit having a latch unit housing, a latch notch provided in the latch unit housing, a lock bracket pivotally mounted in the latch unit housing adjacent to the latch notch and positional between latched and unlatched positions and an actuating arm engaging the lock bracket; a torque shaft coupled to the actuating arm; a handle unit having a handle housing and a handle plate pivotally mounted in the handle housing and coupled to the torque shaft; and at least one position indicator lip provided on the handle plate.

Latch assembly

An eccentric fastening device is provided. The eccentric fastening device includes a first threaded fastener, a base and a rotary lug providing a non-fastened pre-assembled position. The base includes a top, a bottom, a stem and a hole, where the stem axially extends from the bottom of the base, and the hole axially extends from the top through the stem of the base. The rotary lug is releasably retained in the hole of the base by the first threaded fastener. The rotary lug includes a cylindrical portion having a thread and a head, wherein the head is offset from the cylindrical portion. The cylindrical portion is substantially axially concentric with the hole of the base, allowing the head to be eccentrically rotated on or off of the stem, whereby a selective structure may be variably clamped and releasably retained between said head and said base. An aircraft having an eccentric fastening device is also provided. A method of installing the same is also provided.

Eccentric fastening device

A dead bolt lock apparatus specifically adapted for use with a flight deck door of an aircraft. The apparatus includes a dead bolt member which can be moved between locked and unlocked positions via a key. A lockout handle is included on the side of the apparatus which faces the flight deck area of the aircraft. The lockout handle is movable rotationally from a first position, wherein it has no affect on the use of the key to unlock the dead bolt, to a second position wherein it prevents the dead bolt from being moved out of a locked position by use of the key. The apparatus thus provides an additional degree of security to occupants of the flight deck by allowing them to prevent unlocking of the apparatus even with the key.

Dead bolt lock assembly for flight deck door of an aircraft

An intruder-resistant latch useful for latching an aircraft flight deck door includes a damper for reducing noise while the door is being operated. The latch also includes a driver member having coated pins that reduce noise while the latch is in operation. The latch allows a flight deck door to be operated with minimal disturbance to a flight crew at work and/or crew members who may be resting. The latch is fabricated of ballistic impact-resistant material(s).

Apparatus and methods for latching an aircraft door

A quick release panel assembly comprising a panel which is releasably fastened to a structure by a release and locking assembly. The release and locking assembly includes a driver element and four actuating arms that are pivotally connected to the driver element, the cover, and to four respective locking mechanisms located at each edge of the panel. The driver element moves the actuating arms between first and second positions to move the locking mechanisms between a locking position to fasten the cover to the structure and an unlocking position.

Growing community of inventors

Black Diamond, WA, United States of America

Richard J LaConte