The Boeing Company

Theboeing Company

Timothy Mark Jones

Russell Warren Keck

Michael Steven Lewis

Christopher J Mills

Harold G Erickson

Roland D Mair

Nathanial C Cuddy

Chris Gren McInelly

Daniel E Rivera

Mitchell Zachary Kotlik

Derrick Joseph Hanratty

Tushar Mayur Sampat

Emily Yang

Michael Patrick Durbin

Lauryn T Zolondek

Jeremy P Harris

Mark Andrew Lewandowski

Chris Gren Mcinelly

Nathaniel C Cuddy

Harold Glenn Erickson

An adhesive membrane that includes a plurality of spherical particles bonded together so as to form interstitial gaps between the spherical particles. The plurality of spherical particles comprise an adhesive and form a lattice. The interstitial gaps are a size that is larger than a water vapor molecule.

Adhesion membrane technology

A fastener assembly includes a base which defines a bore which extends through the base. The fastener assembly further includes a receptacle wherein the receptacle includes a sidewall wherein the sidewall defines a channel which extends through the receptacle. The channel extends from a first opening defined by the sidewall to a second opening defined by the sidewall and the sidewall is connected to the base wherein the second opening aligns with the bore of the base. The sidewall of the receptacle defines a vent opening which extends through the sidewall. The receptacle and the base define a flow path through the vent opening of the sidewall, through the channel of the receptacle, through the second opening of the sidewall of the receptacle and through the bore of the base.

Air management of honeycomb composite inserts

A floor panel connection system for attaching a floor panel to an aircraft airframe is disclosed. The connection system includes a vertical load resisting coupling device and a shear load resisting coupling device to connect the floor panel to the airframe and resist forces applied to the panel. The vertical load resisting coupling device is configured to resist forces perpendicular to a top facial plane of the floor panel, without significantly resisting lateral forces. The shear load resisting coupling device is configured to resist forces parallel to the top facial plane of the floor panel, without significantly resisting vertical forces.

Aircraft floor panel floating connection system

Aircraft floor panel connection system

Aircraft passageway storage units are disclosed herein. An example apparatus includes a storage assembly to be supported on a floor of an interior of a fuselage of an aircraft. The storage assembly has a corner to be adjacent a passageway of the interior of the fuselage, and the passageway is to extend around the corner. The example apparatus also includes a door coupled to the storage assembly. The door extends from a first side of the storage assembly to a second side of the storage assembly and defines a portion of the corner. The door is to cover an opening of a compartment of the storage assembly when the door is in a closed position, and the opening is to extend from the first side to the second side.

Aircraft passageway storage units

A track fitting assembly having an engaged position and an unengaged position. The track fitting assembly may include a lower track fitting, a cam member, a button, and a biasing member. The lower track fitting may define a recess therein and at least one retaining feature. The retaining feature may be configured to hold the lower track fitting within a track if the track fitting assembly is in the engaged position. The cam member may have a cam main body that defines an aperture. The button may have an indicator surface. The button may be selectively retained within the recess of the lower track fitting. The biasing member may be configured to exert a biasing force. The biasing member may be retained within the recess of the lower track fitting and positioned relative to the button to exert the biasing force against the button.

Track fitting assembly having a visible indicator to confirm engagement with a track

Aircraft passageway storage unit

A method and apparatus having an elongate housing and connectors. The elongate housing has a channel configured to hold a number of lines. The connectors extend from a side of the elongate housing. The connectors are configured to engage channels formed in a surface of a structure such that the elongate housing is connected to the structure.

Snap-in raceway

A method for privately transferring filtered air through a partition of a compartment in an aircraft cabin to equalize a pressure difference between the inside and outside the compartment via a vent assembly comprising two substantially structurally identical vent halves joining together in a locking manner through a vent opening in the partition. Each vent half comprising integrally molded rim, frame, plurality of louvers fixed within the frame, latch, keeper, guide prong, and a installation index key; plastic injection molded from high strength unreinforced polycarbonate.

Interlocking vent assembly for equalizing pressure in a compartment

Growing community of inventors

Lake Stevens, WA, United States of America

Timothy Mark Jones