B/e Aerospace, Inc.

Other

Rockwell Collins, Inc.

Club Glider Holdings, LLC

Glenn Allen Johnson

Mark Brian Dowty

Alexander Nicholas Pozzi

Charles Martin Hansson

Kevin Mak

John Paul Pallay

Michael M Princip

Jefferey M McKee

Tommy George Plant

Travis K Finlay

Robert J Henshaw

Adam Lee Smith

Trevor B Skelly

Daniel I Udriste

Suzuko Hisata

Martin Richard Darbyshire

Tracy N Pence

Michael J Baum

Jeffrey W Hontz

Matt Round

Travis J Vaninetti

Javier Valdes De La Garza

John D Edquist

Russell J Kroll

Andrew Gordon Wallace

William E Pangburn

Cameron Smith

Lucas Tretout

Gary Sherrell

Ollie Price

Weiwei He

Benjamin D Stephens

Robert D Wilkey

Bryan Cabatic

James Randy Penley

Francis Xavier Garing

Horng Jaan Lin

Fernando J Rentas

Justin M Pallay

Daniel N Moe

Thomas Martz

Alex L Velet

Lyle T Davis

Lazaro Martinez

Jaan Lin

Nikhil Anthony Saldanha

Adil Mumdood Ali

Craig Cunningham

Mark W Peurifoy

Randy Penley

Maxime Dempah

John H Pratt, Jr

Michael W Kalinowski

Andrew David Mitchell

Brian P Wenger

Gururaja Nekkar

Chirag Krishnamurthy

Adam Paul Warren

James Allen Mazzarelli, Jr

Alexander Filip Grauls

Marc H Schatell

Paul Benedict Rutter

Shawn Raybell

Geraldine Arnold

Kent Kroener

Dennis M Heuer

JaeHun Gu

Nicole Sluder Whyte

Paul A Evens

Ann Tucker

Samikshya Parida

Edgar Owen Kinnier, Iii

Ting-Yu Chen

Jara Freeman

Lawrence J Cudzewicz

Jenny Wilson

Pierre J Vignal

Joachim Gustav Voight

Gary William McKelvey

Mark Wayne Peurifoy

Tracy Neal Pence

Mark P Dowty

Ann M Tucker

Luis Gomez

Martin Darbyshire

Francis X Garing

Adam Smith

Carlos Gatti

Ankit Gupta

An aircraft lavatory is disclosed herein. The aircraft lavatory includes a standard access door providing access to the aircraft lavatory from at least one of an aisle, a cross aisle, or a passageway of an aircraft, a first moveable wall adjacent the standard access door, the first moveable wall having a first end and a second end and configured to move between a closed position and an open position, the first end of the first moveable wall configured to rotate about a first pivot point, and a second moveable wall adjacent the first moveable wall, the second movable wall having a first end and a second end and configured to move between a closed position and an open position, the first end of the second moveable wall configured to rotate about a second pivot point.

Wheelchair accessible airliner lavatory

A triply periodic minimal surface (TPMS) is described. The TPMS is adjustable and tunable depending on desired breathability, vibration performance, weight reduction, pressure distribution, and the like. The TPMS may be used in a cushion of a passenger seat. The cushion may be used for one or more locations of the passenger seat, including a head rest cushion, a back rest cushion, a seat pan cushion, and the like. the TPMS may include a cylindrical gyroid. Each of the cushions may include multiple of the cylindrical gyroids.

Printed optimized TPMS structure

An expandable lavatory and an aircraft cabin configuration including the same. First, second and third walls form the lavatory interior and the third wall is repositionable to expand the lavatory interior footprint to accommodate a wheelchair. The third wall carries a door deployable when the third wall is in the expanded configuration such that the wheelchair can access the lavatory interior via an exit pathway. A first door positioned in the second wall provides access to the lavatory interior via a longitudinal aisle. In some embodiments, a wheelchair securement area is positioned longitudinally aligned with the second door, when the second door is deployed, such that wheelchair access to the lavatory is provided through second door when the lavatory is in the expanded configuration.

Expandable lavatory and cabin configuration including dedicated seating area and expandable lavatory

An economy class (Y class) private suite includes a continuous seatback and a stowable aisle-side panel. The continuous seatback covers the gaps between seats of a 3-seat or 4-seat PAX and the stowable aisle-side panel slides to close off the PAX from the aisle when desirable. Each seat in the PAX includes an extension element to extend from the anterior surface of the seat cushion and establish a substantially flat surface including the seat cushions and extension elements. A separate padded element may be placed over the substantially flat surface. Each seatback cushion in the PAX is removable and reconfigurable as a reclining support or expanded armrest.

Private suite for economy cabin space in aircraft

A slanted aircraft seat privacy panel may include a body. The body may be defined by a contour line along at least a portion of a height of the body. The contour line may be a straight line slanted at an angle relative to a vertical line. The vertical line may be defined relative to a floor of the aircraft cabin. The contour line being slanted may generate increased shoulder space in the passenger compartment in the aircraft cabin. The increased shoulder space in the passenger compartment may use a portion of non-fully utilized space in an adjacent passenger compartment in the aircraft cabin. The passenger compartment and the adjacent passenger compartment may be offset relative to an aisle in the aircraft cabin. A portion of each of the passenger compartment and the adjacent passenger compartment may be formed by the slanted aircraft seat privacy panel.

Slanted aircraft seat privacy panels

A universal passenger seat system includes a system controller and a physical connection interface with a standardized communication protocol for coupling the system controller with seating hardware, at least one peripheral device, and at least one network connection. The system controller can also be in communication with a biometric sensor, a physiological sensor, and/or a situational data sensor. An artificial intelligence engine is communicatively coupled to or embedded within the system controller. The artificial intelligence engine is configured to determine a passenger status based on data received from the biometric sensor, the physiological sensor, and/or the situational data sensor and is further configured to generate one or more communication signals based on the data. For example, the communication signals can include control signals for the seating hardware, information signals for peripheral devices, or status signals for transmission via the network connection.

Universal passenger seat system and data interface

A seat usage prevention device is disclosed. The seat usage prevention deice includes at least one device component being configured to interact with one or more seat components of a first seat. The device component is configured to prevent usage of at least one of a seat pan or seatback of the first seat. The device component further separates a second seat from at least a third seat, wherein the third seat is proximate to at least one of the first seat or the second seat. The seat usage prevention device may include a device component that further includes a cushion, a base, an amenity console, or a vertical separator, or combination thereof.

Seat usage prevention device

A combination adaptive energy absorption and emergency flotation device for positioning beneath a plurality of seat pans of a seat assembly in an aircraft seating application. The device includes a plurality of fluidly coupled inflatable elastic bladders, at least one constrictor valve fluidly coupling at least two adjacent ones of the plurality of inflatable elastic bladders allowing fluid flow therethrough in response to predetermined pressure on the device from the plurality of seat pans, and a fluid supply source fluidly coupled to the plurality of inflatable elastic bladders for outputting a positive flow of fluid to the plurality of inflatable elastic bladders, wherein the adaptive energy absorption device is detached from the plurality of seat pans to allow removal from beneath the plurality of seat pans for use as an emergency flotation device.

Combination energy impact attenuation, vibration mitigation and flotation device for aircraft seating applications

A static aircraft seat privacy panel may include a body. At least a portion of a surface of the body may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge of the body may be configured to couple to a floor via a set of floor-mounted components. The set of floor-mounted components may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge of the body may be configured to be offset a selected distance from a surface of one or more overhead structures of the aircraft cabin when the body is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel may be compliant with 9G force requirements for aviation transport.

Static aircraft seat privacy panels

A system for both onboard piloting and remote piloting an aircraft having thereon at least one onboard pilot includes an aircraft having an onboard flight control system, onboard flight control devices, and onboard condition indicators mounted proximal the pilot seat. A remote flight control system, in electronic communication with the onboard flight control system, includes remote flight control devices and remote condition indicators. At least in a remote piloting mode, the onboard flight control system transmits flight and aircraft condition-related signals to the remote flight control system, receives flight control signals from the remote flight control system, and actuates, according to the flight control signals received from the remote flight control system, onboard actuators thereby remote piloting the aircraft. In the remote piloting mode, the aircraft may be cooperatively piloted by a remote pilot and at least one alert onboard pilot as another onboard pilot rests.

Methods and systems for remote piloting a two-pilot aircraft for extended flights

An aircraft passenger compartment suite may include a privacy divider configured to separate a first side of the aircraft passenger compartment suite including a first aircraft seat and a second side of the aircraft passenger compartment suite including a second aircraft seat. The aircraft passenger compartment suite may include a collapsible display device positioned proximate to the privacy divider of the aircraft passenger compartment suite. The aircraft passenger compartment suite may include a first display device and a first plate configured to be an extension of a horizontal surface in the first side when the first display device is in a first display device stowed position. The aircraft passenger compartment suite may include a second display device and a second plate configured to be an extension of a horizontal surface in the second side when the second display device is in a second display device stowed position.

Actuatable display devices for aircraft passenger compartment suites

An aircraft passenger compartment suite may include a privacy shell element proximate to an aircraft seat installed within the aircraft passenger compartment suite. The privacy shell element may include a first section configured to conform to a primary section of the aircraft seat, and a second section configured to conform to an auxiliary section of the aircraft seat. The privacy shell element may include a first profile configured to conform with the aircraft seat when the aircraft seat is in a first position, and a second profile configured to conform with the aircraft seat when the aircraft seat is in a second position. The second profile of the privacy shell element may be configured to occupy a greater amount of passenger aircraft living space surrounding the aircraft passenger compartment suite than an amount of passenger aircraft living space occupied by the first profile of the privacy shell element.

Contoured passenger seat privacy shell shape of aircraft passenger compartment suites

An aircraft passenger compartment suite may include at least one single passenger compartment including at least one single aircraft seat. The at least one single aircraft seat may be configured to seat a single passenger. The aircraft passenger compartment suite may include a combined divan passenger compartment with a combined divan aircraft seat. The combined divan aircraft seat may be configured to seat at least one passenger. The combined divan aircraft seat may have a width greater than a width of the at least one single aircraft seat. The combined divan passenger compartment may include a stowage compartment configured to stow large passenger amenities in a substantially vertical orientation. The aircraft passenger compartment suite may include a privacy divider separating the combined divan passenger compartment and the at least one single passenger compartment.

Combined divan aircraft seat for aircraft passenger compartment suites

Systems and methods for monitoring passenger activity in an aircraft cabin environment to predict immediate future passenger needs. The systems and methods make use of sensors positioned within an aircraft cabin environment configured to sense condition changes of objects corresponding to predetermined service issues, device(s) usable by the service crew indicating the sensed condition changes, and processing circuitry configured to receive sensor signals and indicate the condition changes through the device(s) such that the service crew is made aware of the condition changes requiring actions to be completed by the service crew to attend to the immediate future passenger needs.

Predictive aircraft passenger cabin service system and method

Growing community of inventors

Rural Hall, NC, United States of America

Glenn Allen Johnson