The Boeing Company

Theboeing Company

Joseph Andrew Bolton

Keith Daniel Humfeld

Murat Saylik

Sarah E Zayic

Matthew R Larson

Niki Lewis

Methods for machining a composite material substrate are discloses comprising integrating a predetermined pattern area having a disbond material for the purpose of creating a disbond region into the composite material substrate at a predetermined thickness, detecting the disbond region and forming a plurality of recesses in the composite material substrate by removing a machined plug from the composite material substrate to form recesses positioned at locations corresponding to the predetermined pattern area, and composite components comprising the recesses machined according to such methods.

Integrally stiffened bonded panel with machined recesses and improved methods of manufacture

A fuel tank disinfection system, including one or more ultraviolet (UV) light emitters disposed within a fuel tank and configured to irradiate one or more water collecting areas within the fuel tank with UV light; and one or more UV light sensors disposed within the fuel tank and in proximity to the one or more water collecting areas and configured to measure the UV light irradiated on the one or more water collecting areas.

System and method for disinfecting fuel tanks

Examples provide a seat assembly, a system including the seat assembly and a method for reducing electromagnetic interference in an aircraft. A seat assembly for an aircraft includes a frame having a base and a support member operatively coupled to the base. A seat is coupled to the base and a first side of the support member. The seat includes a conductive substrate layer configured to absorb electrical charges.

Seat assembly having a conductive substrate layer

In an example, a method for accelerated conditioning of a composite core sandwich coupon is described. The method includes setting a first temperature and a first relative humidity level of the conditioning apparatus, wherein a combination of the first temperature and the first relative humidity level correspond to a desired relative humidity level of the plurality of cells of the core layer at room temperature. The method includes maintaining the first temperature and the first relative humidity for a first period, wherein during the first period a core humidity of the plurality of cells in the core layer approaches the first relative humidity level. The method includes determining that the core humidity has reached the first relative humidity level. The method includes, based on determining that the core humidity has reached the first relative humidity level, adjusting the first temperature to a second temperature.

Systems and methods for accelerated conditioning of composite core sandwich coupons

Methods, systems, and apparatuses are disclosed for the selective and controlled removal of debris from specific areas of a substrate outer surface without adversely impacting the substrate outer surface, including substrate outer surface coatings, and returning an actual substrate outer surface profile containing affixed debris to a predetermined substrate outer surface profile by comparing a library of predetermined profiles to an actual substrate outer surface profile in real time.

Robotic laser and vacuum cleaning for environmental gains

A fastener includes a head that is configured to be engaged by a tool, and a shaft extending from the head. The shaft includes a distal end that is opposite from the head. At least one optical component is coupled to one or both of the head or the shaft. The optical component(s) is configured to allow light to pass through the fastener. A window system includes a panel that includes an exterior surface and an interior surface, and the fastener extending between the exterior surface and the interior surface of the panel. A screen is coupled to the interior surface. The screen receives light from the optical component(s) of the fastener.

Window systems including optical fasteners

An example method for curing a composite part includes placing the composite part onto a topside of a cure tool, and a bottom surface of the composite part contacts the topside of the cure tool and a top surface of the composite part is opposite the bottom surface of the composite part. The method also includes placing the cure tool and the composite part into an autoclave, using the autoclave to apply external heat to the cure tool and the composite part so that air flows over the top surface of the composite part to heat the top surface, and applying additional heat to a backside of the cure tool via radiation provided by at least one heating source of the cure tool, so as to reduce a temperature difference between the backside of the cure tool and the top surface of the composite part being cured.

Systems, cure tools, and methods for thermally curing a composite part

An electrically conductive patch for a sheet that is part of a skin of an aircraft is disclosed. The sheet includes an outermost surface constructed of an electrically conductive material and one or more electrical discharge points that are conductively coupled to the outermost surface of the sheet. The electrically conductive patch is disposed along the outermost surface of the sheet and is conductively coupled to the outermost surface of the sheet. The electrically conductive patch is constructed of a voltage responsive film configured to change from a first coloration and into a second coloration in response to experiencing a threshold voltage difference, where the first coloration substantially matches a coloration of the skin of the aircraft.

Electrically conductive patch for indicating a compromised electrical discharge point in an aircraft

A composite structure forming system configured to form a contoured elongate composite structure in a continuous process is presented. The composite structure forming system comprises a plurality of charge forming stations and a plurality of conveyor systems. The plurality of charge forming stations is configured to operate in parallel, each charge forming station of the plurality of charge forming stations is configured to form a respective composite charge of the contoured elongate composite structure. Each conveyor system of the plurality of conveyor systems is configured to transport a respective composite charge through a respective charge forming station.

Forming contoured elongate composite structures

There is provided a hydraulic system for a vehicle. The hydraulic system has a hydraulic rotary actuator assembly rotationally coupled to a road wheel of the vehicle. The hydraulic rotary actuator assembly has a first operating mode, wherein a rotation of the road wheel causes the hydraulic rotary actuator assembly to pump a fluid from a fluid supply system. The hydraulic system further has a variable restrictor assembly coupled to the hydraulic rotary actuator assembly in the vehicle. The variable restrictor assembly controls a flow of the fluid flowing from the hydraulic rotary actuator assembly, to brake the rotation of the road wheel on a ground surface. The hydraulic system further has a variable restrictor controller coupled to the variable restrictor assembly. The variable restrictor controller controls the variable restrictor assembly, so as to enable a variation of a rate of braking of the road wheel on the ground surface.

Hydraulic system for a vehicle and method of using the same

A method of making a part comprising stacking a plurality of uncured composite sheets to form an uncured composite stack. The method also comprises interposing a resistor wire between an adjacent two of the uncured composite sheets of the uncured composite stack. The method further comprises applying heat to the uncured composite stack externally of the uncured composite stack to at least partially cure the plurality of uncured composite sheets. The method additionally comprises transmitting an electric current through the resistor wire to generate heat, from the resistor wire, internally within the uncured composite stack to at least partially cure the plurality of uncured composite sheets. Applying heat to the uncured composite stack externally and generating heat internally converts the plurality of uncured composite sheets into a plurality of cured composite sheets and converts the uncured composite stack into a cured composite stack.

Method for curing and embedding an antenna in a composite part

A radio-frequency identification ('RFID') device includes a substrate and a load formed in the substrate, where the load includes at least one microchannel and at least one body of fusible metal contained within the at least one microchannel. The RFID device also includes an antenna electrically connected to the load, and a protective layer covering at least a portion of the substrate.

Radio-frequency identification device for indicating a temperature history of a composite structure

Optical fasteners having heads with lenses

Systems, methods, and apparatus for permanent magnet damping and generated light are disclosed. In one or more embodiments, a method for damping and generating light comprises damping, by a permanent magnet (PM) damper connected to a panel (e.g., a door of an aircraft luggage bin), the speed of opening of the panel, while the panel is opened. The method further comprises generating, by the PM damper, electrical power, during the opening of the panel. Also, the method comprises storing the electrical power in an electrical power storage unit, such as a capacitor or a battery. In addition, the method comprises powering, by using the stored electrical power, lighting, such as a lighting emitting diode (LED). Further, the method comprises dissipating any remaining electrical power of the electrical power, which is stored in the electrical power storage unit, when the panel is closed.

Growing community of inventors

Newalla, OK, United States of America

Joseph Andrew Bolton