公开(公告)号：US20200061948A1

公开(公告)日：2020-02-27

申请号：US16106808

申请日：2018-08-21

Applicant: THE BOEING COMPANY

Inventor： Jamie J. Childress ,  Lindsey Flangas

IPC: B30B9/30

Abstract: A trash compactor assembly includes a receptacle including a base connected to at least one wall having an upper edge. A retaining chamber is defined between the wall(s) and the upper edge. A compaction plate is disposed within the retaining chamber. The compaction plate is configured to be manually moved in an upward direction from the base towards the upper edge to compact trash within the retaining chamber.

公开(公告)号：US20190177083A1

公开(公告)日：2019-06-13

申请号：US15839300

申请日：2017-12-12

Applicant: THE BOEING COMPANY

Inventor： Jamie J. Childress ,  Daniel Joseph Perron

IPC: B65F1/14 ,  B64D11/02 ,  B30B15/16 ,  B30B15/00

Abstract: A trash compactor system includes a receptacle defining a retaining chamber that is configured to receive and retain trash, a compaction plate moveably secured within the retaining chamber, and a foot pedal operatively coupled to the compaction plate. Engagement of the foot pedal moves the compaction plate within the retaining chamber to compact the trash retained within the retaining chamber. A flap may cover an opening into the retaining chamber. The foot pedal may also be operatively coupled to the flap, such that the engagement of the foot pedal moves the flap into an open position that exposes the opening.

公开(公告)号：US10279902B2

公开(公告)日：2019-05-07

申请号：US14500691

申请日：2014-09-29

Applicant: The Boeing Company

Inventor： Jamie J. Childress ,  Daniel J. Perron

IPC: B64C29/00 ,  B64C39/02

Abstract: An aircraft launch system includes a riser coupleable to an aircraft. The riser includes an actuator and a tether coupled to the actuator. The aircraft launch system further includes a sky crane coupled to the tether. The actuator is operable to retract the tether and draw together the sky crane and the aircraft.

公开(公告)号：US09745034B2

公开(公告)日：2017-08-29

申请号：US14929561

申请日：2015-11-02

Applicant: The Boeing Company

Inventor： Jamie J. Childress ,  Marci A. George ,  Paul L. Wynns ,  Kurt A. Matthews ,  John J. Fagan, Jr. ,  Egan Greenstein

IPC: B63G8/14 ,  B64D1/02 ,  B64D17/00 ,  B63B21/48

CPC classification number: B63G8/14 ,  B63B21/48 ,  B63B22/003 ,  B63B22/18 ,  B64D1/02 ,  B64D17/00

Abstract: A method for deploying a payload into a body of water using a deployment vessel, the deployment vessel including a hull defining a payload compartment, the method including positioning the payload in the payload compartment of the deployment vessel, the deployment vessel and the payload having a buoyancy, wherein the buoyancy is initially negative, deploying the deployment vessel into the water at a drop zone, wherein the deployment vessel moves horizontally through the water as it submerges vertically downward under a force of gravity, changing the buoyancy to positive after a minimum horizontal distance is established between the drop zone and the deployment vessel, thereby causing the deployment vessel to surface and, after the surfacing of the deployment vessel, opening the hull to release the payload therefrom.

公开(公告)号：US20160090179A1

公开(公告)日：2016-03-31

申请号：US14500691

申请日：2014-09-29

Applicant: The Boeing Company

Inventor： Jamie J. Childress ,  Daniel J. Perron

IPC: B64C29/00 ,  B64C39/02

CPC classification number: B64C29/0091 ,  B64C39/024 ,  B64C2201/088

Abstract: Described herein is an aircraft launch system that includes a riser coupleable to an aircraft. The riser includes an actuator and a tether coupled to the actuator. The aircraft launch system further includes a sky anchor coupled to the tether. The actuator is operable to retract the tether and draw together the sky anchor and the aircraft.

Abstract translation: 这里描述的是包括可与飞机相连的提升板的飞行器发射系统。 提升管包括联接到致动器的致动器和系绳。 飞机发射系统还包括耦合到系绳的天空锚。 致动器可操作以缩回系绳并将天空锚和飞机拉在一起。

公开(公告)号：US12246103B2

公开(公告)日：2025-03-11

申请号：US17455093

申请日：2021-11-16

Applicant: THE BOEING COMPANY

Inventor： Jamie J. Childress ,  Arthur Edward Brockschmidt, Jr.

IPC: A61L2/10 ,  A61L2/26

Abstract: A sanitizing system and method include multiple ultraviolet (UV) lamps and a power supply module. The UV lamps each include one or more UV emitters configured to emit UV light. The UV lamps are positioned to emit the UV light towards one or more target components within a space. The power supply module is electrically connected to each of the UV lamps and configured to provide electrical energy to the UV lamps to power the UV emitters to sanitize the one or more target components.

公开(公告)号：US12172753B2

公开(公告)日：2024-12-24

申请号：US17645908

申请日：2021-12-23

Applicant: THE BOEING COMPANY

Inventor： Jamie J. Childress

IPC: B64D11/00 ,  B64D47/08 ,  B64F1/36 ,  G06V20/00 ,  G06V20/59 ,  G08B21/18 ,  G06V20/52

Abstract: A system of monitoring carry-on items for a flight of an aircraft includes one or more cameras positioned to capture images of carry-on items associated with passengers of an aircraft. The system includes an interface configured to receive image data from the one or more cameras. The system also includes one or more processors coupled to the interface. The one or more processors are configured to analyze the image data to determine characteristics of a carry-on item. The one or more processors are configured to determine that one or more alert conditions are satisfied based on a comparison of one or more alert criteria to the characteristics of the carry-on item and data associated with the aircraft. The one or more processors are also configured to send, to one or more devices, an output based on satisfaction of the one or more alert conditions.

公开(公告)号：USD1052155S1

公开(公告)日：2024-11-19

申请号：US29735235

申请日：2020-05-19

Applicant: THE BOEING COMPANY

Designer： Christopher Edward Plass ,  Jamie J. Childress

公开(公告)号：US12144904B2

公开(公告)日：2024-11-19

申请号：US17703209

申请日：2022-03-24

Applicant: THE BOEING COMPANY

Inventor： Jamie J. Childress ,  Jeffrey Scott Bissell

IPC: A61L2/10 ,  H05K9/00

Abstract: An ultraviolet (UV) light sanitizing system includes an electromagnetic interference (EMI) reducing cover configured to couple to a housing of a UV lamp assembly having a UV light source that is configured to emit UV light through a light outlet of the housing. The EMI reducing cover is further configured to be disposed one or more of within, below, or over the light outlet. The EMI reducing cover includes one or more grids including beams and light openings defined between the beams. The light openings provide open areas through which the UV light emitted from the UV light source passes, and wherein the EMI reducing cover includes at least 90% open space. In at least one embodiment, the beams include at least one surface that is transverse to a direction of the UV light that is to be emitted from the UV light source. In at least one embodiment, wherein the EMI reducing cover includes an interior grid and an exterior grid.

公开(公告)号：US12000176B2

公开(公告)日：2024-06-04

申请号：US17472906

申请日：2021-09-13

Applicant: THE BOEING COMPANY

Inventor： Jamie J. Childress

IPC: E05B47/00 ,  E05B63/00 ,  B64D11/02

CPC classification number: E05B47/004 ,  E05B47/0012 ,  E05B63/0065 ,  B64D11/02 ,  E05B2047/0056 ,  E05B2047/0067

Abstract: A latching system and method are configured to selectively latch and unlatch a first component in relation to a second component. The latching system and method include an actuator, a first coupler secured to the actuator, a latch, and a second coupler secured to the latch. The first coupler is configured to couple to the second coupler to couple the actuator to the latch. The first coupler is configured to uncouple from the second coupler to uncouple the actuator from the latch in response to the latch being manually operated.