-
公开(公告)号：US20230331370A1
公开(公告)日：2023-10-19
申请号：US17659671
申请日：2022-04-19
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc R. Matsen , Waeil M. Ashmawi , Sahrudine Apdalhaliem
CPC classification number: B64C3/26 , B29C70/685 , B29C35/0805 , B29C2035/0811 , B29K2101/12
Abstract: Stiffened skin panels comprise alternating truss core portions and solid laminate portions sandwiched between inner and outer facesheets, all formed from a fiber reinforced thermoplastic. The components of the panels are co-consolidated using induction heating. The panels are stiffened with spars fastened to the solid laminate portions.
-
12.发明申请公开(公告)号：US20200088661A1
公开(公告)日：2020-03-19
申请号：US16691896
申请日：2019-11-22
Applicant: The Boeing Company
Abstract: A computer-implemented method of determining moisture content of a composite structure is provided. The method includes performing a thermal analysis calculation on the composite structure to determine a temporal surface temperature profile of the composite structure based on temporal environmental parameter profiles, wherein the surface temperature profile is determined independently of a moisture content of the composite structure. The method also includes performing a moisture content analysis calculation on the composite structure to determine a moisture content of the composite structure, wherein the moisture content analysis calculation is based on the determined temporal surface temperature profile and a thickness of the composite structure. The thermal analysis calculation is performed iteratively with a first time period and the moisture content analysis calculation is performed iteratively with a second time period that is longer than the first time period.
-
公开(公告)号：US10000299B2
公开(公告)日：2018-06-19
申请号：US14838442
申请日：2015-08-28
Applicant: THE BOEING COMPANY
Inventor： Waeil M. Ashmawi , Sahrudine Apdalhaliem
IPC: B64F5/00 , B29C65/02 , B01J35/06 , B64C1/10 , B01J31/06 , B29C65/54 , B29C65/48 , B29K701/12 , B29L9/00 , B29L31/30
CPC classification number: B64F5/40 , B01J31/06 , B29C65/14 , B29C66/112 , B29C66/116 , B29C66/532 , B29C73/22 , B29K2701/12 , B29K2713/00 , B29L2009/00 , B29L2031/3082 , B64C1/062 , B64C1/10 , B64C1/12
Abstract: Methods and apparatuses are disclosed relating to multilayer 3D textile composite materials containing self-healing resins for use as protective structures on stationary objects, and moving objects including, without limitation, vehicles including spacecraft and aircraft.
-
公开(公告)号：US09957049B2
公开(公告)日：2018-05-01
申请号：US14012383
申请日：2013-08-28
Applicant: The Boeing Company
Inventor： Sahrudine Apdalhaliem , Kimberly Dawn Meredith , Morteza Safai , Lon E. Switzer , Thomas Seth Perkins , Scott A. Langdon , Tuan D. Nguyen
CPC classification number: B64D11/00 , B64C1/14 , B64C1/1423 , B64C1/1484 , B64C1/32 , E06B7/00 , E06B7/28 , Y10T29/49826
Abstract: A heated roller shade system is provided. The heated roller shade system includes a roller located in a cavity defined between an inner wall of a vehicle and an outer wall of the vehicle. The roller shade system also includes a shade coupled to the roller. The roller is configured to selectively move the shade between a deployed position and an open position. The roller shade system also includes a heating mechanism coupled to at least one of the roller and the shade. The heating mechanism facilitates increasing a temperature of at least one of the roller and the shade.
-
公开(公告)号：US09919505B2
公开(公告)日：2018-03-20
申请号：US14340914
申请日：2014-07-25
Applicant: THE BOEING COMPANY
Inventor： Moushumi Shome , Sahrudine Apdalhaliem , Frederick T. Calkins , Waeil M. Ashmawi , Kimberly Meredith
IPC: B29C70/34 , B29C70/54 , B32B37/00 , B32B37/10 , B32B37/18 , B29C33/38 , B29C33/48 , B29C70/44 , B29L31/30
CPC classification number: B32B37/1036 , B29C33/38 , B29C33/485 , B29C70/446 , B29C70/54 , B29K2905/00 , B29L2031/3076 , B32B37/0046 , B32B37/18 , B32B2605/18 , Y02T50/43
Abstract: In one or more aspects of the present disclosure, a mandrel is disclosed. The mandrel having a shape memory alloy (SMA) shell having a longitudinal axis, an interior extending along the longitudinal axis and an exterior contour, the SMA shell being configured to interface with a structure to be cured, and at least one SMA actuation member disposed within the interior and connected to the SMA shell, where the at least one SMA actuation member is configured to exert pressure against the SMA shell effecting an interface pressure between the exterior contour of the SMA shell and the structure to be cured where the exterior contour has a predetermined actuated shape that corresponds to a predetermined cured shape of the structure to be cured.
-
Patent Agency Ranking
公开(公告)号：US09731455B2
公开(公告)日：2017-08-15
申请号：US14476611
申请日：2014-09-03
Applicant: The Boeing Company
Inventor： Kimberly D. Meredith , Morteza Safai , Sahrudine Apdalhaliem , William B. Avery
IPC: B29C70/58 , B07C5/36 , B07C5/34 , B07C5/342 , B07C5/04 , B29C70/62 , B29C70/14 , B29C70/12 , B29C31/04 , B29C31/08 , B29B17/02 , B29L31/30 , B29K105/26 , B29K105/14 , B29K105/12 , B29K105/06
CPC classification number: B29C70/58 , B07C5/04 , B07C5/34 , B07C5/3422 , B07C5/3425 , B07C5/368 , B07C2501/0018 , B29B17/02 , B29B2017/0279 , B29C31/045 , B29C31/085 , B29C70/12 , B29C70/14 , B29C70/62 , B29K2105/06 , B29K2105/12 , B29K2105/14 , B29K2105/26 , B29L2031/3097 , Y02W30/622
Abstract: Chopped fiber composite systems and methods are disclosed. Sorting systems include a conveyor, an imager, a plurality of receptacles, a pneumatic device, and controller. Molding systems include a conveyor, an imager, a mold, a pneumatic device, and a controller. The controller directs the pneumatic device to alter the freefall of chopped fiber composite pieces based on characteristics of the chopped fiber composite pieces as they drop from the conveyor and into a receptacle or a mold. Sorting and molding methods include dropping chopped fiber composite pieces, detecting characteristics of the dropping pieces, and directing the pieces based on the detected characteristics.
-
17.发明申请公开(公告)号：US20170190137A1
公开(公告)日：2017-07-06
申请号：US15465029
申请日：2017-03-21
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc Rollo Matsen , Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , John B. Moser , Brett I. Lyons , Moushumi Shome , Kay Y. Blohowiak
CPC classification number: B32B1/08 , B29C33/52 , B29C70/205 , B29C70/462 , B29C2035/0811 , B32B5/024 , B32B2262/106 , B32B2605/08 , B32B2605/12 , B32B2605/18 , D04C1/06
Abstract: Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.
-
18.发明申请METHODS AND SYSTEMS FOR DETERMINING AN ALLOWABLE MOISTURE CONTENT IN A COMPOSITE STRUCTURE 审中-公开用于确定复合结构中允许水分含量的方法和系统公开(公告)号：US20160370309A1
公开(公告)日：2016-12-22
申请号：US14745813
申请日：2015-06-22
Applicant: THE BOEING COMPANY
IPC: G01N25/00
CPC classification number: G01N25/00 , B64F5/60 , G01N17/00 , G01N33/442
Abstract: A method of determining an allowable moisture content of a composite structure includes performing a thermal analysis on the composite structure to determine a surface temperature profile of the composite structure. The surface temperature profile is determined independently of a moisture content of the composite structure. The method also includes performing a moisture analysis on the composite structure to determine an allowable moisture content of the composite structure such that the moisture analysis is based on the determined surface temperature profile.
Abstract translation: 确定复合结构的允许水分含量的方法包括对复合结构进行热分析以确定复合结构的表面温度分布。 独立于复合结构的水分含量来确定表面温度分布。 该方法还包括对复合结构进行水分分析以确定复合结构的允许含水量，使得水分分析基于确定的表面温度分布。
-
19.发明申请ASSEMBLIES INCLUDING SHAPE MEMORY ALLOY FITTINGS AND COMPOSITE STRUCTURAL MEMBERS 有权包括形状记忆合金配件和复合结构件的组装公开(公告)号：US20160003280A1
公开(公告)日：2016-01-07
申请号：US14323529
申请日：2014-07-03
Applicant: The Boeing Company
Inventor： Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , Jeffery L. Marcoe , Moushumi Shome
IPC: F16B17/00
CPC classification number: F16B1/0014
Abstract: Provided are assemblies having composite structures interlocked with shape memory alloy structures and methods of fabricating such assemblies. Interlocking may involve inserting an interlocking protrusion of a shape memory alloy structure into an interlocking opening of a composite structure and heating at least this protrusion of the shape memory alloy structure to activate the alloy and change the shape of the protrusion. This shape change engages the protrusion in the opening such that the protrusion cannot be removed from the opening. The shape memory alloy structure may be specifically trained prior to forming an assembly using a combination of thermal cycling and deformation to achieve specific pre-activation and post-activation shapes. The pre-activation shape allows inserting the interlocking protrusion into the opening, while the post-activation shape engages the interlocking protrusion within the opening. As such, activation of the shape memory alloy interlocks the two structures.
Abstract translation: 提供了具有与形状记忆合金结构互锁的复合结构的组件和制造这种组件的方法。 联锁可以包括将形状记忆合金结构的互锁突起插入到复合结构的互锁开口中，并且加热形状记忆合金结构的至少该突起以激活合金并改变突起的形状。 这种形状变化与开口中的突起接合，使得突起不能从开口移除。 在使用热循环和变形的组合形成组件以实现特定的预激活和后激活形状之后，形状记忆合金结构可以被特别地训练。 预激活形状允许将互锁突起插入开口中，而后激活形状与开口内的互锁突起接合。 因此，形状记忆合金的激活将两个结构互锁。
-
公开(公告)号：US20150296565A1
公开(公告)日：2015-10-15
申请号：US14248782
申请日：2014-04-09
Applicant: The Boeing Company
Inventor： Sahrudine Apdalhaliem , Kimberly D. Meredith , Morteza Safai
IPC: H05B1/02
CPC classification number: H05B1/0236 , B64C1/1484 , B64C1/1492 , H05B3/84
Abstract: A method and apparatus for managing heating of a window system. The apparatus comprises a dimmable window panel and a heating system. The dimmable window panel has an inner portion and an outer portion around the inner portion. The heating system is thermally connected to the outer portion of the dimmable window panel.
Abstract translation: 一种用于管理窗系统的加热的方法和装置。 该装置包括可调光窗板和加热系统。 可调光窗板具有围绕内部部分的内部部分和外部部分。 加热系统热连接到可调光窗板的外部。
-
-
-
-
-
-
-
-
-
Search Results
61
records
(took 0.028 seconds)
