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公开(公告)号：US10099338B2
公开(公告)日：2018-10-16
申请号：US15280133
申请日：2016-09-29
Applicant: The Boeing Company
Inventor： Bernard L. DiAntonio , Antonio Paesano
IPC: B24B23/00 , B24B23/08 , B24B57/00 , B24B19/14 , B24B23/02 , B23P6/00 , B24B41/06 , B24B55/00 , B23Q11/00
Abstract: A portable booth assembly for receiving a work piece to facilitate working on a work area of the work piece including a housing and an inner core disposed within an interior area of the housing is provided. The portable booth assembly includes an aperture that is formed in the housing and the inner core. The aperture is configured to receive the work piece. The inner core defining the aperture is configured to be supported by the work piece if the work piece is large, or support the work piece if the work piece is small, and isolate the work area within the portable booth assembly. The portable booth assembly further includes a cut out formed in the housing. The cut out is configured to enable access to the work area for working on the work area.
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公开(公告)号：US11346001B2
公开(公告)日：2022-05-31
申请号：US16863614
申请日：2020-04-30
Applicant: The Boeing Company
Inventor： Antonio Paesano
IPC: C23C18/30 , C23C18/31 , C23C18/20 , C23C18/16 , C23C18/22 , C23C18/32 , C25D3/12 , C25D5/54 , C23C18/28
Abstract: An example method of coating a substrate involves cleaning the substrate and, after cleaning the substrate, sensitizing the substrate using a sensitizing solution including tin chloride and hydrochloric acid. The method also involves, after sensitizing the substrate, activating the substrate in an activating solution including palladium chloride and hydrochloric acid. Further, the method involves subsequently neutralizing the substrate using a neutralizing solution including ammonium hydroxide. Still further, the method involves, after neutralizing the substrate, depositing an electroless nickel layer on the substrate. The method may then involve depositing an electrolytic nickel layer on top of the electroless nickel layer, and depositing an outer layer of metallic material, ceramic material, polymeric material, or any combination thereof on top of the electrolytic nickel layer.
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公开(公告)号：US09482096B1
公开(公告)日：2016-11-01
申请号：US14698334
申请日：2015-04-28
Applicant: The Boeing Company
Inventor： Antonio Paesano , Robert B. Thompson
CPC classification number: F01D5/141 , B63B1/06 , B63B1/36 , B63H25/38 , B64C3/26 , B64C2230/22 , F05D2220/323 , F05D2220/36 , F05D2240/30 , F05D2250/63 , F15D1/005 , Y02T70/121
Abstract: A surface area of a structure is fabricated with a textured surface that reduces the surface wear rate or erosion caused by a high speed flow of fluid containing abrasive particles over the surface area. More particularly, a leading edge surface such as a rotor leading edge surface, an aircraft airfoil leading edge surface, a propeller leading edge surface, etc. is fabricated with a textured surface comprised of a plurality of grooves that alter or break up a high speed flow of fluid containing abrasive particles over the textured surface. The grooves are contacted by the high speed flow of fluid containing the abrasive particles and alter or break up the flow of fluid and abrasive particles and thereby reduce surface wear rate or erosion of the structure leading edge.
Abstract translation: 结构的表面区域被制造成具有纹理表面，其减小由表面积上含有磨料颗粒的流体的高速流动引起的表面磨损率或侵蚀。 更具体地，制造具有由多个凹槽组成的前缘表面，例如转子前缘表面，飞行器翼型件前缘表面，螺旋桨前缘表面等，其纹理表面改变或破坏高速 在磨砂表面上含有磨料颗粒的流体流。 凹槽通过含有磨料颗粒的流体的高速流动而接触，并改变或分解流体和磨料颗粒的流动，从而降低结构前缘的表面磨损率或腐蚀。
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4.发明申请
公开(公告)号：US20250011008A1
公开(公告)日：2025-01-09
申请号：US18346299
申请日：2023-07-03
Applicant: THE BOEING COMPANY
Inventor： Antonio Paesano
IPC: B64F5/40
Abstract: A system and a method for removing a first component from a second component of an assembly include retaining cooling agent within a first retaining chamber of a first container; disposing at least a portion of the assembly within the first retaining chamber so that the first component is covered by the cooling agent within the first retaining chamber; coupling a refrigerant line to a second retaining chamber of a second container; fluidly connecting the first retaining chamber to the second retaining chamber by a conduit; removing the at least a portion of the assembly from the first retaining chamber after a predetermined period of time when the first component is readily removable from the second component; draining the cooling agent into the second retaining chamber via the conduit after said removing the at least a portion of the assembly from the first retaining chamber; and cooling fluid circulating through the refrigerant line with the cooling agent.
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公开(公告)号：US10081140B2
公开(公告)日：2018-09-25
申请号：US14526706
申请日：2014-10-29
Applicant: The Boeing Company
Inventor： Antonio Paesano , Steven Cullison
CPC classification number: B29C70/541 , B29C70/54 , B29L2031/3076
Abstract: A forming apparatus and method of using the apparatus with a concave mandrel to form composite materials is presented where the apparatus has a forming head with an outer surface having a contour that matches the interior surface of the concave cavity of a matching mandrel. A handle and a grip surface to allow an operator to use the forming apparatus to exert a compaction force to successive plies of prepreg to conform the laminate of plies to the interior surface of the concave cavity. Each ply is heated before contact with the forming head of the apparatus.
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公开(公告)号：US20180085883A1
公开(公告)日：2018-03-29
申请号：US15280133
申请日：2016-09-29
Applicant: The Boeing Company
Inventor： Bernard L. DiAntonio , Antonio Paesano
CPC classification number: B24B23/005 , B23P6/002 , B23Q11/0042 , B24B19/14 , B24B23/028 , B24B23/08 , B24B41/06 , B24B55/00 , B24B57/00
Abstract: A portable booth assembly for receiving a work piece to facilitate working on a work area of the work piece including a housing and an inner core disposed within an interior area of the housing is provided. The portable booth assembly includes an aperture that is formed in the housing and the inner core. The aperture is configured to receive the work piece. The inner core defining the aperture is configured to be supported by the work piece if the work piece is large, or support the work piece if the work piece is small, and isolate the work area within the portable booth assembly. The portable booth assembly further includes a cut out formed in the housing. The cut out is configured to enable access to the work area for working on the work area.
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公开(公告)号：US20160319668A1
公开(公告)日：2016-11-03
申请号：US14698334
申请日：2015-04-28
Applicant: The Boeing Company
Inventor： Antonio Paesano , Robert B. Thompson
CPC classification number: F01D5/141 , B63B1/06 , B63B1/36 , B63H25/38 , B64C3/26 , B64C2230/22 , F05D2220/323 , F05D2220/36 , F05D2240/30 , F05D2250/63 , F15D1/005 , Y02T70/121
Abstract: A surface area of a structure is fabricated with a textured surface that reduces the surface wear rate or erosion caused by a high speed flow of fluid containing abrasive particles over the surface area. More particularly, a leading edge surface such as a rotor leading edge surface, an aircraft airfoil leading edge surface, a propeller leading edge surface, etc. is fabricated with a textured surface comprised of a plurality of grooves that alter or break up a high speed flow of fluid containing abrasive particles over the textured surface. The grooves are contacted by the high speed flow of fluid containing the abrasive particles and alter or break up the flow of fluid and abrasive particles and thereby reduce surface wear rate or erosion of the structure leading edge.
Abstract translation: 结构的表面区域被制造成具有纹理表面，其减小由表面积上含有磨料颗粒的流体的高速流动引起的表面磨损率或侵蚀。 更具体地，制造具有由多个凹槽组成的前缘表面，例如转子前缘表面，飞行器翼型件前缘表面，螺旋桨前缘表面等，其纹理表面改变或破坏高速 在磨砂表面上含有磨料颗粒的流体流。 凹槽通过含有磨料颗粒的流体的高速流动而接触，并改变或分解流体和磨料颗粒的流动，从而降低结构前缘的表面磨损率或腐蚀。
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公开(公告)号：US20240376939A1
公开(公告)日：2024-11-14
申请号：US18313424
申请日：2023-05-08
Applicant: THE BOEING COMPANY
Inventor： Antonio Paesano , Douglas R. Ludin , Howard Rolleston
Abstract: A covering system and method for a pitch link of a helicopter include a boot having a bellows, and a cap removably secured to the boot. The boot and the cap are configured to cover at least a portion of the pitch link. The cap is removable from the boot to provide access to the pitch link.
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公开(公告)号：US20160121553A1
公开(公告)日：2016-05-05
申请号：US14526706
申请日：2014-10-29
Applicant: The Boeing Company
Inventor： Antonio Paesano , Steven Cullison
IPC: B29C70/02
CPC classification number: B29C70/541 , B29C70/54 , B29L2031/3076
Abstract: A forming apparatus and method of using the apparatus with a concave mandrel to form composite materials is presented where the apparatus has a forming head with an outer surface having a contour that matches the interior surface of the concave cavity of a matching mandrel. A handle and a grip surface to allow an operator to use the forming apparatus to exert a compaction force to successive plies of prepreg to conform the laminate of plies to the interior surface of the concave cavity. Each ply is heated before contact with the forming head of the apparatus.
Abstract translation: 提出了一种使用具有凹心轴来形成复合材料的装置的成形装置和方法，其中装置具有成形头，其外表面具有与匹配心轴的凹腔的内表面相匹配的轮廓。 手柄和抓握表面，以允许操作者使用成形装置对连续的预浸料层施加压实力，以使层压体层合到凹腔的内表面。 每个层在与设备的成形头接触之前被加热。
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10.发明授权
公开(公告)号：US09182227B1
公开(公告)日：2015-11-10
申请号：US13893091
申请日：2013-05-13
Applicant: The Boeing Company
Inventor： Antonio Paesano , Francis Kendra , Frank J. Gill
CPC classification number: G01C9/005 , B64C27/008
Abstract: Methods and apparatus to measure an angular position of craft components are disclosed. An example apparatus includes an opening to receive a component along a first plane, and a first magnetic coupler positioned along a first exterior side of the apparatus to removably couple an inclinometer to the apparatus at a first angle relative to the first plane.
Abstract translation: 公开了测量工艺部件的角位置的方法和装置。 示例性装置包括沿着第一平面接纳部件的开口和沿着装置的第一外侧定位的第一磁耦合器，以相对于第一平面以第一角度可移除地将倾斜计耦合到装置。
