公开(公告)号：US09302434B2

公开(公告)日：2016-04-05

申请号：US14095531

申请日：2013-12-03

Applicant: The Boeing Company

Inventor： James Scott Griffing

IPC: B29C45/02 ,  B29C70/50 ,  B29C45/04 ,  B29K105/12

CPC classification number: B29C70/50 ,  B29C45/02 ,  B29C45/0408 ,  B29C70/081 ,  B29C70/12 ,  B29C70/46 ,  B29K2105/12 ,  Y10T428/24132 ,  Y10T428/31504 ,  Y10T428/31533 ,  Y10T428/31721

Abstract: A compression molded composite structure includes an elongated thermoplastic composite part having integral thermoplastic composite fittings.

Abstract translation: 压缩成型的复合结构包括具有整体的热塑性复合配件的细长的热塑复合部件。

公开(公告)号：US20150151467A1

公开(公告)日：2015-06-04

申请号：US14095531

申请日：2013-12-03

Applicant: The Boeing Company

Inventor： James Scott Griffing

IPC: B29C45/02

CPC classification number: B29C70/50 ,  B29C45/02 ,  B29C45/0408 ,  B29C70/081 ,  B29C70/12 ,  B29C70/46 ,  B29K2105/12 ,  Y10T428/24132 ,  Y10T428/31504 ,  Y10T428/31533 ,  Y10T428/31721

Abstract: A compression molded composite structure includes an elongated thermoplastic composite part having integral thermoplastic composite fittings.

Abstract translation: 压缩成型的复合结构包括具有整体的热塑性复合配件的细长的热塑复合部件。

公开(公告)号：US10899428B2

公开(公告)日：2021-01-26

申请号：US16674727

申请日：2019-11-05

Applicant: The Boeing Company

Inventor： David E. Sterling ,  James Scott Griffing ,  Thomas Seth Perkins ,  Hannah Katherine Beck ,  Adam Robert Weston ,  Sara Lynn Walter

IPC: B64C1/18 ,  B64F5/10 ,  B64C1/00

Abstract: A method of installing a decompression panel assembly in an aircraft. The decompression panel assembly includes a body portion, a baffle member, and a panel member. The method includes coupling the body portion to the panel member, wherein the body portion includes a plurality of frame members defining a plurality of openings in the body portion. The method also includes coupling the baffle member to the plurality of frame members such that the baffle member removably obstructs at least one opening of the plurality of openings. The baffle member is integrally formed with the plurality of frame members and is configured for at least partial displacement from the at least one opening during a decompression event. The decompression panel assembly is then coupled between a sidewall and a floor panel of the aircraft.

公开(公告)号：US20200062372A1

公开(公告)日：2020-02-27

申请号：US16674727

申请日：2019-11-05

Applicant: The Boeing Company

Inventor： David E. Sterling ,  James Scott Griffing ,  Thomas Seth Perkins ,  Hannah Katherine Beck ,  Adam Robert Weston ,  Sara Lynn Walter

IPC: B64C1/18 ,  B64F5/10

Abstract: A method of installing a decompression panel assembly in an aircraft. The decompression panel assembly includes a body portion, a baffle member, and a panel member. The method includes coupling the body portion to the panel member, wherein the body portion includes a plurality of frame members defining a plurality of openings in the body portion. The method also includes coupling the baffle member to the plurality of frame members such that the baffle member removably obstructs at least one opening of the plurality of openings. The baffle member is integrally formed with the plurality of frame members and is configured for at least partial displacement from the at least one opening during a decompression event. The decompression panel assembly is then coupled between a sidewall and a floor panel of the aircraft.

公开(公告)号：US20170283029A1

公开(公告)日：2017-10-05

申请号：US15085411

申请日：2016-03-30

Applicant: The Boeing Company

Inventor： David E. Sterling ,  James Scott Griffing ,  Thomas Seth Perkins ,  Hannah Katherine Beck ,  Adam Robert Weston ,  Sara Lynn Walter

IPC: B64C1/14 ,  B64F5/00 ,  B64C1/18

CPC classification number: B64C1/18 ,  B64C2001/009 ,  B64F5/10

Abstract: A decompression panel assembly for use in an aircraft includes a body portion comprising a plurality of frame members defining a plurality of openings in the body portion. The decompression panel assembly also includes a baffle member integrally formed with the plurality of frame members such that the baffle member removably obstructs at least one opening of the plurality of openings. The baffle member is configured for at least partial displacement from the at least one opening during a decompression event.