公开(公告)号：US11953953B2

公开(公告)日：2024-04-09

申请号：US16144165

申请日：2018-09-27

Applicant: The Boeing Company

Inventor： Ramon L. Cuenca ,  Shellini P. Dowell ,  Thomas A. Jessett ,  Fadl I. Khalil ,  Warren S. Ng ,  Scott B. Vacknitz ,  Collis M. Walker ,  Archibald A. Gray ,  James C. Russell ,  Charles O. Adler

IPC: G06F1/18 ,  B64D45/00 ,  G01S5/18 ,  G01S7/02 ,  G01S13/95 ,  H01M10/052 ,  H01M50/202 ,  H01M50/244 ,  H01M50/262 ,  H01M50/375

CPC classification number: G06F1/182 ,  B64D45/00 ,  G01S5/183 ,  G01S13/953 ,  G06F1/188 ,  H01M50/202 ,  H01M50/244 ,  H01M50/262 ,  H01M50/375 ,  B64D2045/0065 ,  G01S7/027 ,  H01M10/052 ,  H01M2220/20

Abstract: An avionics unit assembly for an aircraft can include an avionics unit (e.g., an underwater locator device, “ULD”), and a battery to power the avionics unit. The avionics unit assembly can further include a housing that encases the avionics unit and the battery. The housing includes a vent port for exhausting an emission from the housing during a failure of the avionics unit. The avionics unit assembly can further include one or more of a suppressor that filters the emission, a shield element that is resistant to chemical and/or thermal effects of the emission, and a bracket for mounting the avionics unit to a surface. A method integrating the avionics unit assembly onto a forward aircraft bulkhead at a mount location under an aircraft radome and for manufacturing the avionics unit, and an aircraft including the avionics unit are also described.