公开(公告)号：US11919647B2

公开(公告)日：2024-03-05

申请号：US16875704

申请日：2020-05-15

Applicant: The Boeing Company

Inventor： Andrew David Clark ,  Thamir Rauf Al-Alusi ,  David William Kirkbride ,  Frederick T. Calkins ,  Bradley J. Mitchell

IPC: B64D13/02 ,  B60T5/00 ,  B64C25/00 ,  B64C25/42 ,  F16D65/78

CPC classification number: B64D13/02 ,  B60T5/00 ,  B64C25/001 ,  B64C25/42 ,  F16D65/78

Abstract: Thermal control system for aircraft main landing gear wheel wells and related methods are disclosed. An example thermal control system includes a conduit defining a fluid passageway between an inlet and an outlet. The inlet of the conduit positioned in fluid communication with a landing gear wheel well and the outlet of the conduit positioned in fluid communication with the atmosphere. The conduit generates a pressure differential through the fluid passageway between the inlet and the outlet to exhaust heat from the landing gear wheel well to the atmosphere.

公开(公告)号：US20210354831A1

公开(公告)日：2021-11-18

申请号：US16875704

申请日：2020-05-15

Applicant: The Boeing Company

Inventor： Andrew David Clark ,  Thamir Rauf Al-Alusi ,  David William Kirkbride ,  Frederick T. Calkins ,  Bradley J. Mitchell

IPC: B64D13/02

Abstract: Thermal control system for aircraft main landing gear wheel wells and related methods are disclosed. An example thermal control system includes a conduit defining a fluid passageway between an inlet and an outlet. The inlet of the conduit positioned in fluid communication with a landing gear wheel well and the outlet of the conduit positioned in fluid communication with the atmosphere. The conduit generates a pressure differential through the fluid passageway between the inlet and the outlet to exhaust heat from the landing gear wheel well to the atmosphere.