Title:
THERMAL INSULATION SYSTEM WITH STAGNANT FUEL
Document Type and Number:
Japanese Patent JP2013044433
Kind Code:
A
Abstract:
To provide a fluid line thermal insulation system for an aircraft having a structure configured to be placed around a fluid line in a fuel tank of the aircraft that is configured to hold fuel.
There are provided a method and an apparatus comprising a structure 220. The structure 220 is configured to be placed around a fluid line 224 in a container 204 holding fluid. The structure 220 is further configured to reduce a flow of fluid 214 within a volume of the structure such that the fluid 214 within the volume insulates the fluid line 224.
Inventors:
HOLBROOK MICHAEL LYLE
GAW KEVIN O'BRIEN
WAUGH GREGORY M
CLEMENTS RONALD LAWRENCE
GAW KEVIN O'BRIEN
WAUGH GREGORY M
CLEMENTS RONALD LAWRENCE
Application Number:
JP2012185297A
Publication Date:
March 04, 2013
Filing Date:
August 24, 2012
Export Citation:
Assignee:
BOEING CO
International Classes:
B64C13/40; F16L59/147
Domestic Patent References:
| JPS5965694A | 1984-04-13 | |||
| JPS53117813A | 1978-10-14 | |||
| JP2002295788A | 2002-10-09 | |||
| JP2008545567A | 2008-12-18 |
Foreign References:
| US2676773A | 1954-04-27 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori