Title:
HEATING SYSTEM AND METHOD FOR AN AIRCRAFT WATER CIRCUIT
Document Type and Number:
WIPO Patent Application WO/2023/099255
Kind Code:
A1
Abstract:
The invention relates to a heating system (S) for a water circuit (2) of an aircraft (1), the water circuit (2) defining, on the inside, an inside environment (M1) in which water can circulate and, on the outside, an outside environment (M2), the heating system (S) comprising at least one heating member (3), at least one inside temperature sensor (42), at least one humidity sensor (41) and at least one computer (5) that is configured to activate the heating member if the inside temperature (T1) is below a predetermined temperature threshold (TS), calculate a dew point (TR) based on the humidity parameter (H1) and the inside temperature (T1), and deactivate the heating member if the inside temperature (T1) is higher than the dew point (TR).
Inventors:
PERHERIN DANIEL (FR)
Application Number:
PCT/EP2022/082564
Publication Date:
June 08, 2023
Filing Date:
November 21, 2022
Export Citation:
Assignee:
AIRBUS ATLANTIC (FR)
International Classes:
B64D11/02; B64D11/04
Foreign References:
| JP2010065508A | 2010-03-25 | |||
| EP3070995A1 | 2016-09-21 |
Attorney, Agent or Firm:
ARGYMA (FR)
Download PDF:
Previous Patent: RESIN PARTICLE DISPERSION FOR INKJET PRINTING
Next Patent: METHOD FOR TRANSPORTING A PRODUCT ITEM TO AN ACCESS STATION
Next Patent: METHOD FOR TRANSPORTING A PRODUCT ITEM TO AN ACCESS STATION