Patent · US Active

Aircraft vapour trail control system

US10371003B2 · kind B2 · utility

8Cited by
4References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 24, 2016
Grant dateAug 6, 2019
Priority date
Expiry dateJul 31, 2037

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

The invention concerns an aircraft propulsion system having an engine core within which fuel is combusted to produce an exhaust containing water produced from the combustion of fuel, at least one propulsive fan for generating a mass flow of air which mixes with the exhaust of the engine core, and one or more sensor arranged to sense a condition indicative of vapor trail formation by the exhaust flow from the engine; and a controller arranged to control the ratio of the mass flow of water in the exhaust to the mass flow of air propulsed by the propulsive fan such that the ratio is reduced upon sensing of said condition by the one or more sensor.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.