Abstract: A heat exchanger comprises a conduit defining an inlet flow path for a fluid; a heat exchanger matrix disposed to receive a flow from the inlet flow path; and a swirler disposed within the conduit and arranged to improve dispersion of a flow from the inlet flow path over the heat exchanger matrix.
Type:
Grant
Filed:
October 12, 2017
Date of Patent:
January 21, 2020
Assignee:
HS MARSTON AEROSPACE LTD.
Inventors:
Jacob Diffey, John Marsh, James Green, Chris McNab