Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8522529
APP PUB NO 20090025366A1
SERIAL NO

11996019

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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An aircraft propulsion unit including a turbojet and a heat exchanger located above the turbojet and drawing a cooling air stream and a hot air stream in the turbojet. Wherein the cooling air intake and hot air intake surfaces in the housing are directed forward of the turbojet and have normal lines inclined relative to the axis of the turbojet. The embodiment also concerns an aircraft equipped with at least one such propulsion unit.

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First Claim

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Patent Owner(s)

  • AIRBUS OPERATIONS SAS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Marche, Herve Roquettes, FR 19 242
Martinou, Jean-Marc L'Union, FR 6 122

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