US 2025/0019085 A1 · Primary Component For An Aircraft With Integrated Thermal Management

Abstract

A primary component (100) for an aircraft (10) comprises a first surface (102) and a second surface (104) arranged opposite the first surface (102) as well as a heat exchanger (200). The heat exchanger (200) comprises a heat exchanger body (201) and a plurality of ports (212, 214, 222, 224). The heat exchanger (200) defines a first fluid circuit (210) and a second fluid circuit (220), wherein each fluid circuit is fluidically connected to two ports, respectively, and the first fluid circuit (210) is fluidically separated from the second fluid circuit (220). The heat exchanger body (201) is embedded in the primary component (100) in such a way that the heat exchanger body (201) is arranged between the first surface (102) and the second surface (104) of the primary component (100), and each of the plurality of ports (212, 214, 222, 224) is fluidically accessible either via the first surface (102) or via the second surface (104).

Claims13

Dependent claims

A primary component (100) for an aircraft (10), the primary component (100) comprising:

a first surface (102);
a second surface (104) arranged opposite the first surface (102);
a heat exchanger (200) with a heat exchanger body (201) and a plurality of ports (212, 214, 222, 224);
wherein the heat exchanger (200) defines a first fluid circuit (210) and a second fluid circuit (220), wherein the first fluid circuit (210) and the second fluid circuit (220) is fluidically connected to two ports, respectively, and the first fluid circuit (210) is fluidically separated from the second fluid circuit (220);
wherein the heat exchanger body (201) is embedded into the primary component (100) in such a way that the heat exchanger body (201) is arranged between the first surface (102) and the second surface (104) of the primary component (100), and each of the plurality of ports (212, 214, 222, 224) is fluidly accessible via the first surface (102) or via the second surface (104).

2 more elements

Dependencies are inferred from the claim text.

Primary Component For An Aircraft With Integrated Thermal Management

Life of this patent

Primary Component For An Aircraft With Integrated Thermal Management

Life of this patent

Abstract

Claims13