Aircraft including plane equipment heating with a thermodynamic loop having a closed circuit in which heat transfer liquid circulates and the closed circuit loop including an evaporator
First Claim
1. An aircraft comprising:
- aircraft skin;
a first piece of aeronautic equipment, the first piece of aeronautic equipment comprising a part arranged at the aircraft skin and an appendage; and
a second piece of aeronautic equipment spaced apart from the first piece of aeronautic equipment, the second piece of aeronautic equipment generating heat during operation,wherein the part of the first piece of aeronautic equipment comprises a thermodynamic loop comprising a closed circuit in which a heat transfer fluid circulates, the closed circuit in which the heat transfer fluid circulates being a tubular channel with an empty section,wherein the closed circuit comprises an evaporator connected to a condenser by the tubular channel,wherein the evaporator is located spaced apart from the second piece of aeronautic equipment generating heat so that the heat given off from the second piece of aeronautic equipment heats the evaporator and the heat transfer fluid in the evaporator, the second piece of aeronautic equipment thereby generating heat that is a heat source to the evaporator, andwherein the condenser is located in the appendage so that a condensation of the heat transfer fluid can occur in the appendage to heat the appendage during the operation of the second piece of aeronautic equipment.
1 Assignment
0 Petitions
Accused Products
Abstract
An aircraft provided with at least one piece of aeronautic equipment, the equipment (25) including a part intended to be arranged at a skin (27) of the aircraft and elements for heating the part, characterized in that the heating elements include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including an evaporator (14) associated with functional elements (70) of the aircraft forming a heat source giving off heat during their operation and a zone in which a condensation of the heat transfer fluid can occur in the appendage to heat it, and in that outside the evaporator, the circuit in which the fluid circulates is formed by a tubular channel with an empty section.
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Citations
15 Claims
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1. An aircraft comprising:
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aircraft skin; a first piece of aeronautic equipment, the first piece of aeronautic equipment comprising a part arranged at the aircraft skin and an appendage; and a second piece of aeronautic equipment spaced apart from the first piece of aeronautic equipment, the second piece of aeronautic equipment generating heat during operation, wherein the part of the first piece of aeronautic equipment comprises a thermodynamic loop comprising a closed circuit in which a heat transfer fluid circulates, the closed circuit in which the heat transfer fluid circulates being a tubular channel with an empty section, wherein the closed circuit comprises an evaporator connected to a condenser by the tubular channel, wherein the evaporator is located spaced apart from the second piece of aeronautic equipment generating heat so that the heat given off from the second piece of aeronautic equipment heats the evaporator and the heat transfer fluid in the evaporator, the second piece of aeronautic equipment thereby generating heat that is a heat source to the evaporator, and wherein the condenser is located in the appendage so that a condensation of the heat transfer fluid can occur in the appendage to heat the appendage during the operation of the second piece of aeronautic equipment. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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Specification