Self-supporting vapor cycle refrigeration system for an aircraft
A vapor cycle refrigeration system for an aircraft comprises a compressor, a condenser unit with a condenser radiator, a condenser fan and a condenser air duct configured to direct a stream of air generated by the condenser fan through the condenser radiator, an expansion device, an evaporator unit with an evaporator radiator, an evaporator fan and an evaporator air duct configured to direct a stream of air generated by the evaporator fan through the evaporator radiator, and a piping system connecting the compressor, the condenser radiator, the expansion device and the evaporator radiator in a closed circuit for a refrigerant, wherein each of the compressor, the condenser radiator, the condenser fan, the expansion device, the evaporator radiator, the evaporator fan and the piping system is fully supported directly or indirectly by at least one of the condenser air duct and the evaporator air duct such that the system is self-supporting.
1. A vapor cycle refrigeration system for an aircraft, the system comprising:
a compressor,
a condenser unit with a condenser radiator, a condenser fan and a condenser air duct configured to direct a stream of air generated by the condenser fan through the condenser radiator,
an expansion device,
an evaporator unit with an evaporator radiator, an evaporator fan and an evaporator air duct configured to direct a stream of air generated by the evaporator fan through the evaporator radiator, and
a piping system connecting the compressor, the condenser radiator, the expansion device and the evaporator radiator in a closed circuit for a refrigerant,
wherein each of the compressor, the condenser radiator, the condenser fan, the expansion device, the evaporator radiator, the evaporator fan and the piping system is fully supported directly or indirectly by at least one of the condenser air duct and the evaporator air duct in such a manner that the system is self-supporting.
2. The vapor cycle refrigeration system according to claim 1 , wherein each of the compressor, the condenser radiator, the condenser fan, the expansion device, the evaporator radiator and the evaporator fan is fully supported either by the condenser air duct or by the evaporator air duct so that the system is separable into two self-supporting modules.
3. The vapor cycle refrigeration system according to claim 1 , furthermore comprising a controller mounted to and fully supported on an outside surface of the condenser air duct or on an outside surface of the evaporator air duct.
4. The vapor cycle refrigeration system according to claim 3 , wherein a heat sink structure of the controller protrudes into the interior of the air duct on which the controller is supported, in particular into the interior of the condenser air duct.
5. The vapor cycle refrigeration system according to claim 1 , wherein the condenser air duct and/or the evaporator air duct comprise an arrangement of mounting protrusions for mounting other components of the system, the mounting protrusions preferably being formed in one piece with the corresponding air duct.
6. The vapor cycle refrigeration system according to claim 1 , wherein the evaporator unit is supported on the condenser air duct by way of a console and/or a strut.
7. The vapor cycle refrigeration system according to claim 1 , wherein the condenser air duct and/or the evaporator air duct are made from a fiber composite material.
8. The vapor cycle refrigeration system according to claim 1 , wherein the evaporator air duct comprises two separate air inlets and a mixing chamber upstream from the evaporator radiator.
9. The vapor cycle refrigeration system according to claim 1 , wherein the compressor is supported on an inclined surface portion of the condenser air duct and is arranged between the condenser unit and the evaporator unit.
10. An air craft comprising a vapor cycle refrigeration system according to claim 1 , wherein the vapor cycle refrigeration system is fixed to the air craft in such a manner that all components of the vapor cycle refrigeration system are supported on the aircraft via at least one of the condenser air duct and the evaporator air duct.