[go: up one dir, main page]

SU856154A1 - Air conditioning system on the aircraft - Google Patents

Air conditioning system on the aircraft

Info

Publication number
SU856154A1
SU856154A1 SU2915713/23A SU2915713A SU856154A1 SU 856154 A1 SU856154 A1 SU 856154A1 SU 2915713/23 A SU2915713/23 A SU 2915713/23A SU 2915713 A SU2915713 A SU 2915713A SU 856154 A1 SU856154 A1 SU 856154A1
Authority
SU
USSR - Soviet Union
Prior art keywords
turbo
heat exchanger
compressor
line
conditioning system
Prior art date
Application number
SU2915713/23A
Other languages
Russian (ru)
Inventor
А.А. Абрамян
Г.И. Зубова
В.Н. Пронин
Н.И. Рудченко
Original Assignee
А.А. Абрамян
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by А.А. Абрамян filed Critical А.А. Абрамян
Priority to SU2915713/23A priority Critical patent/SU856154A1/en
Application granted granted Critical
Publication of SU856154A1 publication Critical patent/SU856154A1/en

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

1. Система кондиционирования воздуха на летательном аппарате, содержащая теплообменник, включенный в линию продувочного воздуха и в замкнутый через гермоотсек контур, в котором установлены также турбохолодильник и компрессор, имеющий приводную турбину, установленную в линии питания, сообщенной с источником сжатого воздуха, отличающаяся тем, что, с целью повышения холодопроизводительности, линия продувочного воздуха оборудована обратным клапаном, который установлен перед теплообменником, а линия питания на ее участке за приводной турбиной компрессора соединена с линией продувочного воздуха на ее участке между обратным клапаном и теплообменником.2. Система по п.1, отличающаяся тем, что, с целью повышения надежности работы при переохлаждении воздуха за приводной турбиной компрессора, система оборудована влагоотделителем, установленным в замкнутом контуре на его участке между турбохолодильником и гермоотсеком.1. An air conditioning system on an aircraft containing a heat exchanger included in the purge air line and in a loop closed through the pressurized compartments, in which a turbo-cooler and a compressor are also installed, having a drive turbine installed in the supply line communicated with a source of compressed air, that, in order to increase the cooling capacity, the purge air line is equipped with a check valve, which is installed in front of the heat exchanger, and the power line at its site behind the drive turbo another compressor is connected to the purge air line in its section between the check valve and the heat exchanger. The system according to claim 1, characterized in that, in order to increase the reliability of operation when air is supercooling behind the drive turbine of the compressor, the system is equipped with a moisture separator installed in a closed loop on its section between the turbo-cooler and the pressurized compartment.

SU2915713/23A 1980-04-25 1980-04-25 Air conditioning system on the aircraft SU856154A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2915713/23A SU856154A1 (en) 1980-04-25 1980-04-25 Air conditioning system on the aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2915713/23A SU856154A1 (en) 1980-04-25 1980-04-25 Air conditioning system on the aircraft

Publications (1)

Publication Number Publication Date
SU856154A1 true SU856154A1 (en) 2006-03-10

Family

ID=60525119

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2915713/23A SU856154A1 (en) 1980-04-25 1980-04-25 Air conditioning system on the aircraft

Country Status (1)

Country Link
SU (1) SU856154A1 (en)

Similar Documents

Publication Publication Date Title
ES8507252A1 (en) High efficiency air cycle air conditioning system
US4996845A (en) Cooling, heating and power generating device using automobile waste heat
ES461529A1 (en) Multi:stage compressor and turbine installation - has heat accumulator with liquid storage medium through which air passes to air accumulator
US4283924A (en) Climatizing of aircraft
ES461991A1 (en) Heat recovery system
EP0119024A3 (en) Refrigerator cooling and freezing system
GB1016710A (en) Improvements in a method and means for obtaining dry gas or air
US3400555A (en) Refrigeration system employing heat actuated compressor
ES484947A1 (en) Power generation-refrigeration system and method of operating the same.
SU856154A1 (en) Air conditioning system on the aircraft
JPS52104644A (en) Vane type gas prime mover
JPS54100551A (en) Refrigerator
JPS5737100A (en) Ship's air conditioner
SU575908A1 (en) COOLING AND HEATING SYSTEM OF THE OBJECT
SU629415A1 (en) Air refrigerating plant
FR2363064A1 (en) Air conditioner using heat exchangers - passes preset quantities of air from premises and outside through both heat exchangers
SU799584A1 (en) INSTALLATION FOR PROVISION OF THE OBJECT WITH HEAT AND COLD
JPS5475648A (en) Air conditioner
JPS5755213A (en) Air conditioner
SU1119264A1 (en) AIR CONDITIONING SYSTEM ON AIRCRAFT
SU832241A1 (en) Method of trasporting natural gas in main pipeline
SU819524A1 (en) Air refrigerating equipment
SU475017A1 (en) AIR COOLING SYSTEM
SU1195151A1 (en) Air turbo-refrigerating plant
JPS6470669A (en) Air conditioner