SU547084A1 - Air conditioning system on the plane - Google Patents

Air conditioning system on the plane

Info

Publication number
SU547084A1
SU547084A1 SU2175067/23A SU2175067A SU547084A1 SU 547084 A1 SU547084 A1 SU 547084A1 SU 2175067/23 A SU2175067/23 A SU 2175067/23A SU 2175067 A SU2175067 A SU 2175067A SU 547084 A1 SU547084 A1 SU 547084A1
Authority
SU
USSR - Soviet Union
Prior art keywords
line
air
purge
cooling
conditioning system
Prior art date
Application number
SU2175067/23A
Other languages
Russian (ru)
Inventor
В.В. Демченко
Ю.И. Катюшин
Л.Я. Климов
Г.В. Комиссаров
В.И. Слотин
Н.А. Ульянов
Е.П. Чуриков
Original Assignee
В.В. Демченко
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 В.В. Демченко filed Critical В.В. Демченко
Priority to SU2175067/23A priority Critical patent/SU547084A1/en
Application granted granted Critical
Publication of SU547084A1 publication Critical patent/SU547084A1/en

Links

Landscapes

  • Central Air Conditioning (AREA)

Abstract

Система кондиционирования воздуха на самолете, содержащая первичный радиатор с линией продувки на встречном потоке и регенератор, установленный на линии сброса охлаждающего воздуха из расположенного за ним теплообменника вентиляции снаряжения и кабины, а также турбохолодильник с обводной линией и исполнительные органы регулятора температуры охлаждаемого воздуха, установленные в линиях продувки и подачи охлаждающего и горячего воздуха, отличающаяся тем, что, с целью повышения экономичности, участок линии охлаждающего воздуха после теплообменника вентиляции снаряжения и места сброса воздуха из кабины выполнен с сужением, формирующим камеру смешения эжектора, сопло которого соединено с входом линии продувки первичного радиатора при помощи трубопровода, оборудованного заслонкой регулятора температуры охлаждаемого воздуха.The air conditioning system on the aircraft, containing a primary radiator with a purge line on the counter-flow and a regenerator installed on the cooling air discharge line from the equipment and cabin ventilation heat exchanger behind it, as well as a turbo-refrigerator with a bypass line and the cooling air regulator control units installed in cooling and hot air purge and supply lines, characterized in that, in order to improve efficiency, the section of the cooling air line after The heat exchanger of the equipment ventilation and the place of air discharge from the cabin is made with a constriction that forms the mixing chamber of the ejector, the nozzle of which is connected to the inlet of the purge line of the primary radiator by means of a pipeline equipped with a gate of the cooled air temperature controller.

SU2175067/23A 1975-09-25 1975-09-25 Air conditioning system on the plane SU547084A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2175067/23A SU547084A1 (en) 1975-09-25 1975-09-25 Air conditioning system on the plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2175067/23A SU547084A1 (en) 1975-09-25 1975-09-25 Air conditioning system on the plane

Publications (1)

Publication Number Publication Date
SU547084A1 true SU547084A1 (en) 2006-01-27

Family

ID=60520675

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2175067/23A SU547084A1 (en) 1975-09-25 1975-09-25 Air conditioning system on the plane

Country Status (1)

Country Link
SU (1) SU547084A1 (en)

Similar Documents

Publication Publication Date Title
GB1011742A (en) Improvements in or relating to an induction type room air conditioning unit
GB1178642A (en) Improvements in Air-Cooled Steam Condensers
SU547084A1 (en) Air conditioning system on the plane
GB1152440A (en) Process and Apparatus For Cooling Air
GB1152439A (en) Process and Apparatus For Cooling Air
ES354264A1 (en) Air temperature regulating device
GB753120A (en) Improvements in or relating to an aircraft air-conditioning system
GB592389A (en) Improvements in or relating to thermal power plants
FR2269644A1 (en) Water cooled I.C. engine with heat exchanger - has thermostatic valve control systems for heating or cooling the combustion air
ES450063A1 (en) Air temperature control system for a room having an outside wall
SU809761A1 (en) Air conditioning system for aircraft
SU690889A1 (en) AIR CONDITIONING SYSTEM
SU565150A1 (en) Combined air heater
GB698407A (en) Improvements in or relating to systems for the supply of conditioned air in aircraft
SU916954A1 (en) Heat exchange apparatus
GB705265A (en) Improvements relating to heat-exchange apparatus
GB721676A (en) Air conditioning means for an enclosure
SU379138A1 (en) Air conditioning system on a supersonic aircraft
SU147279A1 (en) The way to protect the recuperators of industrial furnaces
GB853761A (en) Improvements relating to vehicle ventilating systems
SU731208A1 (en) Air conditioning plant
SU396959A1 (en) Device for controlling the humidity of the air on an aircraft
SU268190A1 (en) VENTILATION VENTILATION SYSTEM
GB780934A (en) Improved air conditioner apparatus
GB1001588A (en) Method and means for air-conditioning