SU1037575A1 - Air supply system - Google Patents

Air supply system

Info

Publication number
SU1037575A1
SU1037575A1 SU3399818/23A SU3399818A SU1037575A1 SU 1037575 A1 SU1037575 A1 SU 1037575A1 SU 3399818/23 A SU3399818/23 A SU 3399818/23A SU 3399818 A SU3399818 A SU 3399818A SU 1037575 A1 SU1037575 A1 SU 1037575A1
Authority
SU
USSR - Soviet Union
Prior art keywords
air
aircraft
icing device
air supply
structural elements
Prior art date
Application number
SU3399818/23A
Other languages
Russian (ru)
Inventor
В.А. Привалихин
Ю.Н. Щербаков
Я.М. Ицкович
В.Л. Рубан
А.В. Щербаков
Original Assignee
В.А. Привалихин
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.А. Привалихин filed Critical В.А. Привалихин
Priority to SU3399818/23A priority Critical patent/SU1037575A1/en
Application granted granted Critical
Publication of SU1037575A1 publication Critical patent/SU1037575A1/en

Links

Landscapes

  • Central Air Conditioning (AREA)

Abstract

Система подачи воздуха, содержащая два воздухо-воздушных теплообменника, приводную заслонку и регуляторы температуры в магистралях кондиционируемого воздуха и воздуха, подаваемого в устройство защиты от обледенения элементов конструкции самолета, снабженное включателем, отличающаяся тем, что, с целью повышения надежности и уменьшения веса путем упрощения системы и увеличения перепада температур на теплообменниках, в систему введены логические элементы "НЕ" и "И", в которых первые входы подключены к выходам регуляторов температуры в магистралях, соответственно, кондиционируемого воздуха и воздуха, подаваемого в устройство защиты от обледенения элементов конструкции самолета, выходы - к приводу заслонки, а вторые входы - к выключателю устройства защиты от обледенения элементов конструкции самолета, причем теплообменник в магистрали кондиционируемого воздуха входом тракта охлаждающего воздуха сообщен с выходом заслонки, а выходом - со входом тракта охлаждающего воздуха теплообменника в магистрали подачи воздуха в устройство защиты от обледенения элементов конструкции самолета.An air supply system containing two air-to-air heat exchangers, an air damper and temperature regulators in the airways of the conditioned air and air supplied to the anti-icing device for the aircraft’s structural components, equipped with a switch, characterized in system and increase the temperature difference on the heat exchangers, the system introduced the logical elements "NOT" and "I", in which the first inputs are connected to the outputs of the temperature regulators in the ma Gistral, respectively, conditioned air and air supplied to the anti-icing device of the aircraft’s structural elements, outlets to the damper actuator, and the second inputs to the switch of the anti-icing device of the aircraft’s structural elements; with the outlet of the valve, and the outlet with the inlet of the path of the cooling air of the heat exchanger in the air supply line to the anti-icing device of the structural elements and aircraft.

SU3399818/23A 1982-02-19 1982-02-19 Air supply system SU1037575A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3399818/23A SU1037575A1 (en) 1982-02-19 1982-02-19 Air supply system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3399818/23A SU1037575A1 (en) 1982-02-19 1982-02-19 Air supply system

Publications (1)

Publication Number Publication Date
SU1037575A1 true SU1037575A1 (en) 2006-05-20

Family

ID=60526280

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3399818/23A SU1037575A1 (en) 1982-02-19 1982-02-19 Air supply system

Country Status (1)

Country Link
SU (1) SU1037575A1 (en)

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