SU1037575A1 - Air supply system - Google Patents
Air supply systemInfo
- 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
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.
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) |
-
1982
- 1982-02-19 SU SU3399818/23A patent/SU1037575A1/en active
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