SU1412193A1 - AIR-HEATED ANTI-FRONT SYSTEM OF AIRCRAFT - Google Patents
AIR-HEATED ANTI-FRONT SYSTEM OF AIRCRAFTInfo
- Publication number
- SU1412193A1 SU1412193A1 SU4037947/23A SU4037947A SU1412193A1 SU 1412193 A1 SU1412193 A1 SU 1412193A1 SU 4037947/23 A SU4037947/23 A SU 4037947/23A SU 4037947 A SU4037947 A SU 4037947A SU 1412193 A1 SU1412193 A1 SU 1412193A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- air
- aircraft
- cavity
- source
- inner shell
- Prior art date
Links
Landscapes
- Road Paving Structures (AREA)
Abstract
1. Воздушно-тепловая противообледенительная система летательного аппарата, содержащая источник сжатого воздуха, соединенный трубопроводами подвода воздуха с полостью горячего воздуха, выполненной между обогреваемой обшивкой и внутренней оболочкой, отличающаяся тем, что, с целью повышения экономичности системы, источник сжатого воздуха выполнен в виде компрессора, установленного на валу маршевого двигателя, при этом вход компрессора соединен с холодной полостью, образованной внутренней оболочкой, в которой выполнены отверстия.2. Система по п.1, отличающаяся тем, что в горячей полости установлены продольные перегородки, образующие каналы.1. Air-thermal anti-icing system of the aircraft, containing a source of compressed air connected by pipelines for supplying air with a cavity of hot air, made between heated skin and the inner shell, characterized in that, in order to improve the efficiency of the system, the source of compressed air is designed as a compressor mounted on the main engine shaft, while the compressor inlet is connected to a cold cavity formed by the inner shell in which the holes are made. A system according to claim 1, characterized in that longitudinal partitions forming channels are installed in the hot cavity.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4037947/23A SU1412193A1 (en) | 1986-03-17 | 1986-03-17 | AIR-HEATED ANTI-FRONT SYSTEM OF AIRCRAFT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4037947/23A SU1412193A1 (en) | 1986-03-17 | 1986-03-17 | AIR-HEATED ANTI-FRONT SYSTEM OF AIRCRAFT |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1412193A1 true SU1412193A1 (en) | 2005-02-20 |
Family
ID=60535998
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4037947/23A SU1412193A1 (en) | 1986-03-17 | 1986-03-17 | AIR-HEATED ANTI-FRONT SYSTEM OF AIRCRAFT |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1412193A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2736706C2 (en) * | 2016-05-02 | 2020-11-19 | Зе Боинг Компани | Systems and methods for preventing formation of ice on aircraft parts |
-
1986
- 1986-03-17 SU SU4037947/23A patent/SU1412193A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2736706C2 (en) * | 2016-05-02 | 2020-11-19 | Зе Боинг Компани | Systems and methods for preventing formation of ice on aircraft parts |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SE8803415D0 (en) | GAS TURBINE ENGINE | |
GB1094761A (en) | Conversion of heat to mechanical energy | |
SU1412193A1 (en) | AIR-HEATED ANTI-FRONT SYSTEM OF AIRCRAFT | |
JPS57119117A (en) | Low fuel consumption compound engine | |
ATE21439T1 (en) | GAS DYNAMIC PRESSURE WAVE CHARGER FOR VEHICLE COMBUSTION ENGINES. | |
JPS6430175A (en) | Fuel cell power generating system | |
JPS57167597A (en) | Treatment of evaporated gas in lng carrying ship | |
DE3865650D1 (en) | GAS TURBINE SYSTEM. | |
GB2158883B (en) | Gas turbine engine cooling air supply | |
BR8807763A (en) | INTERNAL COMBUSTION ENGINES | |
GB2053362A (en) | Gas turbine power system with fuel injection and combustion catalyst | |
SU1413258A1 (en) | Internal combustion engine | |
JPS53510A (en) | Automotive air-conditioner unit | |
JPS57122107A (en) | Combined cycle generator | |
ES8504326A1 (en) | Supercharger for heat engine | |
RU92013764A (en) | DIESEL ENGINE WITH HEAT EXCHANGER | |
JPS5696104A (en) | Fuel and steam double engine | |
JPS54133664A (en) | Freezer refrigerator | |
JPS5325750A (en) | Discharged heat recovdry and water producer of internal combustion engine | |
UA9056A1 (en) | Installation for heat takeoff from cooled object | |
SU249946A1 (en) | Aircraft compartment cooling system | |
UA16466A1 (en) | Device for cooling gas-turbine engine bearing | |
SU1658542A1 (en) | POWER INSTALLATION OF AIRCRAFT WITH A DOUBLE-CIRCUIT TURBO-DRIVE ENGINE MOUNTED ON A PILON | |
JPS562424A (en) | Cooling device for rotary piston engine | |
SU1475257A1 (en) | HEATED AIR RECEIVING GAS TURBINE ENGINE |