SU325891A2 - DEVICE FOR PROTECTION OF TURBO-REACTIVE ENGINES AGAINST SUCTION OF EXTERNAL OBJECTS WHEN TAKING AND ADMISSION OF A PLANE - Google Patents

DEVICE FOR PROTECTION OF TURBO-REACTIVE ENGINES AGAINST SUCTION OF EXTERNAL OBJECTS WHEN TAKING AND ADMISSION OF A PLANE

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Publication number
SU325891A2
SU325891A2 SU1463789/23A SU1463789A SU325891A2 SU 325891 A2 SU325891 A2 SU 325891A2 SU 1463789/23 A SU1463789/23 A SU 1463789/23A SU 1463789 A SU1463789 A SU 1463789A SU 325891 A2 SU325891 A2 SU 325891A2
Authority
SU
USSR - Soviet Union
Prior art keywords
protection
turbo
admission
taking
plane
Prior art date
Application number
SU1463789/23A
Other languages
Russian (ru)
Inventor
Ю.Н. Волков
М.А. Зимин
К.Н. Матвеев
Н.И. Раков
В.Н. Шевырев
Original Assignee
Ю.Н. Волков
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 Ю.Н. Волков filed Critical Ю.Н. Волков
Priority to SU1463789/23A priority Critical patent/SU325891A2/en
Application granted granted Critical
Publication of SU325891A2 publication Critical patent/SU325891A2/en

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Abstract

Устройство для защиты турбореактивных двигателей от засасывания посторонних предметов при взлете и посадке самолета по авт. св. № 229974, отличающееся тем, что, с целью предохранения штанги от воздействия высоких температур путем уменьшения температуры газов за камерой сгорания и повышения эффективности защитной завесы за счет увеличения расхода газов, в нем в корневой части штанги за камерой сгорания смонтирован эжектор подсоса наружного воздуха.A device for protection of turbojet engines from the suction of foreign objects during takeoff and landing of an aircraft by bus. St. No. 229974, characterized in that, in order to protect the rod from high temperatures by reducing the temperature of the gases behind the combustion chamber and increasing the effectiveness of the protective curtain by increasing the flow rate of gases, an ejector of external air suction is mounted in the root of the rod behind the combustion chamber.

SU1463789/23A 1970-08-03 1970-08-03 DEVICE FOR PROTECTION OF TURBO-REACTIVE ENGINES AGAINST SUCTION OF EXTERNAL OBJECTS WHEN TAKING AND ADMISSION OF A PLANE SU325891A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1463789/23A SU325891A2 (en) 1970-08-03 1970-08-03 DEVICE FOR PROTECTION OF TURBO-REACTIVE ENGINES AGAINST SUCTION OF EXTERNAL OBJECTS WHEN TAKING AND ADMISSION OF A PLANE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1463789/23A SU325891A2 (en) 1970-08-03 1970-08-03 DEVICE FOR PROTECTION OF TURBO-REACTIVE ENGINES AGAINST SUCTION OF EXTERNAL OBJECTS WHEN TAKING AND ADMISSION OF A PLANE

Publications (1)

Publication Number Publication Date
SU325891A2 true SU325891A2 (en) 2005-03-20

Family

ID=60514556

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1463789/23A SU325891A2 (en) 1970-08-03 1970-08-03 DEVICE FOR PROTECTION OF TURBO-REACTIVE ENGINES AGAINST SUCTION OF EXTERNAL OBJECTS WHEN TAKING AND ADMISSION OF A PLANE

Country Status (1)

Country Link
SU (1) SU325891A2 (en)

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