SU268183A1 - DEVICE FOR PROTECTION OF A TURBO-REACTIVE MOTOR OF AN AIRPLANE FROM CONTAMINATION OF OUTSIDE OBJECTS IN THE AIR INTAKE CHANNEL - Google Patents

DEVICE FOR PROTECTION OF A TURBO-REACTIVE MOTOR OF AN AIRPLANE FROM CONTAMINATION OF OUTSIDE OBJECTS IN THE AIR INTAKE CHANNEL

Info

Publication number
SU268183A1
SU268183A1 SU1302522/23A SU1302522A SU268183A1 SU 268183 A1 SU268183 A1 SU 268183A1 SU 1302522/23 A SU1302522/23 A SU 1302522/23A SU 1302522 A SU1302522 A SU 1302522A SU 268183 A1 SU268183 A1 SU 268183A1
Authority
SU
USSR - Soviet Union
Prior art keywords
airplane
air intake
nozzle
intake channel
protection
Prior art date
Application number
SU1302522/23A
Other languages
Russian (ru)
Inventor
Н.Ф. Наумов
В.А. Терентьев
Original Assignee
Наумов Н.Ф.
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 Наумов Н.Ф. filed Critical Наумов Н.Ф.
Priority to SU1302522/23A priority Critical patent/SU268183A1/en
Application granted granted Critical
Publication of SU268183A1 publication Critical patent/SU268183A1/en

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  • Jet Pumps And Other Pumps (AREA)
  • Supercharger (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

Устройство для защиты турбореактивного двигателя самолета от попадания посторонних предметов в канал воздухозаборника, состоящее из патрубка и соединенного с ним сопла, установленных в нижней части передней кромки обечайки двигателя и связанных с источником сжатого газа, отличающееся тем, что, с целью повышения эффективности работы устройства, между его патрубком и соплом образована щель для создания зонтообразной газовой защиты, а сопло снабжено эжектирующим насадком.A device to protect the turbojet engine of an airplane from the ingress of foreign objects into the air intake channel consisting of a nozzle and a nozzle connected to it, installed in the lower part of the front edge of the engine shell and connected to a source of compressed gas, characterized in that a gap is formed between its pipe and the nozzle to create an umbrella-shaped gas protection, and the nozzle is provided with an ejecting nozzle.

SU1302522/23A 1969-01-31 1969-01-31 DEVICE FOR PROTECTION OF A TURBO-REACTIVE MOTOR OF AN AIRPLANE FROM CONTAMINATION OF OUTSIDE OBJECTS IN THE AIR INTAKE CHANNEL SU268183A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1302522/23A SU268183A1 (en) 1969-01-31 1969-01-31 DEVICE FOR PROTECTION OF A TURBO-REACTIVE MOTOR OF AN AIRPLANE FROM CONTAMINATION OF OUTSIDE OBJECTS IN THE AIR INTAKE CHANNEL

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1302522/23A SU268183A1 (en) 1969-01-31 1969-01-31 DEVICE FOR PROTECTION OF A TURBO-REACTIVE MOTOR OF AN AIRPLANE FROM CONTAMINATION OF OUTSIDE OBJECTS IN THE AIR INTAKE CHANNEL

Publications (1)

Publication Number Publication Date
SU268183A1 true SU268183A1 (en) 2005-03-10

Family

ID=60514593

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1302522/23A SU268183A1 (en) 1969-01-31 1969-01-31 DEVICE FOR PROTECTION OF A TURBO-REACTIVE MOTOR OF AN AIRPLANE FROM CONTAMINATION OF OUTSIDE OBJECTS IN THE AIR INTAKE CHANNEL

Country Status (1)

Country Link
SU (1) SU268183A1 (en)

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