RU2001123101A - Flame tube of a combustion chamber of a gas turbine engine - Google Patents

Flame tube of a combustion chamber of a gas turbine engine

Info

Publication number
RU2001123101A
RU2001123101A RU2001123101/06A RU2001123101A RU2001123101A RU 2001123101 A RU2001123101 A RU 2001123101A RU 2001123101/06 A RU2001123101/06 A RU 2001123101/06A RU 2001123101 A RU2001123101 A RU 2001123101A RU 2001123101 A RU2001123101 A RU 2001123101A
Authority
RU
Russia
Prior art keywords
housing
combustion chamber
gas turbine
turbine engine
flame tube
Prior art date
Application number
RU2001123101/06A
Other languages
Russian (ru)
Other versions
RU2212587C2 (en
Inventor
Андрей Владимирович Охлобыстин
Владимир Васильевич Птицын
Original Assignee
Открытое акционерное общество "Научно-производственное объединение "Сатурн"
Filing date
Publication date
Application filed by Открытое акционерное общество "Научно-производственное объединение "Сатурн" filed Critical Открытое акционерное общество "Научно-производственное объединение "Сатурн"
Priority to RU2001123101A priority Critical patent/RU2212587C2/en
Priority claimed from RU2001123101A external-priority patent/RU2212587C2/en
Publication of RU2001123101A publication Critical patent/RU2001123101A/en
Application granted granted Critical
Publication of RU2212587C2 publication Critical patent/RU2212587C2/en

Links

Claims (1)

Жаровая труба камеры сгорания газотурбинного двигателя, содержащая корпус и сегменты, снабженные двумя продольными и двумя поперечными ребрами и закрепленные на корпусе, по крайней мере, в одной точке, отличающаяся тем, что на корпусе выполнены поперечные бурты, между которыми расположены поперечные ребра сегментов; каждое из продольных ребер сегментов имеет выступ, при этом выступ на одном ребре сегмента расположен ближе к корпусу, а на другом - удален от корпуса, выступы соседних сегментов установлены один над другим с возможностью контакта и крепление сегмента к корпусу выполнено вблизи выступа, удаленного от корпуса.A flame tube of a combustion chamber of a gas turbine engine, comprising a housing and segments provided with two longitudinal and two transverse ribs and mounted on the housing at least at one point, characterized in that transverse collars are made on the housing, between which transverse ribs of the segments are located; each of the longitudinal ribs of the segments has a protrusion, while the protrusion on one edge of the segment is located closer to the housing, and on the other it is remote from the housing, the protrusions of adjacent segments are mounted one above the other with the possibility of contact and the segment is attached to the housing near the protrusion remote from the housing .
RU2001123101A 2001-08-16 2001-08-16 Gas-turbine engine combustion chamber flame tube RU2212587C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001123101A RU2212587C2 (en) 2001-08-16 2001-08-16 Gas-turbine engine combustion chamber flame tube

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001123101A RU2212587C2 (en) 2001-08-16 2001-08-16 Gas-turbine engine combustion chamber flame tube

Publications (2)

Publication Number Publication Date
RU2001123101A true RU2001123101A (en) 2003-05-10
RU2212587C2 RU2212587C2 (en) 2003-09-20

Family

ID=29776877

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001123101A RU2212587C2 (en) 2001-08-16 2001-08-16 Gas-turbine engine combustion chamber flame tube

Country Status (1)

Country Link
RU (1) RU2212587C2 (en)

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