RU94001662A - GAS TURBINE ENGINE - Google Patents

GAS TURBINE ENGINE

Info

Publication number
RU94001662A
RU94001662A RU94001662/06A RU94001662A RU94001662A RU 94001662 A RU94001662 A RU 94001662A RU 94001662/06 A RU94001662/06 A RU 94001662/06A RU 94001662 A RU94001662 A RU 94001662A RU 94001662 A RU94001662 A RU 94001662A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
turbine
multithreaded
cushioned
Prior art date
Application number
RU94001662/06A
Other languages
Russian (ru)
Other versions
RU2157905C2 (en
Inventor
В.А. Плотников
Original Assignee
Акционерное общество закрытого типа "Энерготех"
Filing date
Publication date
Application filed by Акционерное общество закрытого типа "Энерготех" filed Critical Акционерное общество закрытого типа "Энерготех"
Priority to RU94001662A priority Critical patent/RU2157905C2/en
Priority claimed from RU94001662A external-priority patent/RU2157905C2/en
Publication of RU94001662A publication Critical patent/RU94001662A/en
Application granted granted Critical
Publication of RU2157905C2 publication Critical patent/RU2157905C2/en

Links

Claims (1)

Изобретение относится к авиационным малоразмерным газотурбинным двигателям. Целью изобретения является повышение частоты вращения, упрощение охлаждения радиальной турбины, аэродинамическое понижение давления газа за турбиной. Для достижения цели шестерни многопоточного редуктора установлены в корпусах, задемпфированных в окружном направлении, турбокомпрессор выполнен консольным, вентилятор - без спрямляющего аппарата, камера сгорания - с вращающейся топливной форсункой.The invention relates to aircraft small gas turbine engines. The aim of the invention is to increase the rotational speed, simplify the cooling of the radial turbine, the aerodynamic lowering of the gas pressure behind the turbine. To achieve the goal, the gears of the multithreaded gearbox are installed in housings, cushioned in the circumferential direction, the turbocharger is made console, the fan is without spraying apparatus, the combustion chamber is with rotating fuel nozzle.
RU94001662A 1994-01-17 1994-01-17 Gas-turbine engine RU2157905C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94001662A RU2157905C2 (en) 1994-01-17 1994-01-17 Gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94001662A RU2157905C2 (en) 1994-01-17 1994-01-17 Gas-turbine engine

Publications (2)

Publication Number Publication Date
RU94001662A true RU94001662A (en) 1995-12-27
RU2157905C2 RU2157905C2 (en) 2000-10-20

Family

ID=20151584

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94001662A RU2157905C2 (en) 1994-01-17 1994-01-17 Gas-turbine engine

Country Status (1)

Country Link
RU (1) RU2157905C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2621854C2 (en) * 2011-07-04 2017-06-07 Снекма Gas-turbine engine drive shaft device, gas-turbine engine and aircraft

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2926738B1 (en) * 2008-01-29 2010-04-02 Snecma DEHUILING DEVICE AND TURBOMACHINE COMPRISING SAID DEVICE
FR2942203B1 (en) * 2009-02-13 2011-04-22 Snecma SYSTEM OF CONTRAROTATIVE PROPELLERS WITH REDUCED SIZE
FR2964943B1 (en) * 2010-09-20 2012-10-05 Snecma DEVICE FOR SEALING A HOUSING FOR THE CROSSING CROSS BY A CONNECTING ROD OF A CONTROL SYSTEM FOR ORIENTATION OF BLOWER BLADES OF A TURBOPROPULSOR
FR3020410B1 (en) * 2014-04-29 2021-09-17 Snecma AIRCRAFT TURBOMACHINE WITH IMPROVED MECHANICAL POWER TAKE-OFF
FR3020409B1 (en) * 2014-04-29 2020-10-23 Snecma AIRCRAFT TURBOMACHINE ASSEMBLY, INCLUDING A MECHANICAL POWER TAPPING BOX WITH EASY ACCESS
RU2597322C1 (en) * 2015-04-28 2016-09-10 Открытое акционерное общество "Омское моторостроительное конструкторское бюро" (ОАО "ОМКБ") Small-size gas turbine engine
RU2711895C2 (en) * 2017-06-19 2020-01-23 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" Double-flow jet turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2621854C2 (en) * 2011-07-04 2017-06-07 Снекма Gas-turbine engine drive shaft device, gas-turbine engine and aircraft

Similar Documents

Publication Publication Date Title
JP4463810B2 (en) Aircraft engine equipment
CA1050774A (en) Diffuser-burner casing for a gas turbine engine
US7475549B2 (en) Thermal management system for a gas turbine engine
US20090110561A1 (en) Turbine engine components, turbine engine assemblies, and methods of manufacturing turbine engine components
GB1436796A (en) Gas turbine ducted fan engines of multi-shaft and multi-flow construction
CA2117241A1 (en) Improvements in or relating to gas turbine engines
US4240252A (en) Acoustically-treated mixer for a mixed flow gas turbine engine
GB1361036A (en) Gas turbine ducted fan propulsion unit
US10260748B2 (en) Gas turbine engine combustor with tailored temperature profile
WO1999023374A3 (en) Jet engine having radial turbine blades and flow-directing turbine manifolds
JPS6424126A (en) Combustor with intensified turbine nozzle cooling
CN2695659Y (en) Composite ramjet and fanjet engine
RU94001662A (en) GAS TURBINE ENGINE
US3824031A (en) Turbine casing for a gas turbine engine
US8403629B2 (en) Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
GB1435687A (en) Gas generators
RU2157905C2 (en) Gas-turbine engine
RU2096639C1 (en) Gas-turbine engine
RU2126906C1 (en) Transport two-shaft and three-shaft gas-turbine engines (variants)
GB2017222A (en) Gas Turbine Unit
RU185175U1 (en) Turbine generator rotor assembly
GB595982A (en) Improvements in and relating to gas turbines
RU2027886C1 (en) Gas-turbine engine
GB129739A (en) Improvements in and relating to Internal Combustion Engines.
Martinuzzi Gas-Turbine Progress Report—Cycle Components