RU2016134175A - TURBOPROP - Google Patents

TURBOPROP Download PDF

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Publication number
RU2016134175A
RU2016134175A RU2016134175A RU2016134175A RU2016134175A RU 2016134175 A RU2016134175 A RU 2016134175A RU 2016134175 A RU2016134175 A RU 2016134175A RU 2016134175 A RU2016134175 A RU 2016134175A RU 2016134175 A RU2016134175 A RU 2016134175A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
gearbox
turboprop
axis
Prior art date
Application number
RU2016134175A
Other languages
Russian (ru)
Other versions
RU2645863C2 (en
Inventor
Валерий Владимирович Леонтьев
Алексей Владимирович Григорьев
Original Assignee
Акционерное общество "Климов"
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 Акционерное общество "Климов" filed Critical Акционерное общество "Климов"
Priority to RU2016134175A priority Critical patent/RU2645863C2/en
Publication of RU2016134175A publication Critical patent/RU2016134175A/en
Application granted granted Critical
Publication of RU2645863C2 publication Critical patent/RU2645863C2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Claims (1)

Турбовинтовой двигатель, содержащий турбовальный газотурбинный двигатель и редуктор воздушных винтов, причем выводной вал турбовального газотурбинного двигателя соединен с редуктором воздушных винтов с помощью механической трансмиссии, отличающийся тем, что редуктор имеет выводные валы для привода соосных воздушных винтов, а ось редуктора смещена относительно оси турбовального газотурбинного двигателя на величину, позволяющую разместить воздухозаборник газотурбинного двигателя в средней зоне радиуса воздушных винтов.A turboprop engine comprising a turboshaft gas turbine engine and a propeller gearbox, wherein the output shaft of the turboshaft gas turbine engine is connected to the propeller gearbox using a mechanical transmission, characterized in that the gearbox has output shafts for driving coaxial propellers, and the gearbox axis is offset relative to the axis of the turboshaft gas turbine engine by an amount that allows you to place the air intake of the gas turbine engine in the middle zone of the radius of the propellers.
RU2016134175A 2016-08-19 2016-08-19 Turboprop engine RU2645863C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016134175A RU2645863C2 (en) 2016-08-19 2016-08-19 Turboprop engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016134175A RU2645863C2 (en) 2016-08-19 2016-08-19 Turboprop engine

Publications (2)

Publication Number Publication Date
RU2016134175A true RU2016134175A (en) 2018-02-22
RU2645863C2 RU2645863C2 (en) 2018-02-28

Family

ID=61258736

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016134175A RU2645863C2 (en) 2016-08-19 2016-08-19 Turboprop engine

Country Status (1)

Country Link
RU (1) RU2645863C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110486165B (en) * 2019-07-31 2021-05-07 中国航发南方工业有限公司 Turboprop engine and unmanned aerial vehicle

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0950808A3 (en) * 1998-04-13 2000-05-24 Nikkiso Company, Ltd. Turbofan engine including fans with reduced speed
DE102004042730B4 (en) * 2004-05-21 2008-07-31 Robert Bosch Gmbh Filter device, in particular for an exhaust system of an internal combustion engine
FR2940247B1 (en) * 2008-12-19 2011-01-21 Snecma SYSTEM OF CONTRAROTATIVE PROPELLERS DRAWN BY AN EPICYCLOIDAL TRAIN PROVIDING A BALANCED TORQUE DISTRIBUTION BETWEEN THE TWO PROPELLERS
DE102010022932A1 (en) * 2010-06-04 2011-12-08 Christian Seefluth Bypass jet engine i.e. counterflow engine, for use in aircraft, has front blower deflecting fresh air around specified degrees in collecting cavity of core engine, where fresh air is sucked in front of outer housing of core engine

Also Published As

Publication number Publication date
RU2645863C2 (en) 2018-02-28

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