RU98100457A - AIRCRAFT GAS TURBINE ENGINE - Google Patents

AIRCRAFT GAS TURBINE ENGINE

Info

Publication number
RU98100457A
RU98100457A RU98100457/06A RU98100457A RU98100457A RU 98100457 A RU98100457 A RU 98100457A RU 98100457/06 A RU98100457/06 A RU 98100457/06A RU 98100457 A RU98100457 A RU 98100457A RU 98100457 A RU98100457 A RU 98100457A
Authority
RU
Russia
Prior art keywords
engine
gas turbine
aircraft gas
turbine engine
housing
Prior art date
Application number
RU98100457/06A
Other languages
Russian (ru)
Other versions
RU2162957C2 (en
Inventor
Л.А. Савин
А.М. Долотов
О.В. Соломин
Д.Е. Устинов
Original Assignee
Орловский государственный технический университет
Filing date
Publication date
Application filed by Орловский государственный технический университет filed Critical Орловский государственный технический университет
Priority to RU98100457A priority Critical patent/RU2162957C2/en
Priority claimed from RU98100457A external-priority patent/RU2162957C2/en
Publication of RU98100457A publication Critical patent/RU98100457A/en
Application granted granted Critical
Publication of RU2162957C2 publication Critical patent/RU2162957C2/en

Links

Claims (1)

Авиационный газотурбинный двигатель, содержащий корпус, входное и сопловое устройства, камеру сгорания, турбокомпрессор, установленный на газовых подшипниках, образованных компрессорными и турбинными цапфами роторов и вкладышами подшипников, закрепленных на корпусе двигателя посредством полых лопаток направляющего, спрямляющего и соплового аппаратов, либо поверхностями ободов, образованных бандажными полками компрессорных или турбинных лопаток и ответными поверхностями элементов корпуса двигателя, отличающийся тем, что внутри полого ротора турбокомпрессора установлен воздушно-реактивный прямоточный двигатель, корпусом которого является кожух, закрепленный неподвижно на корневых частях полых лопаток направляющего или соплового аппаратов.An aircraft gas turbine engine comprising a housing, an inlet and nozzle device, a combustion chamber, a turbocompressor mounted on gas bearings formed by compressor and turbine axles of rotors and bearing shells fixed to the engine housing by means of hollow vanes of a guide, straightening and nozzle apparatus, or by the surfaces of the rims, formed by retaining shelves of compressor or turbine blades and mating surfaces of the elements of the engine casing, characterized in that inside th turbocharger rotor mounted air-breathing ramjet engine, whose housing cover is mounted fixedly on the root portions of the hollow nozzle vanes or guide devices.
RU98100457A 1998-01-06 1998-01-06 Aircraft gas-turbine engine RU2162957C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU98100457A RU2162957C2 (en) 1998-01-06 1998-01-06 Aircraft gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU98100457A RU2162957C2 (en) 1998-01-06 1998-01-06 Aircraft gas-turbine engine

Publications (2)

Publication Number Publication Date
RU98100457A true RU98100457A (en) 2000-01-10
RU2162957C2 RU2162957C2 (en) 2001-02-10

Family

ID=20201079

Family Applications (1)

Application Number Title Priority Date Filing Date
RU98100457A RU2162957C2 (en) 1998-01-06 1998-01-06 Aircraft gas-turbine engine

Country Status (1)

Country Link
RU (1) RU2162957C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2009148052A (en) 2009-12-24 2011-06-27 Владимир Тарасович Шведов (RU) METHOD FOR CRAWLING FOR A VEHICLE INTENDED FOR MOVEMENT IN A FLUID
RU2626278C2 (en) * 2015-03-20 2017-07-25 Виктор Серафимович Бахирев Hybrid air-breathing engine
RU2608426C2 (en) * 2015-05-26 2017-01-18 Виктор Серафимович Бахирев Versatile air-breather engine

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