[go: up one dir, main page]

RU94022652A - Multipurpose aerspace module - Google Patents

Multipurpose aerspace module

Info

Publication number
RU94022652A
RU94022652A RU94022652/11A RU94022652A RU94022652A RU 94022652 A RU94022652 A RU 94022652A RU 94022652/11 A RU94022652/11 A RU 94022652/11A RU 94022652 A RU94022652 A RU 94022652A RU 94022652 A RU94022652 A RU 94022652A
Authority
RU
Russia
Prior art keywords
aircraft
fuselage
aerspace
multipurpose
module
Prior art date
Application number
RU94022652/11A
Other languages
Russian (ru)
Inventor
С.Ф. Тандилов
Original Assignee
С.Ф. Тандилов
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 С.Ф. Тандилов filed Critical С.Ф. Тандилов
Priority to RU94022652/11A priority Critical patent/RU94022652A/en
Publication of RU94022652A publication Critical patent/RU94022652A/en

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

FIELD: manufacture of aircraft. SUBSTANCE: running along longitudinal axis of flying vehicle fuselage is through center passage where gas compressor is located. Turbine of gas compressor is set in rotation by means of jet engine located in forward fuselage. EFFECT: enhanced aerodynamic efficiency and enhanced efficiency of power plants.

Claims (1)

Изобретение относится к самолетостроению и направлено на улучшение аэродинамических показателей летательных аппаратов, а также на повышение эффективности из силовых установок. Вдоль продольной оси фюзеляжа летательного аппарата проходит сквозной срединный тракт, в котором расположен газовый компрессор, турбина которого приводится во вращение посредством реактивного двигателя, расположенного в передней части фюзеляжа.The invention relates to aircraft construction and is aimed at improving the aerodynamic performance of aircraft, as well as improving efficiency from power plants. Along the longitudinal axis of the fuselage of the aircraft, there is a through median tract, in which there is a gas compressor, the turbine of which is driven by a jet engine located in front of the fuselage.
RU94022652/11A 1994-06-10 1994-06-10 Multipurpose aerspace module RU94022652A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94022652/11A RU94022652A (en) 1994-06-10 1994-06-10 Multipurpose aerspace module

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94022652/11A RU94022652A (en) 1994-06-10 1994-06-10 Multipurpose aerspace module

Publications (1)

Publication Number Publication Date
RU94022652A true RU94022652A (en) 1996-09-20

Family

ID=48447920

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94022652/11A RU94022652A (en) 1994-06-10 1994-06-10 Multipurpose aerspace module

Country Status (1)

Country Link
RU (1) RU94022652A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2597740C1 (en) * 2015-04-22 2016-09-20 Николай Евгеньевич Староверов Unmanned aerial vehicle (versions) and operation method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2597740C1 (en) * 2015-04-22 2016-09-20 Николай Евгеньевич Староверов Unmanned aerial vehicle (versions) and operation method thereof

Similar Documents

Publication Publication Date Title
US11988099B2 (en) Unducted thrust producing system architecture
US6786036B2 (en) Bimodal fan, heat exchanger and bypass air supercharging for piston or rotary driven turbine
US4488399A (en) Propfan aircraft propulsion engine
SE8203975D0 (en) KOMPOUNDDRIVAGGREGAT
CN108891595A (en) Across the medium flight device power device sealed using medium sensing device and duct
GB588096A (en) Improvements in or relating to internal combustion turbine power plants
GB1413845A (en) Marine propulsion
DE3880535D1 (en) GAS TURBINE SYSTEM FOR HELICOPTERS.
RU94022652A (en) Multipurpose aerspace module
GB2169968A (en) Turbo-propeller aircraft gas turbine engines
US5063735A (en) Rocket-powered ducted fan engine
RU2007144088A (en) AIRCRAFT WITH A LOW NOISE, IN PARTICULAR, ON TAKEOFF AND LANDING
RU2465481C2 (en) Vortex propeller
GB583500A (en) Improvements in or relating to internal combustion engine power plants
RU94039826A (en) Multipurpose aerospace module
RU98113534A (en) COMBINED VEHICLE SCREW BLADE OF AIRCRAFT
RU2238223C1 (en) Triple-engine aircraft
US2395262A (en) Supercharging arrangement
RU2125659C1 (en) Turboramjet engine
RU94009999A (en) Transport aircraft with blunted tall section of fuselage
SU1023106A2 (en) Turbofan for open mines
GB586435A (en) Improvements in or relating to internal combustion turbine power plants
RU95101326A (en) Turbojet engine
RU2260704C1 (en) Method of reactive motion and device for its implementation i form of compressorless air-jet engine
SU1270389A1 (en) Combination gas-turbine plant