EA202190881A1 - Гибридный реактивный двигатель - Google Patents

Гибридный реактивный двигатель

Info

Publication number
EA202190881A1
EA202190881A1 EA202190881A EA202190881A EA202190881A1 EA 202190881 A1 EA202190881 A1 EA 202190881A1 EA 202190881 A EA202190881 A EA 202190881A EA 202190881 A EA202190881 A EA 202190881A EA 202190881 A1 EA202190881 A1 EA 202190881A1
Authority
EA
Eurasian Patent Office
Prior art keywords
fairing
fan blades
shaft
central inner
jet engine
Prior art date
Application number
EA202190881A
Other languages
English (en)
Other versions
EA039862B1 (ru
Inventor
Кайл Альбрехт
Original Assignee
Кайл Альбрехт
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 Кайл Альбрехт filed Critical Кайл Альбрехт
Publication of EA202190881A1 publication Critical patent/EA202190881A1/ru
Publication of EA039862B1 publication Critical patent/EA039862B1/ru

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D13/00—Combinations of two or more machines or engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • 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
    • F02K3/06—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 with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Комбинированный реактивный двигатель, содержащий соединенные передний и задний обтекатели, имеющие трубчатую форму, причем задний обтекатель меньше, чем передний обтекатель, центральный внутренний контур и продольный вал, расположенный внутри переднего обтекателя и заднего обтекателя, множество главных лопаток вентилятора, расположенных на первом конце вала на переднем обтекателе, множество вспомогательных лопаток вентилятора, расположенных на втором конце вала на заднем обтекателе, по меньшей мере один аэродинамический стабилизатор, расположенный на поверхности центрального внутреннего контура с прохождением от нее, и по меньшей мере один видоизмененный односторонний клапан Тесла, расположенный на поверхности центрального внутреннего контура, для приема набегающего воздуха и для предоставления набегающего воздуха на множество вспомогательных лопаток вентилятора таким образом, что воздух повторно используется посредством вала центрального внутреннего контура для подачи мощности на множество главных лопаток вентилятора.
EA202190881A 2018-09-24 2019-09-24 Комбинированный реактивный двигатель EA039862B1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US16/139,600 US10837305B2 (en) 2018-09-24 2018-09-24 Hybrid jet engine
PCT/US2019/052711 WO2020068838A1 (en) 2018-09-24 2019-09-24 Hybrid jet engine

Publications (2)

Publication Number Publication Date
EA202190881A1 true EA202190881A1 (ru) 2021-08-06
EA039862B1 EA039862B1 (ru) 2022-03-21

Family

ID=69884506

Family Applications (1)

Application Number Title Priority Date Filing Date
EA202190881A EA039862B1 (ru) 2018-09-24 2019-09-24 Комбинированный реактивный двигатель

Country Status (5)

Country Link
US (1) US10837305B2 (ru)
EP (1) EP3857042B1 (ru)
CN (1) CN113227564B (ru)
EA (1) EA039862B1 (ru)
WO (1) WO2020068838A1 (ru)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112879159B (zh) * 2021-03-02 2021-08-24 江晓东 一种特斯拉阀结构内燃机
CN114278964B (zh) * 2021-12-27 2022-12-13 中国人民解放军国防科技大学 一种适用于宽范围冲压发动机的燃油喷嘴

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2612749A (en) * 1946-04-11 1952-10-07 Tenney Resonant pulse jet device with restricted flow passage
US3365880A (en) * 1966-10-06 1968-01-30 John J. Grebe Combustion apparatus for producing a high kinetic energy working gas stream and method of its use
FR2925120B1 (fr) * 2007-12-18 2010-02-19 Snecma Extension de carter intermediaire pour turboreacteur d'aeronef, comprenant une rainure annulaire sectorisee de reception des capots de nacelle
US9296288B2 (en) * 2012-05-07 2016-03-29 Separation Design Group Llc Hybrid radiant energy aircraft engine
CN104832318A (zh) * 2014-02-10 2015-08-12 苟仲武 一种冲压喷气发动机
CN105888879A (zh) * 2015-01-19 2016-08-24 王小水 一种喷气发电式发动机及燃料多次循环利用的发动机
DE102015206093A1 (de) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Fluggasturbine
FR3042226B1 (fr) * 2015-10-13 2019-06-07 Safran Nacelles Tuyere de section variable pour nacelle d'aeronef et nacelle pour un turboreacteur d'aeronef comportant une telle tuyere

Also Published As

Publication number Publication date
CN113227564A (zh) 2021-08-06
EP3857042B1 (en) 2023-02-22
US10837305B2 (en) 2020-11-17
WO2020068838A1 (en) 2020-04-02
EA039862B1 (ru) 2022-03-21
EP3857042A4 (en) 2021-12-08
CN113227564B (zh) 2022-07-26
US20200095884A1 (en) 2020-03-26
EP3857042A1 (en) 2021-08-04

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