PL3123015T3 - Architektura układu napędowego śmigłowca wielosilnikowego i odpowiadający jej śmigłowiec - Google Patents
Architektura układu napędowego śmigłowca wielosilnikowego i odpowiadający jej śmigłowiecInfo
- Publication number
- PL3123015T3 PL3123015T3 PL15717548T PL15717548T PL3123015T3 PL 3123015 T3 PL3123015 T3 PL 3123015T3 PL 15717548 T PL15717548 T PL 15717548T PL 15717548 T PL15717548 T PL 15717548T PL 3123015 T3 PL3123015 T3 PL 3123015T3
- Authority
- PL
- Poland
- Prior art keywords
- helicopter
- architecture
- engined
- engined helicopter
- helicopter architecture
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/08—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/262—Restarting after flame-out
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical drives
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- 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
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. 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
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/329—Application in turbines in gas turbines in helicopters
-
- 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
- F05D2220/50—Application for auxiliary power units (APU's)
-
- 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
-
- 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
- F05D2240/00—Components
- F05D2240/35—Combustors or associated equipment
-
- 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
- F05D2260/00—Function
- F05D2260/85—Starting
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Eletrric Generators (AREA)
- Control Of Turbines (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Stand-By Power Supply Arrangements (AREA)
- Hybrid Electric Vehicles (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1452647A FR3019218B1 (fr) | 2014-03-27 | 2014-03-27 | Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant |
PCT/FR2015/050693 WO2015145037A1 (fr) | 2014-03-27 | 2015-03-20 | Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant |
EP15717548.0A EP3123015B1 (fr) | 2014-03-27 | 2015-03-20 | Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant |
Publications (1)
Publication Number | Publication Date |
---|---|
PL3123015T3 true PL3123015T3 (pl) | 2019-04-30 |
Family
ID=50780781
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL15717548T PL3123015T3 (pl) | 2014-03-27 | 2015-03-20 | Architektura układu napędowego śmigłowca wielosilnikowego i odpowiadający jej śmigłowiec |
Country Status (11)
Country | Link |
---|---|
US (1) | US10766629B2 (pl) |
EP (1) | EP3123015B1 (pl) |
JP (1) | JP6705753B2 (pl) |
KR (1) | KR102318629B1 (pl) |
CN (1) | CN106458322B (pl) |
CA (1) | CA2942942C (pl) |
ES (1) | ES2702329T3 (pl) |
FR (1) | FR3019218B1 (pl) |
PL (1) | PL3123015T3 (pl) |
RU (1) | RU2690608C2 (pl) |
WO (1) | WO2015145037A1 (pl) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3019219B1 (fr) * | 2014-03-27 | 2016-03-18 | Turbomeca | Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant |
FR3019524B1 (fr) * | 2014-04-03 | 2017-12-08 | Turbomeca | Chaine motrice pour helicoptere incorporant un module moteur pyrotechnique d'assistance et helicoptere la comportant |
FR3024707B1 (fr) * | 2014-08-07 | 2018-03-23 | Turbomeca | Dispositif d'assistance rapide pour une turbomachine a turbine libre d'un aeronef |
WO2016049027A1 (en) * | 2014-09-23 | 2016-03-31 | Sikorsky Aircraft Corporation | Hybrid electric power drive system for a rotorcraft |
US10836505B2 (en) * | 2016-06-23 | 2020-11-17 | Raytheon Technologies Corporation | Operating auxiliary power unit during off-nominal propulsion system operation |
US11415063B2 (en) | 2016-09-15 | 2022-08-16 | Pratt & Whitney Canada Corp. | Reverse-flow gas turbine engine |
US10006375B1 (en) * | 2017-07-11 | 2018-06-26 | General Electric Company | Propulsion system for an aircraft |
FR3069407B1 (fr) * | 2017-07-20 | 2019-08-09 | Safran Electrical & Power | Architecture de ventilation d'helicoptere a chambre de melange |
FR3081150B1 (fr) * | 2018-05-18 | 2020-06-12 | Safran Helicopter Engines | Architecture de puissance d'un aeronef |
FR3082225B1 (fr) * | 2018-06-07 | 2020-06-05 | Safran Helicopter Engines | Systeme propulsif asymetrique a recuperation de chaleur |
FR3084340B1 (fr) * | 2018-07-27 | 2022-05-06 | Safran | Systeme de generation de puissance electrique pour aeronef |
PL3653859T3 (pl) | 2018-08-08 | 2024-05-27 | Pratt & Whitney Canada Corp. | Układ wielosilnikowy i jego sposób |
WO2020180374A1 (en) | 2019-03-01 | 2020-09-10 | United Technologies Advanced Projects Inc. | Distributed propulsion configurations for aircraft having mixed drive systems |
US11732639B2 (en) | 2019-03-01 | 2023-08-22 | Pratt & Whitney Canada Corp. | Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems |
US11628942B2 (en) | 2019-03-01 | 2023-04-18 | Pratt & Whitney Canada Corp. | Torque ripple control for an aircraft power train |
WO2020190344A2 (en) | 2019-03-18 | 2020-09-24 | United Technologies Advanced Projects Inc. | Architectures for hybrid-electric propulsion |
US11299286B2 (en) | 2019-05-15 | 2022-04-12 | Pratt & Whitney Canada Corp. | System and method for operating a multi-engine aircraft |
US11663863B2 (en) | 2019-06-07 | 2023-05-30 | Pratt & Whitney Canada Corp. | Methods and systems for operating a rotorcraft |
US20210310412A1 (en) * | 2020-04-06 | 2021-10-07 | Williams International Co., L.L.C. | External auxiliary power unit |
US11486472B2 (en) | 2020-04-16 | 2022-11-01 | United Technologies Advanced Projects Inc. | Gear sytems with variable speed drive |
CN111520234A (zh) * | 2020-04-30 | 2020-08-11 | 中国直升机设计研究所 | 一种高原环境直升机发动机起动装置及方法 |
FR3114703B1 (fr) | 2020-09-30 | 2023-07-07 | Safran | Conducteur électrique à refroidissement par matériau à changement de phase et son procédé de fabrication |
JP7430134B2 (ja) * | 2020-12-22 | 2024-02-09 | 本田技研工業株式会社 | 航空機用推進システム |
JP7355726B2 (ja) * | 2020-12-22 | 2023-10-03 | 本田技研工業株式会社 | 航空機用推進システム |
US11668249B2 (en) | 2021-09-14 | 2023-06-06 | Pratt & Whitney Canada Corp. | System and method for operating a multi-engine aircraft |
US12037952B2 (en) | 2022-01-04 | 2024-07-16 | General Electric Company | Systems and methods for providing output products to a combustion chamber of a gas turbine engine |
US11933216B2 (en) | 2022-01-04 | 2024-03-19 | General Electric Company | Systems and methods for providing output products to a combustion chamber of a gas turbine engine |
US11794912B2 (en) | 2022-01-04 | 2023-10-24 | General Electric Company | Systems and methods for reducing emissions with a fuel cell |
US11719441B2 (en) | 2022-01-04 | 2023-08-08 | General Electric Company | Systems and methods for providing output products to a combustion chamber of a gas turbine engine |
US11970282B2 (en) | 2022-01-05 | 2024-04-30 | General Electric Company | Aircraft thrust management with a fuel cell |
US12034298B2 (en) | 2022-01-10 | 2024-07-09 | General Electric Company | Power source for an aircraft |
US11804607B2 (en) | 2022-01-21 | 2023-10-31 | General Electric Company | Cooling of a fuel cell assembly |
US12037124B2 (en) | 2022-01-21 | 2024-07-16 | General Electric Company | Systems and method of operating a fuel cell assembly |
US12074350B2 (en) | 2022-01-21 | 2024-08-27 | General Electric Company | Solid oxide fuel cell assembly |
US11967743B2 (en) | 2022-02-21 | 2024-04-23 | General Electric Company | Modular fuel cell assembly |
US12025061B2 (en) | 2022-04-04 | 2024-07-02 | General Electric Company | Gas turbine engine with fuel cell assembly |
US12043406B2 (en) | 2022-05-27 | 2024-07-23 | General Electric Company | Method of operating a fuel cell assembly for an aircraft |
US11817700B1 (en) | 2022-07-20 | 2023-11-14 | General Electric Company | Decentralized electrical power allocation system |
US12078350B2 (en) | 2022-11-10 | 2024-09-03 | General Electric Company | Gas turbine combustion section having an integrated fuel cell assembly |
US11859820B1 (en) | 2022-11-10 | 2024-01-02 | General Electric Company | Gas turbine combustion section having an integrated fuel cell assembly |
US11923586B1 (en) | 2022-11-10 | 2024-03-05 | General Electric Company | Gas turbine combustion section having an integrated fuel cell assembly |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1151717A (fr) | 1956-06-20 | 1958-02-05 | écrou indessérable | |
FR1359766A (fr) | 1963-03-12 | 1964-04-30 | Appareil de traitement médical | |
US5899411A (en) * | 1996-01-22 | 1999-05-04 | Sundstrand Corporation | Aircraft electrical system providing emergency power and electric starting of propulsion engines |
RU2188960C1 (ru) * | 2001-08-20 | 2002-09-10 | Кондрашов Борис Михайлович | Способ преобразования энергии в силовой установке (варианты), струйно-адаптивном двигателе и газогенераторе |
US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
US7701082B2 (en) * | 2006-10-30 | 2010-04-20 | Honeywell International Inc. | Aerospace electrical power DC subsystem configuration using multi-functional DC/DC converter |
FR2914697B1 (fr) * | 2007-04-06 | 2012-11-30 | Turbomeca | Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration |
US8062081B2 (en) * | 2007-12-12 | 2011-11-22 | Foss Maritime Company, Inc. | Hybrid propulsion systems |
FR2954283B1 (fr) * | 2009-12-23 | 2012-03-02 | Hispano Suiza Sa | Aeronef comportant un demarreur-generateur electrique pour le ou chaque turboreacteur et un train d'aterrissage equipe d'un moteur electrique de manoeuvre au sol |
FR2967132B1 (fr) | 2010-11-04 | 2012-11-09 | Turbomeca | Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur dissymetrique a systeme de regulation pour sa mise en oeuvre |
FR2968716B1 (fr) * | 2010-12-13 | 2012-12-28 | Turbomeca | Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et turbomoteur mettant en oeuvre un tel procede |
US20130031912A1 (en) * | 2011-08-01 | 2013-02-07 | Hamilton Sundstrand Corporation | Gas turbine start architecture |
GB2509009B (en) * | 2011-08-30 | 2016-03-09 | Ge Aviat Systems Ltd | Power distribution in aircraft |
US9267438B2 (en) * | 2011-10-11 | 2016-02-23 | Pratt & Whitney Canada Corp. | Starting of aircraft engine |
FR2990573B1 (fr) * | 2012-05-11 | 2015-11-20 | Hispano Suiza Sa | Systeme de commande et d'alimentation en energie des turbomachines d'un helicoptere |
FR2992024B1 (fr) * | 2012-06-15 | 2017-07-21 | Turbomeca | Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere |
-
2014
- 2014-03-27 FR FR1452647A patent/FR3019218B1/fr active Active
-
2015
- 2015-03-20 RU RU2016139023A patent/RU2690608C2/ru active
- 2015-03-20 JP JP2016559339A patent/JP6705753B2/ja not_active Expired - Fee Related
- 2015-03-20 PL PL15717548T patent/PL3123015T3/pl unknown
- 2015-03-20 WO PCT/FR2015/050693 patent/WO2015145037A1/fr active Application Filing
- 2015-03-20 KR KR1020167027382A patent/KR102318629B1/ko active IP Right Grant
- 2015-03-20 ES ES15717548T patent/ES2702329T3/es active Active
- 2015-03-20 US US15/127,747 patent/US10766629B2/en active Active
- 2015-03-20 CA CA2942942A patent/CA2942942C/fr active Active
- 2015-03-20 EP EP15717548.0A patent/EP3123015B1/fr active Active
- 2015-03-20 CN CN201580015360.1A patent/CN106458322B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
FR3019218B1 (fr) | 2016-03-18 |
EP3123015A1 (fr) | 2017-02-01 |
CA2942942C (fr) | 2021-10-12 |
US20170152055A1 (en) | 2017-06-01 |
JP6705753B2 (ja) | 2020-06-03 |
RU2690608C2 (ru) | 2019-06-04 |
WO2015145037A1 (fr) | 2015-10-01 |
CA2942942A1 (fr) | 2015-10-01 |
CN106458322B (zh) | 2019-08-13 |
US10766629B2 (en) | 2020-09-08 |
ES2702329T3 (es) | 2019-02-28 |
RU2016139023A (ru) | 2018-04-28 |
FR3019218A1 (fr) | 2015-10-02 |
CN106458322A (zh) | 2017-02-22 |
KR20170002378A (ko) | 2017-01-06 |
RU2016139023A3 (pl) | 2018-10-26 |
KR102318629B1 (ko) | 2021-10-29 |
EP3123015B1 (fr) | 2018-11-07 |
JP2017514057A (ja) | 2017-06-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IL279836B (en) | aircraft system | |
PL3123015T3 (pl) | Architektura układu napędowego śmigłowca wielosilnikowego i odpowiadający jej śmigłowiec | |
PL3123014T3 (pl) | Architektura układu napędowego śmigłowca wielosilnikowego oraz śmigłowiec | |
HK1218410A1 (zh) | 旋翼升力航空器 | |
GB201508138D0 (en) | Aircraft | |
SG11201709198WA (en) | Rotary-wing aircraft | |
GB201416842D0 (en) | Aircraft | |
PL3177817T3 (pl) | Statek powietrzny | |
EP3168521A4 (en) | Limiting device and aircraft using same | |
IL231811A0 (en) | An asymmetric helicopter with multiple rotors | |
GB201616518D0 (en) | Aircraft | |
GB2527893B (en) | Aircraft airframe assembly | |
PL2905228T3 (pl) | Płatowiec kadłubowy i zbiornik | |
PL3335983T3 (pl) | Statek powietrzny | |
GB201417014D0 (en) | Aircraft seat | |
PL3140189T3 (pl) | Śmigłowiec | |
EP3122628A4 (en) | Aircraft pylon | |
EP3209559A4 (en) | Aircraft | |
HK1201014A2 (en) | Driving mechanism and multi-rotor aircraft | |
GB201417017D0 (en) | Aircraft seat | |
GB2549885B (en) | Landing system | |
GB201417009D0 (en) | Aircraft seat | |
GB201604201D0 (en) | Aircraft galley unit | |
GB2526916B (en) | Aircraft airframe assembly | |
TWM489676U (en) | Quantity-changeable multi-rotor aircraft structure |