BG104795A - Propulsion device for a flying machine - Google Patents
Propulsion device for a flying machineInfo
- Publication number
- BG104795A BG104795A BG104795A BG10479500A BG104795A BG 104795 A BG104795 A BG 104795A BG 104795 A BG104795 A BG 104795A BG 10479500 A BG10479500 A BG 10479500A BG 104795 A BG104795 A BG 104795A
- Authority
- BG
- Bulgaria
- Prior art keywords
- flying machine
- engines
- propulsion device
- separation
- propulsion
- Prior art date
Links
- 238000000926 separation method Methods 0.000 abstract 2
- 230000005540 biological transmission Effects 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 230000001360 synchronised effect Effects 0.000 abstract 1
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
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K5/00—Arrangement or mounting of internal-combustion or jet-propulsion units
- B60K5/08—Arrangement or mounting of internal-combustion or jet-propulsion units comprising more than one engine
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Control Of Turbines (AREA)
- Retarders (AREA)
- Transmission Devices (AREA)
Abstract
The device is designed for a flying machine, in particular for ones which are kept in flight by air flows generated by a rotor compressor. It comprises a propulsion system device and means of transmission to the raising (propelling) devices of the flying machine, as well as at least two independent engines (4, 5), each having the same or similar power, which are synchronized and each acts on a common drive shaft (9). Means are provided for the separation of the propulsion connection (7, 8) from shaft (9) in case of a fault in one of the two engines (4 & 5). The means of separation comprise of preferred automatically operating coupling connections of the driving connection components. 3 claims, 2 figures
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP98105615A EP0945340A1 (en) | 1998-03-27 | 1998-03-27 | Driving system for an aircraft |
PCT/CH1999/000109 WO1999050140A1 (en) | 1998-03-27 | 1999-03-09 | Propulsion system for an aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
BG104795A true BG104795A (en) | 2001-06-29 |
Family
ID=8231664
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BG104795A BG104795A (en) | 1998-03-27 | 2000-09-26 | Propulsion device for a flying machine |
Country Status (14)
Country | Link |
---|---|
EP (2) | EP0945340A1 (en) |
JP (1) | JP2002509841A (en) |
KR (1) | KR20010034656A (en) |
CN (1) | CN1293635A (en) |
AU (1) | AU2607499A (en) |
BG (1) | BG104795A (en) |
BR (1) | BR9909140A (en) |
CA (1) | CA2324447A1 (en) |
HU (1) | HUP0102323A3 (en) |
IL (1) | IL138550A0 (en) |
NO (1) | NO20004825L (en) |
PL (1) | PL343200A1 (en) |
SK (1) | SK13882000A3 (en) |
WO (1) | WO1999050140A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102015105787A1 (en) * | 2015-04-15 | 2016-10-20 | Johann Schwöller | Electric drive for an aircraft and hybrid system for an aircraft |
CN105857623A (en) * | 2016-03-28 | 2016-08-17 | 苏州妙旋无人机应用有限公司 | Engine special for unmanned aerial vehicle |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR465209A (en) * | 1913-11-22 | 1914-04-10 | Porsche Ferdinand A | Propeller control for air vehicles, in particular for airplanes |
US1664399A (en) * | 1923-08-07 | 1928-04-03 | Brown Ellsworth | Multiple-engine drive gear |
US2505853A (en) * | 1948-12-29 | 1950-05-02 | Fairchild Engine & Airplane | Output shaft coupling mechanism for multiple power plants |
US4177693A (en) * | 1978-06-22 | 1979-12-11 | Avco Corporation | Drive system |
US4829850A (en) * | 1987-02-25 | 1989-05-16 | Soloy Dual Pac, Inc. | Multiple engine drive for single output shaft and combining gearbox therefor |
-
1998
- 1998-03-27 EP EP98105615A patent/EP0945340A1/en not_active Withdrawn
-
1999
- 1999-03-09 HU HU0102323A patent/HUP0102323A3/en unknown
- 1999-03-09 CN CN99804109A patent/CN1293635A/en active Pending
- 1999-03-09 EP EP99906012A patent/EP1066194A1/en active Pending
- 1999-03-09 PL PL99343200A patent/PL343200A1/en not_active Application Discontinuation
- 1999-03-09 AU AU26074/99A patent/AU2607499A/en not_active Abandoned
- 1999-03-09 BR BR9909140-2A patent/BR9909140A/en not_active Application Discontinuation
- 1999-03-09 WO PCT/CH1999/000109 patent/WO1999050140A1/en not_active Application Discontinuation
- 1999-03-09 IL IL13855099A patent/IL138550A0/en unknown
- 1999-03-09 JP JP2000541064A patent/JP2002509841A/en active Pending
- 1999-03-09 CA CA002324447A patent/CA2324447A1/en not_active Abandoned
- 1999-03-09 KR KR1020007010590A patent/KR20010034656A/en not_active Application Discontinuation
- 1999-03-09 SK SK1388-2000A patent/SK13882000A3/en unknown
-
2000
- 2000-09-26 BG BG104795A patent/BG104795A/en unknown
- 2000-09-26 NO NO20004825A patent/NO20004825L/en unknown
Also Published As
Publication number | Publication date |
---|---|
KR20010034656A (en) | 2001-04-25 |
EP1066194A1 (en) | 2001-01-10 |
NO20004825D0 (en) | 2000-09-26 |
CN1293635A (en) | 2001-05-02 |
BR9909140A (en) | 2000-12-05 |
CA2324447A1 (en) | 1999-10-07 |
EP0945340A1 (en) | 1999-09-29 |
AU2607499A (en) | 1999-10-18 |
NO20004825L (en) | 2000-09-26 |
HUP0102323A3 (en) | 2001-12-28 |
IL138550A0 (en) | 2001-10-31 |
HUP0102323A2 (en) | 2001-11-28 |
JP2002509841A (en) | 2002-04-02 |
PL343200A1 (en) | 2001-07-30 |
WO1999050140A1 (en) | 1999-10-07 |
SK13882000A3 (en) | 2001-06-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2977315B1 (en) | Apparatus and methods for powering an electrical device associated with an aircraft rotor | |
US5309029A (en) | Aircraft power unit with elective mechanical coupling | |
EP0798454A3 (en) | Gas turbine engine system | |
EP1568606A3 (en) | Engine control system | |
DE50211818D1 (en) | Drive unit of a vehicle | |
CA2246752A1 (en) | Power output apparatus and method of controlling the same | |
US20050280264A1 (en) | Multistage wind-powered generator with shafts and a coupling system | |
WO2003020583A3 (en) | Rotor system for helicopters | |
EP0888966A3 (en) | High efficiency environmental control systems and methods | |
IT1297108B1 (en) | SYSTEM FOR THE TRANSFORMATION OF A SELF-SUPPORTED HORIZONTAL FLIGHT AIRCRAFT INTO AN INTEGRATED, HYBRID TAKE-OFF AIRCRAFT | |
EP1233179A3 (en) | Composite drive system for compressor | |
JPH02164695A (en) | Aircraft propellant device | |
EP1408601A3 (en) | Forced air stator ventilation system for superconducting synchronous machine | |
EP1069044A3 (en) | Auxiliary power and thrust unit | |
WO2003023204A3 (en) | Redundant prime mover system | |
JP2008506568A (en) | Aircraft propulsion device | |
EP1887197A3 (en) | A generator set | |
EP1361639A8 (en) | Power system having generator driven by engine | |
AU2223997A (en) | Modular engine | |
NO20181437A1 (en) | Drive arrangement | |
ES8704588A1 (en) | Auxiliary power unit and gearbox assembly for a gas turbine. | |
CA2273152A1 (en) | Engine-generator set with integral gear reduction | |
BG104795A (en) | Propulsion device for a flying machine | |
EP0795432A3 (en) | Method for mounting two auxiliary machines to automobile and power transmission device | |
EP0984130A3 (en) | Automaticdoor driving mechanism |