NO20004825L - Aircraft operating system - Google Patents

Aircraft operating system

Info

Publication number
NO20004825L
NO20004825L NO20004825A NO20004825A NO20004825L NO 20004825 L NO20004825 L NO 20004825L NO 20004825 A NO20004825 A NO 20004825A NO 20004825 A NO20004825 A NO 20004825A NO 20004825 L NO20004825 L NO 20004825L
Authority
NO
Norway
Prior art keywords
operating system
aircraft operating
connection
propulsion
synchronized
Prior art date
Application number
NO20004825A
Other languages
Norwegian (no)
Other versions
NO20004825D0 (en
Inventor
Alexander Frick
Original Assignee
Frick Aerotech Ag
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 Frick Aerotech Ag filed Critical Frick Aerotech Ag
Publication of NO20004825D0 publication Critical patent/NO20004825D0/en
Publication of NO20004825L publication Critical patent/NO20004825L/en

Links

Classifications

    • 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
    • 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

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)
  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Turbines (AREA)

Abstract

Oppfinnelsen vedrører et fremdriftssystem omfattende minst to uavhengige indre forbrenningsmotorer (4, 5) som er plassert direkte ved siden av hverandre og syn- kronisert og som hver virker på en felles drivaksel (9). Det er anordnet midler for i hver fremdriftsforbindelse (4 til 9 eller 5 til 9) som bryter denne forbindelse når der er et merkbart fall i ytelse (punkter for beregnet brudd, automatisk løskopling).The invention relates to a propulsion system comprising at least two independent internal combustion engines (4, 5) which are located directly next to each other and synchronized and each acting on a common drive shaft (9). Means are provided for in each propulsion connection (4 to 9 or 5 to 9) that break this connection when there is a noticeable drop in performance (points for calculated breakage, automatic release coupling).

NO20004825A 1998-03-27 2000-09-26 Aircraft operating system NO20004825L (en)

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 (2)

Publication Number Publication Date
NO20004825D0 NO20004825D0 (en) 2000-09-26
NO20004825L true NO20004825L (en) 2000-09-26

Family

ID=8231664

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20004825A NO20004825L (en) 1998-03-27 2000-09-26 Aircraft operating system

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
BG104795A (en) 2001-06-29
IL138550A0 (en) 2001-10-31
PL343200A1 (en) 2001-07-30
NO20004825D0 (en) 2000-09-26
WO1999050140A1 (en) 1999-10-07
CN1293635A (en) 2001-05-02
EP0945340A1 (en) 1999-09-29
CA2324447A1 (en) 1999-10-07
HUP0102323A3 (en) 2001-12-28
HUP0102323A2 (en) 2001-11-28
EP1066194A1 (en) 2001-01-10
JP2002509841A (en) 2002-04-02
SK13882000A3 (en) 2001-06-11
BR9909140A (en) 2000-12-05
KR20010034656A (en) 2001-04-25
AU2607499A (en) 1999-10-18

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