IT8622586A0 - Apparecchio e metodo per impedire il rallentamento involontario di un motore funzionante di un aeromobile a piu' motori. - Google Patents

Apparecchio e metodo per impedire il rallentamento involontario di un motore funzionante di un aeromobile a piu' motori.

Info

Publication number
IT8622586A0
IT8622586A0 IT8622586A IT2258686A IT8622586A0 IT 8622586 A0 IT8622586 A0 IT 8622586A0 IT 8622586 A IT8622586 A IT 8622586A IT 2258686 A IT2258686 A IT 2258686A IT 8622586 A0 IT8622586 A0 IT 8622586A0
Authority
IT
Italy
Prior art keywords
engine
slowing
preventing unintentional
aircraft
operating
Prior art date
Application number
IT8622586A
Other languages
English (en)
Other versions
IT1214572B (it
Inventor
Frederick Ebert
Stephen H Silder
Michael A Beins
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of IT8622586A0 publication Critical patent/IT8622586A0/it
Application granted granted Critical
Publication of IT1214572B publication Critical patent/IT1214572B/it

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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/04—Initiating means actuated personally
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/20—Control lever and linkage systems
    • Y10T74/20576—Elements
    • Y10T74/20582—Levers
    • Y10T74/2063—Stops

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Coupling Device And Connection With Printed Circuit (AREA)
  • Time-Division Multiplex Systems (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Retarders (AREA)
  • Time Recorders, Dirve Recorders, Access Control (AREA)
IT8622586A 1985-12-06 1986-12-05 Apparecchio e metodo per impedire il rallentamento involontario di un motore funzionante di un aeromobile a piu' motori. IT1214572B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/805,682 US4655414A (en) 1985-12-06 1985-12-06 Preventing inadvertent downthrottling of the operative engine in a multi-engine aircraft

Publications (2)

Publication Number Publication Date
IT8622586A0 true IT8622586A0 (it) 1986-12-05
IT1214572B IT1214572B (it) 1990-01-18

Family

ID=25192226

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8622586A IT1214572B (it) 1985-12-06 1986-12-05 Apparecchio e metodo per impedire il rallentamento involontario di un motore funzionante di un aeromobile a piu' motori.

Country Status (13)

Country Link
US (1) US4655414A (it)
JP (1) JPS62143799A (it)
AU (1) AU587512B2 (it)
BE (1) BE905870A (it)
CA (1) CA1261436A (it)
DE (1) DE3640995A1 (it)
DK (1) DK159646C (it)
FR (1) FR2591190B1 (it)
GB (1) GB2184074B (it)
GR (1) GR862804B (it)
IT (1) IT1214572B (it)
NL (1) NL8603092A (it)
NO (1) NO162754C (it)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9957057B2 (en) * 2015-07-17 2018-05-01 Embraer S.A. Aircraft throttle quadrant with a gust lock lever system provided with a selectable safety stop

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2407877A (en) * 1942-07-30 1946-09-17 Westinghouse Air Brake Co Interlock apparatus
US2793541A (en) * 1953-05-11 1957-05-28 M J Johnson Aircraft Engineeri Safety locked control handle with override
US3599510A (en) * 1969-10-06 1971-08-17 Boeing Co Controlled device comprising alternate manual or power operators
US4109547A (en) * 1977-01-17 1978-08-29 Caterpillar Tractor Co. Detent mechanism
US4454754A (en) * 1982-05-26 1984-06-19 Chandler Evans, Inc. Engine failure detector
US4567786A (en) * 1982-09-30 1986-02-04 The Boeing Company Modular multi-engine thrust control assembly
GB2132384A (en) * 1982-12-20 1984-07-04 Gen Electric Control for aircraft gas turbine engines

Also Published As

Publication number Publication date
FR2591190B1 (fr) 1988-09-09
JPS62143799A (ja) 1987-06-27
GB8628768D0 (en) 1987-01-07
NO162754C (no) 1990-02-14
NO162754B (no) 1989-11-06
US4655414A (en) 1987-04-07
DK584686A (da) 1987-06-07
NL8603092A (nl) 1987-07-01
GR862804B (en) 1987-03-10
CA1261436A (en) 1989-09-26
DK159646B (da) 1990-11-12
DK584686D0 (da) 1986-12-05
NO864852L (no) 1987-06-09
AU587512B2 (en) 1989-08-17
AU6631386A (en) 1987-06-11
BE905870A (fr) 1987-04-01
GB2184074B (en) 1989-02-08
DK159646C (da) 1991-04-15
GB2184074A (en) 1987-06-17
NO864852D0 (no) 1986-12-03
DE3640995A1 (de) 1987-06-11
FR2591190A1 (fr) 1987-06-12
IT1214572B (it) 1990-01-18

Similar Documents

Publication Publication Date Title
GB2230298B (en) Geared counterrotating turbine/fan propulsion system
FR2623250B1 (fr) Dispositif de ventilation pour la nacelle d'un moteur a turbine a gaz notamment pour un aeronef
GB8627581D0 (en) Gas turbine jet propulsion unit
IT1114372B (it) Apparecchio per montare un motore a getto in particolare sull'ala di un aeromobile
FR2591674B1 (fr) Dispositif de reglage des jeux radiaux entre rotor et stator d'un compresseur
YU45358B (en) Device for stifling blades oscilation on turbo engines
FR2589427B1 (fr) Module d'helice pour un moteur a turbine a gaz aeronautique
IT1204308B (it) Ingresso per motore di aereo
EP0219348A3 (en) Jet engine testing apparatus
IT1146870B (it) Apparecchiatura e procedimento per il controllo di motori di propulsione
GB8619881D0 (en) Increasing speed of turbo-charger on i c engine
DE3666718D1 (en) Method for the safe operation of an internal-combustion engine
EP0234055A3 (en) Method and apparatus for starting an aircraft engine
IT1228547B (it) Apparecchio e metodo per controllare i limiti di sfiancamento di motori a turbina
IT1158286B (it) Apparecchiatura per il controllo di motori di propulsione
IT8567530A0 (it) Elicottero con gruppo propulsore a turbina provvisto di dispositivo mascheratore di scarico
GB8608051D0 (en) Rpm control apparatus for i c engine
GB9018517D0 (en) Gas turbine engine drive system
IT8622586A0 (it) Apparecchio e metodo per impedire il rallentamento involontario di un motore funzionante di un aeromobile a piu' motori.
IT1188299B (it) Dispositivo di impostazione per un gruppo propulsore per aeromobili
IT1217998B (it) Dispositivo di coibentazione per l'impianto di scarico di un motore a c.i.
FR2628386B1 (fr) Systeme d'entrainement d'helice marine
IT8619848A1 (it) Metodo e apparato per controllare aerei a motori multipli
GB8619343D0 (en) Gas turbine engine & navigational system
FR2607915B1 (fr) Systeme de guidage d'engin volant

Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19941130