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FR2450198A1 - Aircraft throttle control system - has shear detector and compensator to reduce speed variation during moderate and heavy turbulence and incorporates gust bias provision - Google Patents

Aircraft throttle control system - has shear detector and compensator to reduce speed variation during moderate and heavy turbulence and incorporates gust bias provision

Info

Publication number
FR2450198A1
FR2450198A1FR7905277AFR7905277AFR2450198A1FR 2450198 A1FR2450198 A1FR 2450198A1FR 7905277 AFR7905277 AFR 7905277AFR 7905277 AFR7905277 AFR 7905277AFR 2450198 A1FR2450198 A1FR 2450198A1
Authority
FR
France
Prior art keywords
compensator
incorporates
control system
throttle control
speed variation
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
FR7905277A
Other languages
French (fr)
Other versions
FR2450198B1 (en
Inventor
Henri Peter-Contesse
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing CofiledCriticalBoeing Co
Priority to FR7905277ApriorityCriticalpatent/FR2450198A1/en
Publication of FR2450198A1publicationCriticalpatent/FR2450198A1/en
Application grantedgrantedCritical
Publication of FR2450198B1publicationCriticalpatent/FR2450198B1/fr
Grantedlegal-statusCriticalCurrent

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Abstract

The system is for processing signals representative of airspeed error and inertial longitudinal acceleration in two channels, respectively, and providing cancellation of the turbulence-induced components of the respective signals. Shear detection and compensation circuits are provided in the system for reducing speed wandering in moderate and heavy turbulence. A circuit processing the signal from the shear detector circuit is utilised to provide a gust bias signal input in the system.
FR7905277A1979-02-281979-02-28Aircraft throttle control system - has shear detector and compensator to reduce speed variation during moderate and heavy turbulence and incorporates gust bias provisionGrantedFR2450198A1 (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
FR7905277AFR2450198A1 (en)1979-02-281979-02-28Aircraft throttle control system - has shear detector and compensator to reduce speed variation during moderate and heavy turbulence and incorporates gust bias provision

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
FR7905277AFR2450198A1 (en)1979-02-281979-02-28Aircraft throttle control system - has shear detector and compensator to reduce speed variation during moderate and heavy turbulence and incorporates gust bias provision

Publications (2)

Publication NumberPublication Date
FR2450198A1true FR2450198A1 (en)1980-09-26
FR2450198B1 FR2450198B1 (en)1984-10-19

Family

ID=9222602

Family Applications (1)

Application NumberTitlePriority DateFiling Date
FR7905277AGrantedFR2450198A1 (en)1979-02-281979-02-28Aircraft throttle control system - has shear detector and compensator to reduce speed variation during moderate and heavy turbulence and incorporates gust bias provision

Country Status (1)

CountryLink
FR (1)FR2450198A1 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3840200A (en)*1973-03-191974-10-08Boeing CoTurbulence compensated throttle control system
US4209152A (en)*1977-11-251980-06-24The Boeing CompanyTurbulence compensated throttle control system for aircraft having throttle command signal path control means responsive to engine rating control and flare initiation

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3840200A (en)*1973-03-191974-10-08Boeing CoTurbulence compensated throttle control system
US4209152A (en)*1977-11-251980-06-24The Boeing CompanyTurbulence compensated throttle control system for aircraft having throttle command signal path control means responsive to engine rating control and flare initiation

Also Published As

Publication numberPublication date
FR2450198B1 (en)1984-10-19

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