FR1272957A - Dispositif automatique de redressement pour avions atterrissant verticalement sur la queue - Google Patents

Dispositif automatique de redressement pour avions atterrissant verticalement sur la queue

Info

Publication number
FR1272957A
FR1272957A FR834660A FR834660A FR1272957A FR 1272957 A FR1272957 A FR 1272957A FR 834660 A FR834660 A FR 834660A FR 834660 A FR834660 A FR 834660A FR 1272957 A FR1272957 A FR 1272957A
Authority
FR
France
Prior art keywords
tail
righting device
landing vertically
automatic righting
airplanes
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.)
Expired
Application number
FR834660A
Other languages
English (en)
Inventor
Guenther Ernst
Jean Paul Joseph Jardinier
Janos Rona
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR834660A priority Critical patent/FR1272957A/fr
Priority to US128321A priority patent/US3169000A/en
Priority to GB27852/61A priority patent/GB927197A/en
Application granted granted Critical
Publication of FR1272957A publication Critical patent/FR1272957A/fr
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/063—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0091—Accessories not provided for elsewhere
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Feedback Control In General (AREA)
FR834660A 1960-08-01 1960-08-01 Dispositif automatique de redressement pour avions atterrissant verticalement sur la queue Expired FR1272957A (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR834660A FR1272957A (fr) 1960-08-01 1960-08-01 Dispositif automatique de redressement pour avions atterrissant verticalement sur la queue
US128321A US3169000A (en) 1960-08-01 1961-07-26 Automatic attitude control device for v.t.o.l.
GB27852/61A GB927197A (en) 1960-08-01 1961-08-01 Improvements in or relating to v.t.o.l. aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR834660A FR1272957A (fr) 1960-08-01 1960-08-01 Dispositif automatique de redressement pour avions atterrissant verticalement sur la queue

Publications (1)

Publication Number Publication Date
FR1272957A true FR1272957A (fr) 1961-10-06

Family

ID=8736659

Family Applications (1)

Application Number Title Priority Date Filing Date
FR834660A Expired FR1272957A (fr) 1960-08-01 1960-08-01 Dispositif automatique de redressement pour avions atterrissant verticalement sur la queue

Country Status (3)

Country Link
US (1) US3169000A (fr)
FR (1) FR1272957A (fr)
GB (1) GB927197A (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3620488A (en) * 1969-05-29 1971-11-16 Rita A Miller Aircraft command mixing device
SA05260056B1 (ar) * 1991-03-08 2008-03-26 شيفرون فيليبس كيميكال كمبني ال بي جهاز لمعالجة الهيدروكربون hydrocarbon
US5330131A (en) * 1992-05-28 1994-07-19 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Engines-only flight control system
US5413700A (en) * 1993-01-04 1995-05-09 Chevron Research And Technology Company Treating oxidized steels in low-sulfur reforming processes
CN1037765C (zh) * 1993-01-04 1998-03-18 切夫里昂化学公司 脱氢方法
USRE38532E1 (en) 1993-01-04 2004-06-08 Chevron Phillips Chemical Company Lp Hydrodealkylation processes
SA94150056B1 (ar) * 1993-01-04 2005-10-15 شيفرون ريسيرتش أند تكنولوجي كمبني عمليات لإزالة الألكلة الهيدروجينية hydrodealkylation
US6274113B1 (en) 1994-01-04 2001-08-14 Chevron Phillips Chemical Company Lp Increasing production in hydrocarbon conversion processes
US6258256B1 (en) 1994-01-04 2001-07-10 Chevron Phillips Chemical Company Lp Cracking processes
US5575902A (en) * 1994-01-04 1996-11-19 Chevron Chemical Company Cracking processes
US6419986B1 (en) 1997-01-10 2002-07-16 Chevron Phillips Chemical Company Ip Method for removing reactive metal from a reactor system
CN118859975B (zh) * 2024-09-24 2025-01-10 成都飞机工业（集团）有限责任公司 一种垂直起降无人机水平模态转换垂直模态的控制方法

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2620149A (en) * 1947-12-05 1952-12-02 Honeywell Regulator Co Aircraft control apparatus
US2701111A (en) * 1951-09-22 1955-02-01 Honeywell Regulator Co Cruise control apparatus
US2936134A (en) * 1956-03-15 1960-05-10 Sperry Rand Corp Longitudinal axis control system for aircraft

Also Published As

Publication number Publication date
US3169000A (en) 1965-02-09
GB927197A (en) 1963-05-29

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