FR2176074A1 - - Google Patents

Info

Publication number
FR2176074A1
FR2176074A1 FR7309195A FR7309195A FR2176074A1 FR 2176074 A1 FR2176074 A1 FR 2176074A1 FR 7309195 A FR7309195 A FR 7309195A FR 7309195 A FR7309195 A FR 7309195A FR 2176074 A1 FR2176074 A1 FR 2176074A1
Authority
FR
France
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
FR7309195A
Other languages
French (fr)
Other versions
FR2176074B1 (en:Method
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of FR2176074A1 publication Critical patent/FR2176074A1/fr
Application granted granted Critical
Publication of FR2176074B1 publication Critical patent/FR2176074B1/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Platform Screen Doors And Railroad Systems (AREA)
FR7309195A 1972-03-14 1973-03-14 Expired FR2176074B1 (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1182872A GB1379814A (en) 1972-03-14 1972-03-14 Aircraft wing flaps

Publications (2)

Publication Number Publication Date
FR2176074A1 true FR2176074A1 (en:Method) 1973-10-26
FR2176074B1 FR2176074B1 (en:Method) 1977-02-04

Family

ID=9993453

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7309195A Expired FR2176074B1 (en:Method) 1972-03-14 1973-03-14

Country Status (3)

Country Link
US (1) US3880384A (en:Method)
FR (1) FR2176074B1 (en:Method)
GB (1) GB1379814A (en:Method)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112193424A (zh) * 2020-10-19 2021-01-08 中南大学 一种基于非常规布局的外吹式动力增升系统

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5214025B2 (ja) * 2008-05-09 2013-06-19 ザ・ボーイング・カンパニー 固定部及び可動部を有する航空機のフィレット・フェアリング、及び関連システム及び方法
US20150233298A1 (en) * 2012-09-28 2015-08-20 United Technologies Corporation Reduction in jet flap interaction noise with geared turbine engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1759164A (en) * 1928-03-06 1930-05-20 James G Lyons Aeroplane
US1773281A (en) * 1929-05-06 1930-08-19 Rossiter S Scott Aircraft
US2120760A (en) * 1935-01-19 1938-06-14 Lumiere Henri Supporting surface of airplanes and the like aircraft
US3614028A (en) * 1970-01-12 1971-10-19 Mc Donnell Douglas Corp Turbofan-powered stol aircraft

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112193424A (zh) * 2020-10-19 2021-01-08 中南大学 一种基于非常规布局的外吹式动力增升系统

Also Published As

Publication number Publication date
FR2176074B1 (en:Method) 1977-02-04
GB1379814A (en) 1975-01-08
US3880384A (en) 1975-04-29

Similar Documents

Publication Publication Date Title
JPS4984720A (en:Method)
JPS4955284A (en:Method)
JPS4963994U (en:Method)
CH568174A5 (en:Method)
BG18227A1 (en:Method)
BG18442A1 (en:Method)
BG26793A1 (en:Method)
CH545685A (en:Method)
CH560800A (en:Method)
CH562773A5 (en:Method)
CH563035A (en:Method)
CH563951A5 (en:Method)
CH564129A5 (en:Method)
CH565143A5 (en:Method)
CH565149A5 (en:Method)
CH565228A5 (en:Method)
CH565324A5 (en:Method)
CH568356A5 (en:Method)
CH570154A5 (en:Method)
CH572051A5 (en:Method)
CH572741A5 (en:Method)
CH573290A5 (en:Method)
CH573495B5 (en:Method)
CH573699A5 (en:Method)
CH573945A5 (en:Method)

Legal Events

Date Code Title Description
ST Notification of lapse