GB1369609A - Aircraft wing with one or more one part or multi part flaps - Google Patents

Aircraft wing with one or more one part or multi part flaps

Info

Publication number
GB1369609A
GB1369609A GB6090571A GB6090571A GB1369609A GB 1369609 A GB1369609 A GB 1369609A GB 6090571 A GB6090571 A GB 6090571A GB 6090571 A GB6090571 A GB 6090571A GB 1369609 A GB1369609 A GB 1369609A
Authority
GB
United Kingdom
Prior art keywords
flap
flaps
fixed support
aircraft wing
support bracket
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
GB6090571A
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.)
Hamburger Flugzeugbau GmbH
Original Assignee
Hamburger Flugzeugbau GmbH
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 Hamburger Flugzeugbau GmbH filed Critical Hamburger Flugzeugbau GmbH
Priority to GB6090571A priority Critical patent/GB1369609A/en
Publication of GB1369609A publication Critical patent/GB1369609A/en
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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

1369609 Aircraft flaps; deflecting propulsion jets HAMBURGER FLUGZEUGBAU GmbH 31 Dec 1971 60905/71 Heading B7G An aircraft wing 1 has a fixed support bracket 11 attached thereto, at least one flap carrier 3 pivoted to said fixed support bracket at 2 and carrying a multiple flap 5, 6 comprising also a relatively movable part 4 mounted by pivot 7 on bracket 3, a flap extending jack 12 connected between brackets 11 and 3 and connecting rods 8, 9, 10 connecting brackets 11 and 3 and flap 4. In an alternative embodiment (Figs. 3 and 4, not shown) a further hinged flap is mounted above the above described set of flaps and connected by a link to a lower flap for pivotal movement therewith and such further flap may be slotted (Figs. 5 and 6, not shown). In a still further embodiment (Figs. 7 and 8, not shown) the lower set of flaps comprise three separate interconnected elements and these may be positioned in way of the efflux from an underslung ducted fan unit driven by a separate gas generator.
GB6090571A 1971-12-31 1971-12-31 Aircraft wing with one or more one part or multi part flaps Expired GB1369609A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB6090571A GB1369609A (en) 1971-12-31 1971-12-31 Aircraft wing with one or more one part or multi part flaps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB6090571A GB1369609A (en) 1971-12-31 1971-12-31 Aircraft wing with one or more one part or multi part flaps

Publications (1)

Publication Number Publication Date
GB1369609A true GB1369609A (en) 1974-10-09

Family

ID=10486306

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6090571A Expired GB1369609A (en) 1971-12-31 1971-12-31 Aircraft wing with one or more one part or multi part flaps

Country Status (1)

Country Link
GB (1) GB1369609A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2469613A (en) * 1980-11-28 2010-10-27 Rolls Royce Plc Aircraft in which the exhaust gas is used to energise the airflow over the wing

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2469613A (en) * 1980-11-28 2010-10-27 Rolls Royce Plc Aircraft in which the exhaust gas is used to energise the airflow over the wing
US7823838B1 (en) 1980-11-28 2010-11-02 Rolls-Royce Limited Aircraft with improved lift
GB2469613B (en) * 1980-11-28 2011-03-23 Rolls Royce Plc Aircraft

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee