GB620860A - Aircraft wing flap assembly - Google Patents

Aircraft wing flap assembly

Info

Publication number
GB620860A
GB620860A GB249647A GB249647A GB620860A GB 620860 A GB620860 A GB 620860A GB 249647 A GB249647 A GB 249647A GB 249647 A GB249647 A GB 249647A GB 620860 A GB620860 A GB 620860A
Authority
GB
United Kingdom
Prior art keywords
rods
rod
flap
hydraulic jack
radius
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
GB249647A
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.)
WILLARD HARVEY MOORE
Original Assignee
WILLARD HARVEY MOORE
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 WILLARD HARVEY MOORE filed Critical WILLARD HARVEY MOORE
Priority to GB249647A priority Critical patent/GB620860A/en
Publication of GB620860A publication Critical patent/GB620860A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/32Air braking surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/32Air braking surfaces
    • B64C9/323Air braking surfaces associated with wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)

Abstract

620,860. Wing flaps. MOORE, W. H. Jan. 27, 1947, No. 2496. [Class 4] A flap comprises three or more pivotally interconnected spanwise strips forming an articulated unit pivotally attached along one edge 42 to the wing 1, the flap being raised or lowered by a series of radius rods 15, 16, 17, 18 actuated by a hydraulic jack 6, 7. The rod 6 of the jack carries a cross-piece 9 to which rods 10, 11, 12, 13 are attached. The rod 10 carries a member 31 to which the lower end of the radius rod 15 is pivoted, while the rods 11, 12, 13 carry further members 32, 33, 34 which successively engage blocks 24, 25, 26, to which the rods 16, 17, 18 are pivoted, when the hydraulic jack is extended. Projections at the upper ends of the members 31, 32, 33, 34 engage the rear faces of the radius rods when the flap is fully raised, Fig. 5. Manually operated rack and pinion, or screw drive, may be substituted for the hydraulic jack.
GB249647A 1947-01-27 1947-01-27 Aircraft wing flap assembly Expired GB620860A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB249647A GB620860A (en) 1947-01-27 1947-01-27 Aircraft wing flap assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB249647A GB620860A (en) 1947-01-27 1947-01-27 Aircraft wing flap assembly

Publications (1)

Publication Number Publication Date
GB620860A true GB620860A (en) 1949-03-31

Family

ID=9740590

Family Applications (1)

Application Number Title Priority Date Filing Date
GB249647A Expired GB620860A (en) 1947-01-27 1947-01-27 Aircraft wing flap assembly

Country Status (1)

Country Link
GB (1) GB620860A (en)

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