GB791423A - High-lift airplane with all-moving tail plane - Google Patents

High-lift airplane with all-moving tail plane

Info

Publication number
GB791423A
GB791423A GB20011/55A GB2001155A GB791423A GB 791423 A GB791423 A GB 791423A GB 20011/55 A GB20011/55 A GB 20011/55A GB 2001155 A GB2001155 A GB 2001155A GB 791423 A GB791423 A GB 791423A
Authority
GB
United Kingdom
Prior art keywords
tail plane
aircraft
ensure
lift
control
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
GB20011/55A
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.)
HELIO AIRCRAFT CORP
Original Assignee
HELIO AIRCRAFT CORP
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 HELIO AIRCRAFT CORP filed Critical HELIO AIRCRAFT CORP
Publication of GB791423A publication Critical patent/GB791423A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/16—Stabilising surfaces adjustable about spanwise axes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)

Abstract

791,423. Controlling aircraft. HELIO AIRCRAFT CORPORATION. [July 11, 1955 July 30, 1954], No. 20011/55. Class 4. In an aircraft having a lift coefficient of at least 2-5, means to ensure a high degree of lateral and longitudinal control at low forward speeds comprise a lift spoiling flap 5 on each wing connected with an aileron 6 and associated with automatic leading edge slats 4. Such arrangement is stated to provide a rolling moment proportional to the lift coefficient. In order to ensure adequate control in pitch at low forward speeds with considerable downwash from the propeller slipstream, the tail plane 10 is pivotally movable about an axis 13 by a control 10b and an anti-balance tab 12, pivoted at 16 to the tailplane, is provided with an arm 14 slotted at 15 to co-operate with a fixed pin to ensure automatic deflection when the tail plane is deflected.
GB20011/55A 1954-07-30 1955-07-11 High-lift airplane with all-moving tail plane Expired GB791423A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US791423XA 1954-07-30 1954-07-30

Publications (1)

Publication Number Publication Date
GB791423A true GB791423A (en) 1958-03-05

Family

ID=22148704

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20011/55A Expired GB791423A (en) 1954-07-30 1955-07-11 High-lift airplane with all-moving tail plane

Country Status (1)

Country Link
GB (1) GB791423A (en)

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