GB711637A - Improvements relating to adjustable stabilisers or tailplanes for aircraft - Google Patents

Improvements relating to adjustable stabilisers or tailplanes for aircraft

Info

Publication number
GB711637A
GB711637A GB8052A GB8052A GB711637A GB 711637 A GB711637 A GB 711637A GB 8052 A GB8052 A GB 8052A GB 8052 A GB8052 A GB 8052A GB 711637 A GB711637 A GB 711637A
Authority
GB
United Kingdom
Prior art keywords
aircraft
speed
tailplane
adjustable
incidence
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
GB8052A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB8052A priority Critical patent/GB711637A/en
Publication of GB711637A publication Critical patent/GB711637A/en
Expired legal-status Critical Current

Links

Classifications

    • 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 Control Devices (AREA)

Abstract

711,637. Controlling aircraft. DABROWSKI, J. Jan. 1, 1952, No. 80/52. Class 4 An adjustable tailplane'for aircraft consists of a tailplane a pivotally mounted about an axis b disposed rearwardly of but not beneath the centre of pressure of the tailplane when the aircraft is in its normal level flying position. Resilient means. e.g. a compression spring c, are provided for opposing the pitching torque exerted by the airstream on the tailplane about the axis b. The negative angle of incidence of the surface is varied by the airspeed, so that an increase in speed will increase the negative angle of incidence, and the aircraft will climb and thus lose speed. Similarly a reduction in speed will result in a dive with consequent gain in speed. Manual control e may be provided which may override the automatic control. The latter may be detached by the pilot during flight. An adjustable device d is provided to predetermine the stable speed of the aircraft.
GB8052A 1952-01-01 1952-01-01 Improvements relating to adjustable stabilisers or tailplanes for aircraft Expired GB711637A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8052A GB711637A (en) 1952-01-01 1952-01-01 Improvements relating to adjustable stabilisers or tailplanes for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8052A GB711637A (en) 1952-01-01 1952-01-01 Improvements relating to adjustable stabilisers or tailplanes for aircraft

Publications (1)

Publication Number Publication Date
GB711637A true GB711637A (en) 1954-07-07

Family

ID=9698057

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8052A Expired GB711637A (en) 1952-01-01 1952-01-01 Improvements relating to adjustable stabilisers or tailplanes for aircraft

Country Status (1)

Country Link
GB (1) GB711637A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2405869A1 (en) * 1977-10-17 1979-05-11 Onera (Off Nat Aerospatiale) Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed
DE2914951A1 (en) * 1979-04-12 1980-10-30 Onera (Off Nat Aerospatiale) Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed
GB2230748A (en) * 1986-03-03 1990-10-31 Diehl Gmbh & Co Guidance mechanism for projectiles

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2405869A1 (en) * 1977-10-17 1979-05-11 Onera (Off Nat Aerospatiale) Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed
DE2914951A1 (en) * 1979-04-12 1980-10-30 Onera (Off Nat Aerospatiale) Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed
GB2230748A (en) * 1986-03-03 1990-10-31 Diehl Gmbh & Co Guidance mechanism for projectiles
GB2230748B (en) * 1986-03-03 1991-03-20 Diehl Gmbh & Co Projectile guidance apparatus.

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