SE8605231L - DEVICE FOR ROADS FOR UNIT IN THE FORM OF MISSILE, PROJECTILE, AIRCRAFT ETC - Google Patents

DEVICE FOR ROADS FOR UNIT IN THE FORM OF MISSILE, PROJECTILE, AIRCRAFT ETC

Info

Publication number
SE8605231L
SE8605231L SE8605231A SE8605231A SE8605231L SE 8605231 L SE8605231 L SE 8605231L SE 8605231 A SE8605231 A SE 8605231A SE 8605231 A SE8605231 A SE 8605231A SE 8605231 L SE8605231 L SE 8605231L
Authority
SE
Sweden
Prior art keywords
unit
blades
rudder
blade
missile
Prior art date
Application number
SE8605231A
Other languages
Swedish (sv)
Other versions
SE8605231D0 (en
SE460438B (en
Inventor
T Wik
Original Assignee
Bofors Ab
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 Bofors Ab filed Critical Bofors Ab
Priority to SE8605231A priority Critical patent/SE460438B/en
Publication of SE8605231D0 publication Critical patent/SE8605231D0/en
Publication of SE8605231L publication Critical patent/SE8605231L/en
Publication of SE460438B publication Critical patent/SE460438B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The rudder surface or blade (2') is normally in a collapsed condition, but when the control signal is received it adopts at least one extended position in which it is angularly adjusted in relation to the flight direction of the airborne unit of which it forms part. The blade can be made to extend to varying degree dependent upon one or more control signals (i). Its angular adjustment when extended is between 5 and 30 deg. The airborne unit may be equipped with several rudder surfaces or blades which are positioned in front of the unit main bearer surface, vanes or wings. When the unit is manoeuvred in different directions and roll functions, the rudder surfaces or blades are activated in pairs or groups, the number of surfaces or blades being pref. four to eight.
SE8605231A 1986-12-04 1986-12-04 Rudder arrangement for missile or aeroplane SE460438B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SE8605231A SE460438B (en) 1986-12-04 1986-12-04 Rudder arrangement for missile or aeroplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE8605231A SE460438B (en) 1986-12-04 1986-12-04 Rudder arrangement for missile or aeroplane

Publications (3)

Publication Number Publication Date
SE8605231D0 SE8605231D0 (en) 1986-12-04
SE8605231L true SE8605231L (en) 1988-06-05
SE460438B SE460438B (en) 1989-10-09

Family

ID=20366534

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8605231A SE460438B (en) 1986-12-04 1986-12-04 Rudder arrangement for missile or aeroplane

Country Status (1)

Country Link
SE (1) SE460438B (en)

Also Published As

Publication number Publication date
SE8605231D0 (en) 1986-12-04
SE460438B (en) 1989-10-09

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