GB1036033A - Device for the aerodynamic control of missiles - Google Patents

Device for the aerodynamic control of missiles

Info

Publication number
GB1036033A
GB1036033A GB11658/64A GB1165864A GB1036033A GB 1036033 A GB1036033 A GB 1036033A GB 11658/64 A GB11658/64 A GB 11658/64A GB 1165864 A GB1165864 A GB 1165864A GB 1036033 A GB1036033 A GB 1036033A
Authority
GB
United Kingdom
Prior art keywords
vanes
vaned
end plates
aerodynamic
missile
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
GB11658/64A
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.)
Bolkow GmbH
Original Assignee
Bolkow 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 Bolkow GmbH filed Critical Bolkow GmbH
Publication of GB1036033A publication Critical patent/GB1036033A/en
Expired legal-status Critical Current

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
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/02—Influencing air flow over aircraft surfaces, not otherwise provided for by means of rotating members of cylindrical or similar form
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Braking Arrangements (AREA)

Abstract

1,036,033. Controlling aircraft. BOLKOW, G.m.b.H. March 19, 1964 [March 26, 1963], No. 11658/64. Heading B7G. An aerodynamic control device for the control of missiles comprises spoilers which are rotatable by air flow and which can be braked and have axes of rotation parallel to aerodynamic surfaces of the missile and transverse to the direction of airflow, and have blades which are arranged to enter recesses in the aerodynamic surfaces of the missile. A wing 1 (Fig. 1, not shown) having opposed surfaces 2 and 3 has mountings for freely rotatable vaned members 6 and 7 respectively, so positioned in cut-outs 4 and 5 that their axes lie substantially in the plane of the respective surfaces. The upper member comprises a plurality of vanes 10 attached to circular end plates 12, 13 carried by pivots 8, 9 and the lower member is similarly constructed with end plates 14, 15. An electromagnetic device, comprising an armature 24 mounted on a pivot 34 and stabilized in a central position by a tension spring 38, is provided to retard one vaned member or the other, brake pads 36, 37 being arranged to bear against end plate 12 or 14 when the appropriate coil 28 or 29 is energized. A solenoid 17 is positioned at the other end of the vaned members to attract an armature 42 against the action of a spring 45 to apply simultaneously brake pads 43, 44 against end plates 13, 15. By this means either or both of the vaned members may be held against free rotation to act as control spoilers. Other embodiments are described in which two planar vanes are geared together for free rotation in opposite directions with the planes of the vanes mutually at right angles, solenoidoperated sprags being provided to engage the gear teeth to hold the vanes so that one is in the plane of the corresponding wing surface and the other is normal to its corresponding surface.
GB11658/64A 1963-03-26 1964-03-19 Device for the aerodynamic control of missiles Expired GB1036033A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB71300A DE1264264B (en) 1963-03-26 1963-03-26 Device for the aerodynamic control of flying bodies

Publications (1)

Publication Number Publication Date
GB1036033A true GB1036033A (en) 1966-07-13

Family

ID=6976983

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11658/64A Expired GB1036033A (en) 1963-03-26 1964-03-19 Device for the aerodynamic control of missiles

Country Status (3)

Country Link
CH (1) CH422529A (en)
DE (1) DE1264264B (en)
GB (1) GB1036033A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0264529A1 (en) * 1986-08-19 1988-04-27 Rheinmetall GmbH Missile with a stabilizing device
JP2018510995A (en) * 2015-04-10 2018-04-19 ヴォッベン プロパティーズ ゲーエムベーハーＷｏｂｂｅｎ Ｐｒｏｐｅｒｔｉｅｓ Ｇｍｂｈ Wind power generator-rotor blade

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR597674A (en) * 1924-05-06 1925-11-26 Method and device for preventing the formation of vortices on bodies bathed in a current
DE542471C (en) * 1929-08-06 1932-01-25 Kaeser Ernst Device to increase the transverse drive and to prevent the air flow from being released on the upper side of aircraft wings
US2705934A (en) * 1951-05-22 1955-04-12 Kefeli Michel Mourad Stabilizing device for ships
FR1104006A (en) * 1952-04-23 1955-11-15 Improvements to airfoil bearing surfaces
US2896880A (en) * 1954-01-13 1959-07-28 Raymond D Vogler Rotary spoilers for use in lateral control of an airplane

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0264529A1 (en) * 1986-08-19 1988-04-27 Rheinmetall GmbH Missile with a stabilizing device
US4903917A (en) * 1986-08-19 1990-02-27 Rheinmetall Gmbh Projectile with rotatable stabilizing device
JP2018510995A (en) * 2015-04-10 2018-04-19 ヴォッベン プロパティーズ ゲーエムベーハーＷｏｂｂｅｎ Ｐｒｏｐｅｒｔｉｅｓ Ｇｍｂｈ Wind power generator-rotor blade

Also Published As

Publication number Publication date
DE1264264B (en) 1968-03-21
CH422529A (en) 1966-10-15

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