GB985567A - Spoiler mechanism for guiding aircraft or missiles at supersonic speed - Google Patents

Spoiler mechanism for guiding aircraft or missiles at supersonic speed

Info

Publication number
GB985567A
GB985567A GB2579561A GB2579561A GB985567A GB 985567 A GB985567 A GB 985567A GB 2579561 A GB2579561 A GB 2579561A GB 2579561 A GB2579561 A GB 2579561A GB 985567 A GB985567 A GB 985567A
Authority
GB
United Kingdom
Prior art keywords
spoiler
width
aerodynamic surface
zone
missiles
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
GB2579561A
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
Publication of GB985567A publication Critical patent/GB985567A/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
    • F42B10/02—Stabilising arrangements
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins
    • 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
    • B64C9/326—Air braking surfaces associated with fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

985,567. Ammunition. L. BOLKOW, [trading as BOLKOW ENTWICKLUNGEN KOMM.-GES.]. July 17, 1961 [July 19, 1960], No. 25795/61. Heading F3A. [Also in Division B7] A spoiler mechanism for aircraft or missiles capable of travelling at supersonic speeds comprises a surface 16 disposed perpendicularly to an aerodynamic surface 15 and spaced therefrom so that a pressure wedge is unable to build up immediately in front of the mechanism and thus the shock wave 18 is vertical. The spacer is spaced from the trailing edge of the aerodynamic surface by a distance equal to the depth of the high pressure zone behind the spoiler, caused by the shock wave. The width of the gap 17 may vary between the width of the spoiler and three times this width. The spoiler may be retractable into the aerodynamic surface. Channels may be provided and extend from the zone forward of the spoiler to a zone rearward to prevent pressure build-up forward. Fig. 4 shows spoilers 26, 27 retractively mounted in the nose 30 of a missile and arranged adjacent surfaces 31.
GB2579561A 1960-07-19 1961-07-17 Spoiler mechanism for guiding aircraft or missiles at supersonic speed Expired GB985567A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB58650A DE1122838B (en) 1960-07-19 1960-07-19 Spoiler for controlling aircraft with supersonic speed

Publications (1)

Publication Number Publication Date
GB985567A true GB985567A (en) 1965-03-10

Family

ID=6972157

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2579561A Expired GB985567A (en) 1960-07-19 1961-07-17 Spoiler mechanism for guiding aircraft or missiles at supersonic speed

Country Status (2)

Country Link
DE (1) DE1122838B (en)
GB (1) GB985567A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2570447A1 (en) * 1984-09-19 1986-03-21 Bigeon Pierre Projectile comprising longitudinal devices for improving the hydrodynamic or aerodynamic lift and drag
CN114486159A (en) * 2021-12-30 2022-05-13 中国航天空气动力技术研究院 Control and verification method for embedded weapon machine bomb separation compatibility front edge sawtooth spoiler

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1269500B (en) * 1962-11-16 1968-05-30 Ver Flugtechnische Werke Ges M Flap for aircraft
US5564652A (en) * 1995-01-03 1996-10-15 The Boeing Compay Body spoiler for yaw control of a supersonic airplane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2570447A1 (en) * 1984-09-19 1986-03-21 Bigeon Pierre Projectile comprising longitudinal devices for improving the hydrodynamic or aerodynamic lift and drag
CN114486159A (en) * 2021-12-30 2022-05-13 中国航天空气动力技术研究院 Control and verification method for embedded weapon machine bomb separation compatibility front edge sawtooth spoiler

Also Published As

Publication number Publication date
DE1122838B (en) 1962-01-25

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