FR2666786B1 - Fuselages perfectionnes d'aeronefs et de missiles. - Google Patents

Fuselages perfectionnes d'aeronefs et de missiles.

Info

Publication number
FR2666786B1
FR2666786B1 FR8318889A FR8318889A FR2666786B1 FR 2666786 B1 FR2666786 B1 FR 2666786B1 FR 8318889 A FR8318889 A FR 8318889A FR 8318889 A FR8318889 A FR 8318889A FR 2666786 B1 FR2666786 B1 FR 2666786B1
Authority
FR
France
Prior art keywords
fuselages
missiles
aircraft
improved
improved fuselages
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 - Fee Related
Application number
FR8318889A
Other languages
English (en)
Other versions
FR2666786A1 (fr
Inventor
Herrington Peckham Derek
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.)
UK Government
Original Assignee
UK Government
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 UK Government filed Critical UK Government
Publication of FR2666786A1 publication Critical patent/FR2666786A1/fr
Application granted granted Critical
Publication of FR2666786B1 publication Critical patent/FR2666786B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR8318889A 1982-11-26 1983-11-25 Fuselages perfectionnes d'aeronefs et de missiles. Expired - Fee Related FR2666786B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8233864 1982-11-26

Publications (2)

Publication Number Publication Date
FR2666786A1 FR2666786A1 (fr) 1992-03-20
FR2666786B1 true FR2666786B1 (fr) 1995-05-12

Family

ID=10534568

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8318889A Expired - Fee Related FR2666786B1 (fr) 1982-11-26 1983-11-25 Fuselages perfectionnes d'aeronefs et de missiles.

Country Status (7)

Country Link
US (1) US5139215A (fr)
CA (1) CA1314764C (fr)
DE (1) DE3342861A1 (fr)
FR (1) FR2666786B1 (fr)
GB (1) GB2244968B (fr)
IT (1) IT1235222B (fr)
SE (1) SE467206B (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5322243A (en) * 1992-06-25 1994-06-21 Northrop Corporation Separately banking maneuvering aerodynamic control surfaces, system and method
US5271579A (en) * 1992-07-10 1993-12-21 Luca Nicholas J De Recreational and sport rocket construction
US5417393A (en) * 1993-04-27 1995-05-23 Hughes Aircraft Company Rotationally mounted flexible band wing
DE4337850A1 (de) * 1993-11-05 1995-05-18 Fritz Hausser Flugkörper die an der vorderen Seite die Seitenruder, Querruder und Höhenruder plaziert haben als einzige oder als Verstärkung der hinteren Ruder
US5449131A (en) * 1994-01-28 1995-09-12 Eidetics International, Inc. Vertical nose strake for aircraft stability and control
US5794887A (en) * 1995-11-17 1998-08-18 Komerath; Narayanan M. Stagnation point vortex controller
DE19837800C2 (de) * 1998-08-20 2000-06-21 Daimler Chrysler Ag Rumpfnase zur Steuerung von Fluggeräten
AUPR583001A0 (en) * 2001-06-20 2001-07-12 Kusic, Tom Aircraft spiralling mechanism
US7165742B2 (en) * 2001-06-22 2007-01-23 Tom Kusic Aircraft spiralling mechanism - B
US7637453B2 (en) * 2001-06-22 2009-12-29 Tom Kusic Aircraft spiraling mechanism with jet assistance - A
US7635104B1 (en) 2001-06-22 2009-12-22 Tom Kusic Aircraft spiraling mechanism with jet assistance—B
US7093791B2 (en) * 2001-06-22 2006-08-22 Tom Kusic Aircraft spiralling mechanism—c
AUPR982502A0 (en) * 2002-01-03 2002-01-31 Pax Fluid Systems Inc. A heat exchanger
AUPR982302A0 (en) * 2002-01-03 2002-01-31 Pax Fluid Systems Inc. A fluid flow controller
AUPR982702A0 (en) 2002-01-03 2002-01-31 Pax Fluid Systems Inc. Vortex ring generator to reduce drag on a fuselage
EP1470338A4 (fr) * 2002-01-03 2012-01-11 Pax Scient Inc Generateur d'anneau tourbillonnaire
US6796532B2 (en) * 2002-12-20 2004-09-28 Norman D. Malmuth Surface plasma discharge for controlling forebody vortex asymmetry
US6685143B1 (en) 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
AU2003903386A0 (en) * 2003-07-02 2003-07-17 Pax Scientific, Inc Fluid flow control device
CN1875193A (zh) * 2003-11-04 2006-12-06 百思科技公司 流体循环系统
EP1714039A4 (fr) * 2004-01-30 2007-05-09 Pax Scient Inc Boitier pour ventilateur, pompe ou turbine centrifuge
WO2005073560A1 (fr) * 2004-01-30 2005-08-11 Pax Scientific, Inc Rotor a flux en vortex
WO2008042251A2 (fr) 2006-09-29 2008-04-10 Pax Streamline, Inc. Ventilateur hélicoïdal
US7963442B2 (en) * 2006-12-14 2011-06-21 Simmonds Precision Products, Inc. Spin stabilized projectile trajectory control
US7642491B2 (en) * 2007-03-19 2010-01-05 Tom Kusic Aircraft spiraling mechanism with jet assistance—D
GB0803282D0 (en) 2008-02-22 2008-04-02 Qinetiq Ltd Control of projectiles or the like
US20090308472A1 (en) * 2008-06-15 2009-12-17 Jayden David Harman Swirl Inducer
WO2015198093A1 (fr) * 2014-06-24 2015-12-30 Peter Ireland Améliorations de l'efficacité des chocs de système et de corps de réglage de débit
US9857154B2 (en) * 2014-07-30 2018-01-02 The United States Of America As Represented By The Secretary Of The Army Steerable munitions projectile

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR522506A (fr) * 1918-06-19 1921-08-01 Gaston Charrasse Système de cone de pénétration placé à l'extrémité antérieure des obus employés par les canons à grande portée et ne participant pas au mouvement de rotation de l'obus
US2747816A (en) * 1950-05-11 1956-05-29 Ben O Howard Canard type airplane and controls therefor
BE552464A (fr) * 1955-11-10
US3196794A (en) * 1959-06-18 1965-07-27 Robert C Meade Piezo-electric fuse device
US3067681A (en) * 1960-01-04 1962-12-11 Telecomputing Corp Guided missile
DE1149641B (de) * 1960-06-08 1963-05-30 Pye Ltd Gelenktes Geschoss
US3195462A (en) * 1961-05-17 1965-07-20 Aerojet General Co Pull rocket shroud
US3262655A (en) * 1963-12-26 1966-07-26 Jr Warren Gillespie Alleviation of divergence during rocket launch
SE381016B (sv) * 1973-05-04 1975-11-24 S E Larson Inbordes geometrisk placering av nosvinge och huvudvinge vid flygplan eller annan farkost
IL46548A (en) * 1975-02-03 1978-06-15 Drori Mordeki Stabilized projectile with pivotable fins
US4176813A (en) * 1977-10-05 1979-12-04 Northrop Corporation Shark nose for aircraft
GB2019335A (en) * 1978-03-01 1979-10-31 Bristol Aerojet Ltd Rocket vehicles
US4198016A (en) * 1978-06-12 1980-04-15 The United States Of America As Represented By The Secretary Of The Navy Floating canard with geared tab
US4378922A (en) * 1980-04-18 1983-04-05 The Secretary Of State For Defence In Her Brittannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Aircraft having improved strake configuration
US4373688A (en) * 1981-01-19 1983-02-15 The United States Of America As Represented By The Secretary Of The Army Canard drive mechanism latch for guided projectile

Also Published As

Publication number Publication date
FR2666786A1 (fr) 1992-03-20
DE3342861A1 (de) 1992-05-07
GB2244968B (en) 1992-05-13
CA1314764C (fr) 1993-03-23
SE8306496D0 (sv) 1983-11-24
SE467206B (sv) 1992-06-15
IT8349374A0 (it) 1983-11-22
US5139215A (en) 1992-08-18
IT1235222B (it) 1992-06-26
SE8306496L (sv) 1991-11-22
GB2244968A (en) 1991-12-18

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Legal Events

Date Code Title Description
ST Notification of lapse