ES2041516T3 - DEVICE FOR BRAKING A PUMP AFTER IT HAS GONE FROM AN AIRCRAFT. - Google Patents

DEVICE FOR BRAKING A PUMP AFTER IT HAS GONE FROM AN AIRCRAFT.

Info

Publication number
ES2041516T3
ES2041516T3 ES199090402733T ES90402733T ES2041516T3 ES 2041516 T3 ES2041516 T3 ES 2041516T3 ES 199090402733 T ES199090402733 T ES 199090402733T ES 90402733 T ES90402733 T ES 90402733T ES 2041516 T3 ES2041516 T3 ES 2041516T3
Authority
ES
Spain
Prior art keywords
bomb
cover
jet
propulsion
restoration
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 - Lifetime
Application number
ES199090402733T
Other languages
Spanish (es)
Inventor
Michel Mulleman
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
Application granted granted Critical
Publication of ES2041516T3 publication Critical patent/ES2041516T3/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Regulating Braking Force (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Valves And Accessory Devices For Braking Systems (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Braking Systems And Boosters (AREA)
  • Braking Arrangements (AREA)

Abstract

The bomb body is equipped at its rear end with a propulsion unit 3, at the outlet of which is arranged a jet collector 5 having a plurality of conduits 6 and encased in a cover 7. The cover 7 is kept in position by cables 8. Articulated on the cover 7 are traps 13 which, under the effect of the pressure of the jet issuing from the conduits 6, are unfolded forwards over a limited stroke, thereby deflecting said jet forwards in order to ensure the drag of the bomb. After a reduction in speed of the bomb, measured by a device 11, a pyrotechnic system 10 is controlled so as to ensure the severance of the cables 8 and therefore the ejection of the cover 7 and the restoration of the propulsion of the bomb. The device automatically ensures the braking back of a bomb after its release and the restoration of the propulsion of the latter when the speed of the bomb is below a predetermined value. <IMAGE>
ES199090402733T 1989-10-04 1990-10-03 DEVICE FOR BRAKING A PUMP AFTER IT HAS GONE FROM AN AIRCRAFT. Expired - Lifetime ES2041516T3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8912954A FR2652641B1 (en) 1989-10-04 1989-10-04 DEVICE FOR BRAKING A BOMB AFTER ITS RELEASE FROM AN AIRCRAFT.

Publications (1)

Publication Number Publication Date
ES2041516T3 true ES2041516T3 (en) 1993-11-16

Family

ID=9386071

Family Applications (1)

Application Number Title Priority Date Filing Date
ES199090402733T Expired - Lifetime ES2041516T3 (en) 1989-10-04 1990-10-03 DEVICE FOR BRAKING A PUMP AFTER IT HAS GONE FROM AN AIRCRAFT.

Country Status (5)

Country Link
EP (1) EP0421873B1 (en)
AT (1) ATE89073T1 (en)
DE (1) DE69001532T2 (en)
ES (1) ES2041516T3 (en)
FR (1) FR2652641B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2702556B1 (en) * 1993-03-08 1995-04-28 Giat Ind Sa Incendiary military head.
CN111023916B (en) * 2019-12-31 2020-08-04 蓝箭航天空间科技股份有限公司 Arrow body connector capture device

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE464035A (en) * 1945-03-22 1900-01-01
US2539643A (en) * 1946-05-08 1951-01-30 William R Smythe Apparatus for decelerating torpedoes
US3058304A (en) * 1959-03-02 1962-10-16 Thompson Ramo Wooldridge Inc Steering control for rocket
US3177655A (en) * 1961-01-24 1965-04-13 Thiokol Chemical Corp Rocket motor thrust termination and reversal device
DE2803036A1 (en) * 1978-01-25 1979-07-26 Messerschmitt Boelkow Blohm ARTICULATED BOMB FOR DEEP FLIGHT DEPLOYMENT

Also Published As

Publication number Publication date
FR2652641B1 (en) 1994-04-29
FR2652641A1 (en) 1991-04-05
DE69001532T2 (en) 1993-12-02
EP0421873B1 (en) 1993-05-05
DE69001532D1 (en) 1993-06-09
EP0421873A1 (en) 1991-04-10
ATE89073T1 (en) 1993-05-15

Similar Documents

Publication Publication Date Title
EP0039391A3 (en) Store carrying and launching device, especially for aircraft
ATE174565T1 (en) SHIELD LAUNCHING DEVICE
ATE36836T1 (en) EJECTION SEAT WITH PARACHUTE SYSTEM.
CA2291108A1 (en) Ring airfoil launcher
ES2041516T3 (en) DEVICE FOR BRAKING A PUMP AFTER IT HAS GONE FROM AN AIRCRAFT.
JPS59227597A (en) Capsule and rocket bailout device
ES8606634A1 (en) A no-load missile restraint arrangement.
US2940701A (en) Personnel escape equipment
SE442339B (en) ROBOT SHUTTER LOCK ORGANIZATION
US3456901A (en) Towing cable attachment mechanism for wingless towed aircraft
US3646847A (en) Slug-throwing deployment apparatus
GB1159323A (en) Fastener particularly for Anchoring Helicopters
ES2079908T3 (en) PUSH DEVICE FOR THE MOVEMENT OF ELEMENTS OF AN AUTOMOBILE FROM A NORMAL POSITION TO A SAFETY POSITION.
RU2307770C2 (en) Rotating takeoff gear
US2847964A (en) Ship&#39;s collision preventer and shock absorber
US2959416A (en) Tow member launching and recovery apparatus
GB2106225A (en) An ejector device for stores
CN214241251U (en) Throttle control device for oil-driven unmanned aerial vehicle
GB2023263A (en) A device for scattering a load of divided objects
GB1008477A (en) Improvements in or relating to protection systems for aviators
RU2096272C1 (en) Method of recovery of high-speed flying vehicle
GB982767A (en) Improvements in and relating to jet-propelled aircraft
VIALL Aerodynamic considerations for engine inlet design for subsonic high-bypass fan engines(Nacelle design for high inlet pressure recovery and low external cowl drag, for high by-pass fan engine subsonic aircraft)
GB1307730A (en) Jet propelled aircraft capable of vertical and horizontal flight
RU2105701C1 (en) Method of braking high-velocity object

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 421873

Country of ref document: ES