EP2042827A2 - Military aircraft bomb arming system - Google Patents

Military aircraft bomb arming system Download PDF

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Publication number
EP2042827A2
EP2042827A2 EP08253089A EP08253089A EP2042827A2 EP 2042827 A2 EP2042827 A2 EP 2042827A2 EP 08253089 A EP08253089 A EP 08253089A EP 08253089 A EP08253089 A EP 08253089A EP 2042827 A2 EP2042827 A2 EP 2042827A2
Authority
EP
European Patent Office
Prior art keywords
bomb
arming
fuze
pulse
signal conditioning
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.)
Withdrawn
Application number
EP08253089A
Other languages
German (de)
French (fr)
Other versions
EP2042827A3 (en
Inventor
Graeme Nicholas Snowden
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.)
Portsmouth Aviation Ltd
Original Assignee
Portsmouth Aviation Ltd
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 Portsmouth Aviation Ltd filed Critical Portsmouth Aviation Ltd
Publication of EP2042827A2 publication Critical patent/EP2042827A2/en
Publication of EP2042827A3 publication Critical patent/EP2042827A3/en
Withdrawn legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/005Combination-type safety mechanisms, i.e. two or more safeties are moved in a predetermined sequence to each other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00Electric fuzes
    • F42C11/001Electric circuits for fuzes characterised by the ammunition class or type
    • F42C11/006Electric circuits for fuzes characterised by the ammunition class or type for fall bombs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/28Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
    • F42C15/295Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids operated by a turbine or a propeller; Mounting means therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/40Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected electrically
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C17/00Fuze-setting apparatus
    • F42C17/04Fuze-setting apparatus for electric fuzes

Definitions

  • This invention relates to a military aircraft bomb arming system, and to a bomb fuze adapter.
  • the current UK bomb fuze has both electrical arming, provided by a Lead Electrical Fuze Arming (LEFA) electrical pulse, and mechanical arming by the rotation of an arming vane on the rear of the bomb tail.
  • LEFA Lead Electrical Fuze Arming
  • the invention stems from some work aimed at enabling UK military aircraft to benefit from the utility offered by some of these international fuzes by providing additional arming safety.
  • fuzes utilise an air driven turbine alternator to provide electrical power to arm the fuze of the bomb after release of the bomb from the aircraft, but do not provide an additional means of safety up to the moment of release.
  • an electrical signal is generated by the aircraft at the moment of bomb release that is conditional upon the mechanical unlocking of the aircraft's bomb release unit and hence the separation of the bomb from the aircraft.
  • This signal is directed from the aircraft to the fuze via a LEFA Cable and provides the first arming environment; the second arming environment being produced by the rotation of the arming vane.
  • this LEFA pulse can be harnessed and modified through the medium of a signal conditioning unit to provide the first arming environment for bombs provided with international fuzes, with the second arming environment being provided after release by the air driven turbine alternator of the international fuze.
  • a military aircraft bomb arming system suitable for use with an aircraft that is provided with a Lead Electrical Fuze Arming (LEFA) pulse generator that is configured for use with a bomb fuze of the kind having both electrical and mechanical fuze arming means, the system comprising a signal conditioning unit adapted to be connected between said pulse generator and a bomb fuze of a second kind that is intended to be armed by an air driven turbine alternator, the signal conditioning unit being adapted to convert, in use, a LEFA pulse from the pulse generator into a modified pulse suitable for providing a first arming environment to the bomb fuze of the second kind.
  • LEFA Lead Electrical Fuze Arming
  • the signal conditioning unit is preferably so configured to take the aircraft's LEFA pulse (of "X” voltage, current and pulse length), generated at bomb release, and modify it electronically to provide the first arming environment for the bomb fuze of the second kind (of "Y" voltage, current and pulse length). After a short delay, the air driven turbine alternator will run up to speed, driven by the airflow over the bomb, and provide the second arming environment that then allows the fuze to arm.
  • the signal conditioning unit requires no independent power supply since it need only modify the existing LEFA pulse generated at bomb release.
  • the signal conditioning unit may conveniently be incorporated within the fuze's own electrical cable harness.
  • the LEFA pulse generator In use, when the bomb is mechanically released from the bomb release unit of the aircraft, the LEFA pulse generator sends a standard LEFA pulse to the signal conditioning unit on the bomb.
  • the signal conditioning unit comprises power supply electronics that convert the LEFA pulse to a power suitable to supply a generator for modifying the pulse to a power and duration required for the international bomb fuze of the second kind.
  • the signal conditioning unit may include pulse isolation electronics that, where necessary, isolate the modified pulse from the initial LEFA input by means of a pulse transformer or the like.
  • the modified pulse is then fed to the international bomb fuze of the second kind to provide a first arming environment, the second arming environment being provided subsequently by air flow through an air driven turbine or the like on the bomb.
  • the second arming environment may be mechanical as described, or electrical.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

A military aircraft bomb arming system suitable for use with an aircraft that is provided with a Lead Electrical Fuze Arming (LEFA) pulse generator that is configured for use with a bomb fuze of the kind having both electrical and mechanical fuze arming means is provided. The system comprises a signal conditioning unit adapted to be connected between said pulse generator and a bomb fuze of a second kind that is intended to be armed by an air driven turbine alternator. The signal conditioning unit is adapted to convert, in use, a LEFA pulse from the pulse generator into a modified pulse suitable for providing a first arming environment to the bomb fuze of the second kind.
The system thus enables UK military aircraft to benefit from the utility offered by some of these international fuzes by providing additional arming safey.

Description

  • This invention relates to a military aircraft bomb arming system, and to a bomb fuze adapter.
  • Current UK military aircraft bomb fuzes are required to provide safety through the inclusion of multiple arming environments. Typically these require both mechanical and electrical/electronic means to ensure weapons are not armed whilst the bomb is in carried flight. These are known as the first and second arming environments.
  • The current UK bomb fuze has both electrical arming, provided by a Lead Electrical Fuze Arming (LEFA) electrical pulse, and mechanical arming by the rotation of an arming vane on the rear of the bomb tail.
  • The majority of other bomb fuzes manufactured internationally are electronic in nature and do not provide the same mechanical safety.
  • The invention stems from some work aimed at enabling UK military aircraft to benefit from the utility offered by some of these international fuzes by providing additional arming safety.
  • Most internationally available fuzes utilise an air driven turbine alternator to provide electrical power to arm the fuze of the bomb after release of the bomb from the aircraft, but do not provide an additional means of safety up to the moment of release.
  • On UK military aircraft, an electrical signal, the LEFA pulse, is generated by the aircraft at the moment of bomb release that is conditional upon the mechanical unlocking of the aircraft's bomb release unit and hence the separation of the bomb from the aircraft.
  • This signal is directed from the aircraft to the fuze via a LEFA Cable and provides the first arming environment; the second arming environment being produced by the rotation of the arming vane.
  • We have realised that this LEFA pulse can be harnessed and modified through the medium of a signal conditioning unit to provide the first arming environment for bombs provided with international fuzes, with the second arming environment being provided after release by the air driven turbine alternator of the international fuze.
  • According to one aspect of the invention we provide a military aircraft bomb arming system suitable for use with an aircraft that is provided with a Lead Electrical Fuze Arming (LEFA) pulse generator that is configured for use with a bomb fuze of the kind having both electrical and mechanical fuze arming means, the system comprising a signal conditioning unit adapted to be connected between said pulse generator and a bomb fuze of a second kind that is intended to be armed by an air driven turbine alternator, the signal conditioning unit being adapted to convert, in use, a LEFA pulse from the pulse generator into a modified pulse suitable for providing a first arming environment to the bomb fuze of the second kind.
  • Thus the signal conditioning unit is preferably so configured to take the aircraft's LEFA pulse (of "X" voltage, current and pulse length), generated at bomb release, and modify it electronically to provide the first arming environment for the bomb fuze of the second kind (of "Y" voltage, current and pulse length). After a short delay, the air driven turbine alternator will run up to speed, driven by the airflow over the bomb, and provide the second arming environment that then allows the fuze to arm.
  • Preferably the signal conditioning unit requires no independent power supply since it need only modify the existing LEFA pulse generated at bomb release. The signal conditioning unit may conveniently be incorporated within the fuze's own electrical cable harness.
  • One embodiment of the invention will now be described, by way of the example only, with reference to the accompanying drawings in which:
    • Figure 1 is a schematic side elevation of a bomb that has just been released from the bomb release unit of a UK military aircraft, the bomb fuze being connected to a signal conditioning unit in accordance with the invention,
    • Figure 2 is a flow chart showing the stages in releasing the bomb and providing the first arming environment of the bomb fuze, and
    • Figure 3 is a functional block diagram of the signal conditioning unit in accordance with the invention.
  • In use, when the bomb is mechanically released from the bomb release unit of the aircraft, the LEFA pulse generator sends a standard LEFA pulse to the signal conditioning unit on the bomb.
  • The signal conditioning unit comprises power supply electronics that convert the LEFA pulse to a power suitable to supply a generator for modifying the pulse to a power and duration required for the international bomb fuze of the second kind.
  • The signal conditioning unit may include pulse isolation electronics that, where necessary, isolate the modified pulse from the initial LEFA input by means of a pulse transformer or the like.
  • The modified pulse is then fed to the international bomb fuze of the second kind to provide a first arming environment, the second arming environment being provided subsequently by air flow through an air driven turbine or the like on the bomb.
  • It will be appreciated that the second arming environment may be mechanical as described, or electrical.

Claims (5)

  1. A military aircraft bomb arming system suitable for use with an aircraft that is provided with a Lead Electrical Fuze Arming (LEFA) pulse generator that is configured for use with a bomb fuze of the kind having both electrical and mechanical fuze arming means, the system comprising a signal conditioning unit adapted to be connected between said pulse generator and a bomb fuze of a second kind that is intended to be armed by an air driven turbine alternator, the signal conditioning unit being adapted to convert, in use, a LEFA pulse from the pulse generator into a modified pulse suitable for providing a first arming environment to the bomb fuze of the second kind.
  2. The military aircraft bomb arming system of claim 1 wherein the signal conditioning unit is so configured to take the aircraft's LEFA pulse (of "X" voltage, current and pulse length), generated at bomb release, and modify it electronically to provide the first arming environment for the bomb fuze of the second kind (of "Y" voltage, current and pulse length).
  3. The military aircraft bomb arming system of claim 2 configured such that, in use, after a short delay, the air driven turbine alternator will run up to speed, driven by the airflow over the bomb, to provide the second arming environment that then allows the fuze to arm.
  4. The military aircraft bomb arming system of claim 2 or claim 3 wherein the signal conditioning unit requires no independent power supply.
  5. The military aircraft bomb arming system of claim 2, claim 3 or claim 4 wherein the signal conditioning unit is incorporated within the fuze's own electrical cable harness.
EP08253089A 2007-09-27 2008-09-20 Military aircraft bomb arming system Withdrawn EP2042827A3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0718881A GB2455490A (en) 2007-09-27 2007-09-27 Military aircraft bomb arming system

Publications (2)

Publication Number Publication Date
EP2042827A2 true EP2042827A2 (en) 2009-04-01
EP2042827A3 EP2042827A3 (en) 2010-11-17

Family

ID=38701770

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EP08253089A Withdrawn EP2042827A3 (en) 2007-09-27 2008-09-20 Military aircraft bomb arming system

Country Status (2)

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EP (1) EP2042827A3 (en)
GB (1) GB2455490A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019150080A1 (en) * 2018-02-02 2019-08-08 Portsmouth Aviation Limited Weapon delivery system
EP3605006A1 (en) * 2018-07-30 2020-02-05 Thales Holdings UK Plc A safety and arming unit for a munition

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107782206A (en) * 2017-11-22 2018-03-09 中国工程物理研究院电子工程研究所 A kind of aerial guided bomb fuse and its environmental information recognition methods based on mems accelerometer

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4586436A (en) * 1984-09-13 1986-05-06 The United States Of America As Represented By The Secretary Of The Navy Electronic assembly for moderate hard target penetrator fuze
US4936187A (en) * 1989-04-20 1990-06-26 The United States Of America As Represented By The Secretary Of The Navy Wire-free arming system for an aircraft-delivered bomb

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3757695A (en) * 1969-12-19 1973-09-11 Us Army Charging system for electric bomb fuzes (u)

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4586436A (en) * 1984-09-13 1986-05-06 The United States Of America As Represented By The Secretary Of The Navy Electronic assembly for moderate hard target penetrator fuze
US4936187A (en) * 1989-04-20 1990-06-26 The United States Of America As Represented By The Secretary Of The Navy Wire-free arming system for an aircraft-delivered bomb

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019150080A1 (en) * 2018-02-02 2019-08-08 Portsmouth Aviation Limited Weapon delivery system
EP3605006A1 (en) * 2018-07-30 2020-02-05 Thales Holdings UK Plc A safety and arming unit for a munition
US11280600B2 (en) 2018-07-30 2022-03-22 Thales Holdings Uk Plc Safety and arming unit for a munition

Also Published As

Publication number Publication date
GB0718881D0 (en) 2007-11-07
EP2042827A3 (en) 2010-11-17
GB2455490A (en) 2009-06-17

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