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GB2403789A - Autonomous smart store carrier - Google Patents

Autonomous smart store carrier Download PDF

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Publication number
GB2403789A
GB2403789A GB0412765A GB0412765A GB2403789A GB 2403789 A GB2403789 A GB 2403789A GB 0412765 A GB0412765 A GB 0412765A GB 0412765 A GB0412765 A GB 0412765A GB 2403789 A GB2403789 A GB 2403789A
Authority
GB
United Kingdom
Prior art keywords
store
carrier
aircraft
management system
smart
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.)
Granted
Application number
GB0412765A
Other versions
GB0412765D0 (en
GB2403789B (en
Inventor
John Eaton
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.)
L3Harris Release and Integrated Solutions Ltd
Original Assignee
Edo MBM Technology 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 Edo MBM Technology Ltd filed Critical Edo MBM Technology Ltd
Publication of GB0412765D0 publication Critical patent/GB0412765D0/en
Publication of GB2403789A publication Critical patent/GB2403789A/en
Application granted granted Critical
Publication of GB2403789B publication Critical patent/GB2403789B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/06Rocket or torpedo launchers for rockets from aircraft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/06Rocket or torpedo launchers for rockets from aircraft
    • F41F3/065Rocket pods, i.e. detachable containers for launching a plurality of rockets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B17/00Rocket torpedoes, i.e. missiles provided with separate propulsion means for movement through air and through water
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/46Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means adapted to be launched from aircraft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B22/00Marine mines, e.g. launched by surface vessels or submarines
    • F42B22/44Marine mines, e.g. launched by surface vessels or submarines adapted to be launched from aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)

Abstract

A smart store carrier 10 for military aircraft comprises a store carriage and release system 18, and a carrier store management system 20 integrated into the store carrier so as to be installed or uninstalled as the store carrier is fitted to or removed from the aircraft. The store management system receives data from one or more sensors 22 comprising a satellite positioning system in the store carrier or store and is operatively arranged for safety management of the store. Changes of store types which necessitate changes in sensors in order to maintain store safety in flight can therefore be accommodated by changing or reconfiguring the store carrier 10 without the need for a major refit of the aircraft.

Description

BP-09-0449 2 4 0 37 8 9
AUTONOMOUS SMART STORE CARRIER
Invention Background
This invention relates to store carriers in military aircraft. Conventionally such carriers are attached to the airframe, for example beneath the wings. They are provided with a store release or ejection mechanism as well as electrical and possibly other interfaces for communication between the store and corresponding systems in the aircraft. The aircraft systems provide smart stores with electrical power and input information such as position, groundspeed, airspeed, altitude, proximity to other aircraft, etc. The interface may also lo communicate status information from the store to the pilot and programming and command information from the pilot to the store. The store input information is required for example to maintain the store in a safe condition until it is within range of a target, after which fazing or arming can take place. Different weapons systems require different input and output data so that changing or upgrading weapons systems will often require a major refit of the aircraft.
There is a tendency for smart stores to require ever more complex, diverse and comprehensive input information.
Summary of the Invention
According to the present invention, a smart store carrier comprises a store carriage and release system, a carrier store management system integrated into the store carrier so as to be installed or uninstalled as the store carrier is fitted to or removed from the aircraft, the carrier store management system receiving data from one or more sensors comprising a satellite positioning system in the store carrier or store and being operatively arranged for safety management of the store. Changes of store types which necessitate changes in sensors in order to maintain store safety in flight can therefore be accommodated by changing or reconfiguring the store carrier without the need for a major refit of the aircraft. In effect the "intelligence" required for safe carriage of the store, targeting and store launch/release is substantially removed from the aircraft airframe and integrated into the carrier. The interface between the store carrier and the aircraft is simplified and rendered relatively standard, but at the same time the interface between the store and the carrier can be relatively complex and adaptable, including a wide variety of possible sensor inputs.
BP-09-0449 Preferably the store carrier also comprises its own internal database of type-specific store safety" information for supply to the carrier store management system.
The carrier store management system may also receive data from sensors installed directly in the aircraft, i.e. external to the store carrier. For this purpose it may comprise a datalink module.
The carrier store management system may also supply store status information to the aircraft pilot, as well as receiving store arming/fuzing and/or release and/or programming lo information from the pilot. Alternatively, if desired, store arming/fuzing can be automatic, based on the sensor information received and processed by the carrier store management system.
The invention and its preferred features and advantages are further described below with reference to an illustrative embodiment shown in the single drawing figure.
Brief Description of the Drawing
Figure I is a schematic block diagram of an autonomous smart multiple store carrier (ASMSC) embodying the invention.
Description of the Preferred Embodiment
The ASMSC 10 is a multiple store carrier which provides a comprehensive electronic interface 12 to current and future carriage stores 14 whilst operating from a negligible aircraft interface 16. The ASMSC comprises three main components, these being the carriage and release system (CRS) 18 with a mechanical interface 26 for the stores 14, a central carrier stores management system (CSMS) 20 and internal carrier sensors/libraries 22.
The CSMS 20 is an aircraft equivalent flight safety critical stores management system. Its function is to take all external inputs from aircraft, stores and carrier borne sensors to provide safe communication and control of the carriage stores 14 and to provide the necessary outputs back to the aircraft.
Br94449 The internal carrier position sensors 22 consist of for example a satellite positioning system antenna and data module which can take data from a GPS or like satellite constellation and then process the data into both position and velocity data. Other acceleration, speed, position and heading sensors, for example inertial systems such as gyroscopic/accelerometer based systems, may be used in addition or in the alternative. Further sensors providing additional information necessary for safety management of the stores (for example proximity sensors) may be integrated into the carrier. This information is then fed directly to the carriage stores through the CSMS 20 as the data. alternatively, some or all of these sensors may be located in the store itself. If the carriage store 14 is not itself capable of identifying that it is in range 0 then the CSMS 20 can compare the individual weapon algorithm stored in a generic weapon database or library 24 against its current position, speed and target co-ordinates to determine whether it is in range. Once this has occurred then the CSMS signals the pilot via a tone or other signal 28 that the store is in range. If the carrier has been fully integrated onto the aircraft then it may be possible to indicate this on a HUD or HDD.
The CRS 18 is a means for store retention during flight and safe store ejection during release.
The overall ASMSC 10 is not limited by number of stations, only by the aircraft and carriage store constraints. The invention can be used for the carriage of a single store; however it is preferred that the invention is used for multiple store applications.
The ASMSC differs from a standard multiple store carrier in that the standard multiple carriage system only duplicates the aircraft/store carrier interface at the store carrier/store interface. The ASMSC is deliberately designed to operate without an aircraft stores management system capable of handling the current MIL-STD-1760/Minature Munitions or other future/legacy weapon standards. The necessary additional stores management functions are provided from within the carrier itself. Any additional sensors are provided within the carrier and/or store. The benefit to the end user is that only the store carriage system requires upgrading and not the aircraft as new weapons are added to/substituted for the overall weapon system. To gain the maximum flexibility the initial integration of the store carrier should provide a series of generic functions to the aircraft depending on the store loaded; this state is determined by the carrier itself (thereby effectively driving the system). t.
BP-090449 The overall minimum base requirements for the illustrative ASMSC to function are as follows: Aircraft Power 32 (28V DC) Release Consent 34 Signal Lines 28 (min. 2 off) If a more comprehensive aircraft signal set is available, then it is possible to allow for the stores to be reprogrammed in flight by adding an additional set of datelines, e.g. interfacing with the CSMS via a datalink module 30. These can provide the pilot with a capability to lo communicate basic weapon targeting/fuzing data to the store during flight.
Additional data is taken from the GPS sensor 22 shown in this embodiment to be mounted in the carrier rather than in the stores 14. The GPS antenna provides the additional data to determine position and heading data to provide the stores 14 with an initial fix during weapon initialization. This sensor continues to be available for additional store updates as required depending on store type and external operating conditions (i.e. jamming and store antenna masking from the airframe).
The benefits of this invention are as follows: The invention allows the carriage of stores systems which have higher data requirements than the parent aircraft alone can support.
The invention allows additional stores systems to be integrated/substituted without having to upgrade the parent aircraft.
The carrier may effect all functions except for release consent through its own sensors and weapon data.
The invention may indicate to the aircraft when the store is both correctly prepared for launch and a target is within the reach of its commanded destination. Therefore the aircraft only relays the data to the cockpit for the pilot to make the decision to release the store.
It is also possible for this concept to be used for the multiplexing of more than two weapons (i.e. 3 or more) depending on the baseline weapon carrier design. The individual weapons . BP 090449 carried simultaneously may be the same as or different from each other, with the CSMS sensor and database inputs and data outputs being adapted to the weapons concerned.

Claims (9)

BP-09-0449 CLAIMS
1. A smart store carrier for military aircraft, comprising a store carriage and release system, and a carrier store management system integrated into the store carrier so as to be installed or uninstalled as the store carrier is fitted to or removed from the aircraft, the store management system receiving data from one or more sensors comprising a satellite positioning system in the store carrier or store and being operatively arranged for safety management of the store.
2. A smart store carrier as defined in claim 1, in which the store carrier also comprises lo an internal database of type-specific store safety information for supply to the store management system.
3. A smart store carrier as defined in claim 1 or 2, in which the store management system also receives data from sensors installed directly in the aircraft.
4. A smart store carrier as defined in claim 3, comprising a datalink module.
5. A smart store carrier as defined in any preceding claim, in which the store management system may also supply store status information to the aircraft pilot.
6. A smart store carrier as defined in any preceding claim, in which the store management system receives store release and/or programming information from the pilot.
7. A smart store carrier as defined in any preceding claim, in which the store management system receives an arming/fuzing signal from the pilot.
8. A smart store carrier as defined in any of claims 1 to 6, in which store arming/fuxing is automatic, based on the sensor information received and processed by the store management system.
9. A smart store carrier for military aircraft, substantially as described with reference to or as shown in the drawing.
GB0412765A 2003-07-07 2004-06-08 Autonomous smart store carrier Expired - Lifetime GB2403789B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0316074A GB0316074D0 (en) 2003-07-07 2003-07-07 Autonomous smart store carrier

Publications (3)

Publication Number Publication Date
GB0412765D0 GB0412765D0 (en) 2004-07-07
GB2403789A true GB2403789A (en) 2005-01-12
GB2403789B GB2403789B (en) 2005-08-24

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Family Applications (2)

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GB0316074A Ceased GB0316074D0 (en) 2003-07-07 2003-07-07 Autonomous smart store carrier
GB0412765A Expired - Lifetime GB2403789B (en) 2003-07-07 2004-06-08 Autonomous smart store carrier

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Application Number Title Priority Date Filing Date
GB0316074A Ceased GB0316074D0 (en) 2003-07-07 2003-07-07 Autonomous smart store carrier

Country Status (2)

Country Link
FR (1) FR2857329B1 (en)
GB (2) GB0316074D0 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006007142A1 (en) * 2006-02-16 2007-08-30 Lfk-Lenkflugkörpersysteme Gmbh Unmanned missile and method for determining the position of an unmanned missile which can be uncoupled from an aircraft
EP3540362A1 (en) * 2018-03-12 2019-09-18 Textron Systems Corporation 1-to-n munitions adaptor for an airborne platform

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182126A (en) * 1985-10-23 1987-05-07 Messerschmitt Boelkow Blohm Aircraft weapon suspension means
GB2280736A (en) * 1989-07-06 1995-02-08 Ml Aviat Ltd Store ejector
US5855339A (en) * 1997-07-07 1999-01-05 Raytheon Company System and method for simultaneously guiding multiple missiles
US6254031B1 (en) * 1994-08-24 2001-07-03 Lockhead Martin Corporation Precision guidance system for aircraft launched bombs

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4246472A (en) * 1978-12-18 1981-01-20 The United States Of America As Represented By The Secretary Of The Navy Controlled store separation system
FR2712676A1 (en) * 1989-07-06 1995-05-24 Ml Aviat Ltd Store ejector for releasing missile from aircraft
IL95990A (en) * 1990-10-15 1994-07-31 B V R Technologies Ltd Anti-collision warning system
US6755372B2 (en) * 2001-12-18 2004-06-29 The Boeing Company Air launch system interface

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182126A (en) * 1985-10-23 1987-05-07 Messerschmitt Boelkow Blohm Aircraft weapon suspension means
GB2280736A (en) * 1989-07-06 1995-02-08 Ml Aviat Ltd Store ejector
US6254031B1 (en) * 1994-08-24 2001-07-03 Lockhead Martin Corporation Precision guidance system for aircraft launched bombs
US5855339A (en) * 1997-07-07 1999-01-05 Raytheon Company System and method for simultaneously guiding multiple missiles

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006007142A1 (en) * 2006-02-16 2007-08-30 Lfk-Lenkflugkörpersysteme Gmbh Unmanned missile and method for determining the position of an unmanned missile which can be uncoupled from an aircraft
US7960675B2 (en) 2006-02-16 2011-06-14 Lfk-Lenkflugkoerpersysteme Gmbh Unmanned missile and method for determining the position of an unmanned missile which may be uncoupled from an aircraft
DE102006007142B4 (en) * 2006-02-16 2014-12-18 Mbda Deutschland Gmbh Method for determining the position of an unmanned aerial vehicle which can be decoupled from an aircraft
EP3540362A1 (en) * 2018-03-12 2019-09-18 Textron Systems Corporation 1-to-n munitions adaptor for an airborne platform
US11460273B2 (en) 2018-03-12 2022-10-04 Textron Systems Corporation 1-to-N munitions adapter for an airborne platform

Also Published As

Publication number Publication date
FR2857329A1 (en) 2005-01-14
GB0412765D0 (en) 2004-07-07
GB0316074D0 (en) 2004-06-16
FR2857329B1 (en) 2009-03-06
GB2403789B (en) 2005-08-24

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