Fuse system for projectile

Patent metadata

Field	Value
Publication number	US-10746519-B2
Application number	US-201715998611-A
Country	US
Kind code	B2
Filing date	Feb 8, 2017
Priority date	Feb 16, 2016
Publication date	Aug 18, 2020
Grant date	Aug 18, 2020

Abstract

Fuse system for a projectile for a ranged weapon, the fuse system comprising: a plurality of magnetic field sensors, each sensor being arranged to provide a signal that changes in response to a relative change in position and/or orientation between the system and the Earth's magnetic field, and wherein each sensor has a different alignment in terms of magnetic field sensitivity, and a controller arranged to receive one or more signals from the plurality of magnetic field sensors, and to activate a fuse of the projectile depending on the received one or more signals.

First claim

The invention claimed is:

1. A fuse system for a projectile, the fuse system comprising:
a plurality of magnetic field sensors, each magnetic field sensor configured to provide a signal that changes in response to a particular change in a sensed strength of Earth's magnetic field and/or a particular change in a sensed vector angle of the Earth's magnetic field, wherein each magnetic field sensor has a different alignment in terms of magnetic field sensitivity; and
a controller configured to receive one or more of the signals from at least one of the plurality of magnetic field sensors, and to activate a fuse of the projectile when the particular change in the sensed strength of the Earth's magnetic field and/or the particular change in the sensed vector angle of the Earth's magnetic field equates to the Earth's magnetic field at a target location relative to a firing origin of the projectile.

2. The fuse system of claim 1 , wherein the system comprises three of the magnetic field sensors.

3. The fuse system of claim 1 , wherein the different alignment in terms of magnetic field sensitivity is an orthogonal alignment.

4. The fuse system of claim 1 , wherein the controller comprises a turn counter, to count a number of turns the projectile makes about a longitudinal axis of the projectile, using the one or more received signals.

5. The fuse system of claim 4 , wherein the controller is configured to apply a band pass filter and/or a phased lock loop filter to the received signals, to at least partially filter out signals outside of a turn frequency range of interest.

6. The fuse system of claim 1 , wherein the controller infers a particular change in location of the projectile from the one or more received signals based on the particular change in the sensed strength of the Earth's magnetic field and/or the particular change in the sensed vector angle of the Earth's magnetic field with respect to the Earth's magnetic field at the firing origin of the projectile, and wherein the controller is further configured to activate the fuse when the particular change in location of the projectile equates to the projectile being at the target location.

7. The fuse system of claim 6 , wherein the one or more received signals and/or the firing origin and/or the target location represent a known or sensed magnetic field vector angle and/or a known or sensed magnetic field strength and/or a known or sensed change in a magnetic field vector angle and/or a known or sensed change in magnetic field strength.

8. The fuse system of claim 1 , wherein the magnetic field sensors include:
one or more active magnetic field sensors; and/or
one or more fluxgate sensors; and/or
one or more magnetoresistive sensors.

9. The fuse system of claim 1 , wherein the fuse system stores data that comprises or is at least indicative of one or more of:
priming information; and/or
timing information; and/or
a muzzle velocity of the projectile; and/or
a particular turn count number; and/or
magnetic field information; and/or
projectile firing origin information; and/or
projectile firing origin information in the form of magnetic field strength information; and/or
projectile firing origin information in the form of magnetic field vector angle information; and/or
projectile target location information; and/or
projectile target location in the form of magnetic field strength information; and/or
projectile target location in the form of magnetic field vector angle information.

10. The fuse system of claim 1 , further comprising a receiver to receive an electromagnetic carrier wave, and to decode data encoded in the carrier wave to retrieve that data.

11. The fuse system of claim 10 , wherein the receiver decodes the data by detecting the presence or absence of particular sub-carriers on the carrier wave.

12. The fuse system of claim 11 , wherein the data comprises or is at least indicative of one or more of:
priming information; and/or
timing information; and/or
a muzzle velocity of the projectile; and/or
a particular turn count number; and/or
magnetic field information; and/or
projectile firing origin information; and/or
projectile firing origin information in the form of magnetic field strength information; and/or
projectile firing origin information in the form of magnetic field vector angle information; and/or
projectile target location information; and/or
projectile target location in the form of magnetic field strength information; and/or
projectile target location in the form of magnetic field vector angle information.

13. A projectile for a ranged weapon, the projectile comprising the fuse system of claim 1 .

14. A method of activating a fuse of a projectile, the method comprising:
providing, via a plurality of magnetic field sensors of the projectile, one or more signals that change in response to a particular change in a sensed strength of Earth's magnetic field and/or a particular change in a sensed vector angle of the Earth's magnetic field, each magnetic field sensor having a different alignment in terms of magnetic field sensitivity; and
activating the fuse of the projectile when the particular change in the sensed strength of the Earth's magnetic field and/or the particular change in the sensed vector angle of the Earth's magnetic field equates to the Earth's magnetic field at a target location relative to a firing origin of the projectile.

15. The fuse system of claim 4 , wherein the controller is configured to activate the fuse at a particular turn count.

16. The fuse system of claim 1 , wherein the magnetic field sensors include:
one or more sensors capable of detecting a magnetic field in the range of 25-65 μT; and/or
one or more sensors capable of detecting changes in a magnetic field of 25-65 nT.

17. The fuse system of claim 11 , wherein the data is usable by the controller in the activation of the fuse of the projectile.

18. The fuse system of claim 10 , wherein the data comprises or is at least indicative of one or more of:
priming information; and/or
timing information; and/or
a muzzle velocity of the projectile; and/or
a particular turn count number; and/or
magnetic field information; and/or
projectile firing origin information; and/or
projectile firing origin information in the form of magnetic field strength information; and/or
projectile firing origin information in the form of magnetic field vector angle information; and/or
projectile target location information; and/or
projectile target location in the form of magnetic field strength information; and/or
projectile target location in the form of magnetic field vector angle information.

19. The method of claim 14 , further comprising inferring a particular change in location of the projectile from the one or more received signals based on the particular change in the sensed strength of the Earth's magnetic field and/or the particular change in the sensed vector angle of the Earth's magnetic field with respect to the Earth's magnetic field at the firing origin of the projectile, wherein activating the fuse occurs when the particular change in location of the projectile equates to the projectile being at the target location.

20. A fuse system for a projectile, the fuse system comprising:
a plurality of magnetic field sensors, each sensor to provide a signal that changes in response to a relative change in position and/or orientation between the system and the Earth's magnetic field, and wherein each sensor has a different alignm

Assignees

• Bae Systems Plc

Inventors

• Hucker Martyn John
• Atkinson Stephen John

Classifications

• F42C13/08 Primary

  operated by variations in magnetic field · CPC title

• F42C13/006

  for non-guided, spinning, braked or gravity-driven weapons, e.g. parachute-braked sub-munitions · CPC title

• F42B10/26

  using spin (F42B10/04, F42B10/12, F42B10/14, F42B10/24, F42B14/02 take precedence) · CPC title

• F42C11/065 Primary

  Programmable electronic delay initiators in projectiles · CPC title

• F42C17/04

  for electric fuzes · CPC title