IP Library Granted Patent US 8,616,127
Granted Patent B2
US 8,616,127 · App. 13/647,846 · Granted Dec 31, 2013

Methods for electro-mechanical safety and arming of a projectile

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Quick Facts
Patent No.
US 8,616,127
App. No.
13/647,846
Granted
Dec 31, 2013
Kind
B2
Abstract

A safety and arming apparatus for use with a projectile includes a rotor pivotable between a safe position and an armed position. A biasing element holds a mass engaged with the rotor to restrain the rotor from rotation and is deformable to allow the mass to displace and disengage from the rotor in response to a setback force on the projectile. A second biasing element includes a displaceable end for engaging with the rotor to restrain the rotor from rotation and is deformable to disengage the displaceable end from the rotor in response to projectile spin. A piston actuator can rotate the rotor to the armed position if the mass is disengaged and the displaceable end is disengaged. A detonator on the rotor can be aligned with a detonation cord when the rotor is in the armed position and unaligned when the rotor is in the safe position.

Claims (31)

1. A method for safing a projectile, comprising:

inhibiting rotation of a rotor pivotally coupled to a housing from a safe position to an armed position by biasing a mass against a setback engagement structure of the rotor and biasing a setback retainer within the setback engagement structure against the mass; and

further inhibiting rotation of the rotor from the safe position to the armed position by biasing a displaceable end of a leaf spring against a spin-lock engagement structure on a side surface of the rotor;

wherein the inhibiting rotation or the further inhibiting rotation prevents initiation of a detonation cord operably coupled to the housing by maintaining the rotor in the safe position such that a detonator disposed in the rotor is not aligned with the detonation cord.

2. The method of claim 1 , wherein biasing the mass against the setback engagement structure comprises biasing a setback pin to engage a channel formed in the rotor.

3. The method of claim 1 , wherein biasing the displaceable end of the leaf spring against the spin-lock engagement structure comprises biasing a catch portion of the leaf spring to engage a slot in the side surface of the rotor.

4. The method of claim 1 , further comprising preventing rotation of the rotor from the safe position with a shear tab connected to the rotor and engaged with the housing.

5. The method of claim 1 , wherein biasing a setback retainer within the setback engagement structure against the mass comprises biasing a ball within the setback engagement structure against the mass.

6. A method for arming a projectile, comprising:

displacing a mass away from a setback engagement structure of a rotor pivotally coupled to a housing responsive to an axial acceleration of the projectile above an axial acceleration threshold to enable rotation of the rotor from a safe position to an armed position;

displacing a displaceable end of a leaf spring away from a spin-lock engagement structure on a side surface of the rotor responsive to a spin rate of the projectile above a spin threshold to further enable rotation of the rotor from the safe position to the armed position;

rotating the rotor from the safe position to the armed position by activating a piston actuator to align a detonator disposed in the rotor with a detonation cord operably coupled to the housing; and

after the displacing the mass away from the setback engagement structure, displacing a setback retainer disposed in the setback engagement structure over the mass to prevent the mass from engaging with the setback engagement structure.

7. The method of claim 6 , further comprising:

firing the detonator to initiate the detonation cord; and

detonating at least one explosive charge with the detonation cord.

8. The method of claim 6 , wherein displacing the displaceable end of the leaf spring away from the spin-lock engagement structure comprises disengaging a catch portion of the leaf spring from a slot in the side surface of the rotor.

9. The method of claim 6 , wherein displacing the mass away from the setback engagement structure comprises displacing a setback pin away from a channel formed in the rotor.

10. The method of claim 6 , further comprising, after the displacing the mass and the displacing the displaceable end of the leaf spring, retaining the rotor in the safe position with a shear tab connected to the rotor until the piston actuator is activated.

11. The method of claim 6 , wherein displacing a setback engagement retainer disposed in the setback engagement structure comprises displacing a ball within the setback engagement structure.

12. A method for arming a projectile, comprising:

displacing a mass away from a setback engagement structure of a rotor pivotally coupled to a housing responsive to an axial acceleration of the projectile above an axial acceleration threshold to enable rotation of the rotor from a safe position to an armed position;

displacing a displaceable end of a leaf spring away from a spin-lock engagement structure on a side surface of the rotor responsive to a spin rate of the projectile above a spin threshold to further enable rotation of the rotor from the safe position to the armed position;

rotating the rotor from the safe position to the armed position by activating a piston actuator to align a detonator disposed in the rotor with a detonation cord operably coupled to the housing; and

after the rotating the rotor from the safe position to the armed position, displacing the mass to engage with an indentation in the side surface of the rotor to maintain the rotor in the armed position.

13. The method of claim 12 , further comprising:

firing the detonator to initiate the detonation cord; and

detonating at least one explosive charge with the detonation cord.

14. The method of claim 12 , wherein displacing the displaceable end of the leaf spring away from the spin-lock engagement structure comprises disengaging a catch portion of the leaf spring from a slot in the side surface of the rotor.

15. The method of claim 12 , wherein displacing the mass away from the setback engagement structure comprises displacing a setback pin away from a channel formed in the rotor.

16. The method of claim 12 , further comprising, after the displacing the mass and the displacing the displaceable end of the leaf spring, retaining the rotor in the safe position with a shear tab connected to the rotor until the piston actuator is activated.

Assignments (9)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 8, 2021
From: NORTHROP GRUMMAN INNOVATION SYSTEMS LLC
To: NORTHROP GRUMMAN SYSTEMS CORPORATION
Reel/Frame 055256/0892 →
CHANGE OF NAME Recorded Feb 4, 2021
From: NORTHROP GRUMMAN INNOVATION SYSTEMS, INC.
To: NORTHROP GRUMMAN INNOVATION SYSTEMS LLC
Reel/Frame 055223/0425 →
CHANGE OF NAME Recorded Nov 1, 2018
From: ORBITAL ATK, INC.
To: NORTHROP GRUMMAN INNOVATION SYSTEMS, INC.
Reel/Frame 047400/0381 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jun 6, 2018
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS ADMINISTRATIVE AGENT
To: ORBITAL ATK, INC.
Reel/Frame 046477/0874 →
CHANGE OF NAME Recorded Nov 28, 2017
From: ALLIANT TECHSYSTEMS INC.
To: ORBITAL ATK, INC.
Reel/Frame 044824/0466 →
RELEASE OF SECURITY INTEREST Recorded Oct 8, 2015
From: BANK OF AMERICA, N.A.
To: ALLIANT TECHSYSTEMS INC.; FEDERAL CARTRIDGE CO.; EAGLE INDUSTRIES UNLIMITED, INC.; AMMUNITION ACCESSORIES, INC.; ORBITAL ATK, INC. (F/K/A ALLIANT TECHSYSTEMS INC.)
Reel/Frame 036816/0624 →
SECURITY AGREEMENT Recorded Sep 30, 2015
From: ORBITAL ATK, INC.; ORBITAL SCIENCES CORPORATION
To: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS ADMINISTRATIVE AGENT
Reel/Frame 036732/0170 →
SECURITY AGREEMENT Recorded Nov 26, 2013
From: ALLIANT TECHSYSTEMS INC.; CALIBER COMPANY; EAGLE INDUSTRIES UNLIMITED, INC.; FEDERAL CARTRIDGE COMPANY; SAVAGE ARMS, INC.; SAVAGE RANGE SYSTEMS, INC.; SAVAGE SPORTS CORPORATION
To: BANK OF AMERICA, N.A.
Reel/Frame 031731/0281 →
INTELLECTUAL PROPERTY SECURITY AGREEMENT SUPPLEMENT Recorded Jan 31, 2013
From: ALLIANT TECHSYSTEMS INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 029732/0140 →