Countermeasure flares

Patent metadata

Field	Value
Publication number	US-10330446-B2
Application number	US-201715646022-A
Country	US
Kind code	B2
Filing date	Jul 10, 2017
Priority date	Aug 21, 2012
Publication date	Jun 25, 2019
Grant date	Jun 25, 2019

Abstract

A flare including: a casing; and a grain assembly, at least a portion of the grain assembly being slidably disposed in the casing, the grain assembly including: a shell structure; and a grain component at least partially disposed in the shell structure, the grain component including at least one combustible material and at least one reactive material positioned relative to the combustible material and configured to ignite combustion of the at least one combustible material; wherein the shell structure includes one or more nozzles at an aft end of the shell structure for generating a thrust resulting from ignition of the at least one combustible material.

First claim

What is claimed is:

1. A flare comprising:
a casing; and
a grain assembly, at least a portion the grain assembly being slidably disposed in the casing, the grain assembly comprising:
a shell structure; and
a grain component at least partially disposed in the shell structure, the grain component including at least one combustible material and at least one reactive material positioned relative to the combustible material and configured to ignite combustion of the at least one combustible material;

wherein the shell structure includes one or more nozzles at an aft end of the shell structure for generating a thrust resulting from ignition of the at least one combustible material; and
the one or more nozzles are restrained in a first shape inside the casing and configured to have a second shape, different from the first shape, when the restraint is removed.

2. The flare of claim 1 , further comprising:
an impulse charge device positioned at an aft end of the casing; and
a piston positioned between at least a portion of the one or more nozzle and the impulse charge device such that pressurized gasses generated by initiation of the impulse charge device act on the piston, which in turn ejects the grain assembly from a forward end of the casing.

3. The flare of claim 2 , further comprising an end cap positioned at the forward end of the casing to seal the grain assembly inside the casing.

4. The flare of claim 1 , wherein each of the one or more nozzles include a throat portion and at least one of a expanding portion and a diverging portion connected to the throat.

5. The flare of claim 1 , wherein the one or more nozzle are restrained in the first shape by a mechanical restraint.

6. The flare of claim 1 , wherein the one or more nozzles are restrained in the first shape by a combustible material filling an area inside the one or more nozzles.

7. The flare of claim 1 , wherein the one or more nozzles are restrained in the first shape by a resiliency in the material forming the one or more nozzles.

8. The flare of claim 1 , wherein the one or more nozzles are restrained in the first shape by one or more biasing members.

9. A flare comprising:
a casing; and
a grain assembly, at least a portion the grain assembly being slidably disposed in the casing, the grain assembly comprising:
a shell structure; and
a grain component at least partially disposed in the shell structure, the grain component including at least one combustible material and at least one reactive material positioned relative to the combustible material and configured to ignite combustion of the at least one combustible material;

wherein the shell structure includes one or more nozzles at an aft end of the shell structure for generating a thrust resulting from ignition of the at least one combustible material;
wherein the one or more nozzles comprises two nozzles, each configured to direct thrust in a different direction.

Assignees

• Rastegar Jahangir S
• Murray Richard T
• Raibeck Gretel
• Poret Jay
• Andreola Brandon
• Zimmer Andrew
• Omnitek Partners Llc

Inventors

• Rastegar Jahangir S
• Murray Richard T
• Raibeck Gretel
• Poret Jay
• Andreola Brandon
• Zimmer Andrew

Classifications

• F42B15/10

  Missiles having a trajectory only in the air · CPC title

• F42B15/00

  Self-propelled projectiles or missiles, e.g. rockets; Guided missiles (F42B10/00, F42B12/00, F42B14/00 take precedence; for practice or training F42B8/12; rocket torpedoes F42B17/00; marine torpedoes F42B19/00; cosmonautic vehicles B64G; jet-propulsion plants F02K) · CPC title

• F42B10/26

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

• F42B10/16

  Wrap-around fins · CPC title

• F42B10/14

  using fins spread or deployed after launch, e.g. after leaving the barrel · CPC title