Projectile

Patent metadata

Field	Value
Publication number	US-10684107-B2
Application number	US-201514970956-A
Country	US
Kind code	B2
Filing date	Dec 16, 2015
Priority date	Jan 8, 2015
Publication date	Jun 16, 2020
Grant date	Jun 16, 2020

Abstract

The present invention provides a projectile for use in a simulated fan-blade-off ballistic test. The projectile has an ellipsoid body having a blind axial bore extending from a first axial end. The blind axial bore is for housing a weight adjustment body which can be used to modify the weight and/or centre of gravity of the projectile. A sealing plug may seal the weight adjustment body within the axial bore and an insert may be provided to fix the position of the weight adjustment body and/or to control the sliding of the weight adjustment body within the axial bore.

First claim

The invention claimed is:

1. A projectile for use in a simulated fan-blade-off ballistic test, the projectile having an open axial end and a closed axial end, the projectile being projected toward a target with the open axial end as a tail side of the projectile and the closed axial end as a nose side of the projectile, the projectile comprising:
an ellipsoid body having a blind axial bore extending from the open axial end of the projectile to a blind end of the blind axial bore, the blind axial bore extending for a majority of an entire axial length of the projectile;
at least one weight adjustment body housed within the blind axial bore separated from the blind end of the blind axial bore; and
at least one insert housed within a space between i) the blind end of the blind axial bore and (ii) an end of the at least one weight adjustment body closest to the blind end in an axial direction of the blind axial bore,
the at least one insert being made of a resiliently deformable elastomeric material with a spring constant, the spring constant being selected to control a sliding movement of the at least one weight adjustment body in the axial direction, such that upon impact of the nose side of the projectile on the target, the end of the at least one weight adjustment body moves further toward the blind end of the blind axial bore by compressing the at least one insert.

2. The projectile according to claim 1 , wherein the at least one weight adjustment body is slidable within the blind axial bore.

3. The projectile according to claim 1 , further comprising
a sealing plug for sealing the blind axial bore.

4. The projectile according to claim 1 , wherein the ellipsoid body is formed of aluminium or an aluminium alloy.

5. A kit for use in a simulated fan-blade-off ballistic test, the kit comprising:
the projectile according to claim 1 ; and
a plug for sealing the blind axial bore at the open axial end.

6. The kit according to claim 5 , further comprising
a plurality of weight adjustment bodies of differing masses.

7. The kit according to claim 5 , further comprising
a plurality of inserts of differing axial lengths and/or differing deformation properties and/or differing frictional resistance properties.

8. A simulated fan-blade-off ballistic test method comprising:
firing a projectile towards a test item to be impacted, the projectile having an open axial end and a closed axial end, the projectile being projected toward the test item with the open axial end as a tail side of the projectile and the closed axial end as a nose side of the projectile, the projectile comprising:
an ellipsoid body having a blind axial bore extending from the open axial end of the projectile to a blind end of the blind axial bore, the blind axial bore extending for a majority of an entire axial length of the projectile;
at least one weight adjustment body housed within the blind axial bore separated from the blind end of the blind axial bore; and
at least one insert housed within a space between (i) the blind end of the blind axial bore and (ii) an end of the at least one weight adjustment body closest to the blind end in an axial direction of the blind axial bore,
the at least one insert being made of a resiliently deformable elastomeric material with a spring constant, the spring constant being selected to control a sliding movement of the at least one weight adjustment body in the axial direction, such that upon impact of the nose of the projectile on the target, the end of the at least one weight adjustment body moves further toward the blind end of the blind axial bore by compressing the at least one insert; and
assessing damage to the test item after impact of the projectile.

9. The projectile according to claim 1 , wherein the at least one weight adjustment body slides away from the open axial end of the projectile towards the blind end of the blind axial bore.

10. The projectile according to claim 1 , wherein
the entire axial length of the projectile is approximately 170 mm, and
an entire axial length of the blind axial bore is approximately 164 mm.

11. The projectile according to claim 1 , wherein the blind axial bore has:
a first diameter section disposed at the open axial end,
a second diameter section disposed inward of the first diameter section and having a diameter smaller than a diameter of the first diameter section, and
a third diameter section disposed inward of the second diameter section and having a diameter smaller than the diameter of the second diameter section.

12. The projectile according to claim 1 , wherein the blind axial bore is sealed so that the at least one weight adjustment body flies with the projectile and slides within the blind axial bore upon an impact of the projectile after the flight.

13. The projectile according to claim 1 , further comprising:
paint coatings or gridded lines on an outer surface of the projectile that are monitored by a camera as the projectile is projected and impacted on the target.

Assignees

• Rolls Royce Plc

Inventors

• Williams Christopher
• Finlayson James

Classifications

• F42B8/12 Primary

  Projectiles or missiles (F42B10/48, F42B12/36, F42B19/36 take precedence) · CPC title

• F42B30/00

  Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used (F42B10/00, F42B12/00, F42B14/00 take precedence) · CPC title

• F42B12/02 Primary

  characterised by the warhead or the intended effect · CPC title

• G01N3/30

  by applying a single impulsive force, e.g. by falling weight · CPC title