← Back to Patent Explorer
US4244293A Expired / Lapsed US ⏱️ 0.0 years remaining

Projectile designed for recoilless and virtually noiseless firing

Assignee: Rheinmetall Industrie AG
•
Filing: 1977-06-09
•
Granted: 1981-01-13
•
Expires: 1997-06-09
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A projectile to be fired from a tubular or rail-shaped launcher has a warhead integral with a rearwardly extending tube of smaller diameter which contains a propulsive charge inserted between the warhead and a sabot carrying a frangible inertial mass. The rear end of the tube has a constricted opening which, upon detonation of the charge, retains the rearwardly moving sabot while giving passage to the disintegrating mass as the projectile is propelled forwardly. The propulsion gases evolving within the tube are temporarily retained by one or more heat-destructible plugs in the sabot and/or in the tube which melt, burn or char to allow the delayed escape of the gases whereby an in-flight thrust is imparted to the projectile.

Inventors

  • 👤 Werner Grosswendt
  • 👤 Manfred Moll
  • 👤 Wilfried Becker

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 16:20
CPC Classifications
F; F41; F41A; F41A1/00; F41A1/08; F41A1/10

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 182 words
A projectile comprising: a head provided with a tubular tail; a sabot slidably received in said tail; an inertial body engaged by said sabot with clearance from the inner wall surface of said tail; and a propulsive charge in said tail inserted between said head and said sabot for driving said head and tail forwardly and said sabot and body rearwardly upon being detonated, said tail having a rear end provided with a constricted opening bounded by an inwardly tapering peripheral surface for retaining said sabot permanently in said tail while giving passage to said body, said sabot having a transverse wall interposed between said charge and said body, said transverse wall defining with the peripheral wall of said tail a substantially closed chamber for retention of combustion gases from said charge upon engagement of said sabot with said constricted opening, at least one of said walls being provided with an aperture which is occupied by a heat-destructible plug and forms a path for a delayed escape of said combustion gases from said chamber, said path being initially obstructed by said body.
Claim 2
Dependent Claim 182 words
A projectile comprising: a head provided with a tubular tail; a sabot slidably received in said tail; an inertial body engaged by said sabot with clearance from the inner wall surface of said tail; and a propulsive charge in said tail inserted between said head and said sabot for driving said head and tail forwardly and said sabot and body rearwardly upon being detonated, said tail having a rear end provided with a constricted opening bounded by an inwardly tapering peripheral surface for retaining said sabot permanently in said tail while giving passage to said body, said sabot having a transverse wall interposed between said charge and said body, said transverse wall defining with the peripheral wall of said tail a substantially closed chamber for retention of combustion gases from said charge upon engagement of said sabot with said constricted opening, at least one of said walls being provided with an aperture which is occupied by a heat-destructible plug and forms a path for a delayed escape of said combustion gases from said chamber, said path being initially obstructed by said body.
Claim 3
Dependent Claim 19 words
A projectile as defined in claim 1 wherein said aperture forms a rearwardly diverging nozzle in said transverse wall.
Claim 4
Dependent Claim 22 words
A projectile as defined in claim 1 wherein said peripheral wall has a rearwardly and radially outwardly slanting nozzle forming said aperture.
Claim 5
Dependent Claim 43 words
A projectile as defined in claim 1 wherein said tail has a diameter smaller than that of said head, said tail being provided at said rear end with external wings having outer edges located along a radius equal to that of said head.
Claim 6
Dependent Claim 36 words
A projectile as defined in claim 4 wherein said wings are articulated to said rear end for swinging through an arc of 90° to 180° about pivotal axes transverse to the tube axis of said tail.
Claim 7
Dependent Claim 22 words
A projectile as defined in claim 1 wherein said sabot has a rearwardly facing recess embracing at least part of said body.
Claim 8
Dependent Claim 20 words
A projectile as defined in claim 1 wherein said body consists of a frangible mass disintegrating upon leaving said tail.

References Cited (Backward Citations)

BE555659A Cited
DE831819C Cited
DE1740740U Cited
DE1131560B Cited
US3668872A Cited
US3486451A Cited
DE2004291A1 Cited
US3779130A Cited
US3677131A Cited
US3771417A Cited
US4012987A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-01-13 1984-07-14 1985-01-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-01-13 1988-07-14 1989-01-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-01-13 1992-07-14 1993-01-13 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag