US1243542A - Projectile. - Google Patents

Projectile. Download PDF

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Publication number
US1243542A
US1243542A US14873917A US14873917A US1243542A US 1243542 A US1243542 A US 1243542A US 14873917 A US14873917 A US 14873917A US 14873917 A US14873917 A US 14873917A US 1243542 A US1243542 A US 1243542A
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Prior art keywords
projectile
arms
gun
wings
openings
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Expired - Lifetime
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US14873917A
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William Robbert Moore
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Individual
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/10Missiles having a trajectory only in the air
    • F42B15/105Air torpedoes, e.g. projectiles with or without propulsion, provided with supporting air foil surfaces

Definitions

  • My invention has for its object to provide a projectile for field, siege, coast and v other guns, having wings which will open when the projectile leaves the gun to prevent tumbling, the wing arms to which the wings are secured being held close to the projectile by the powder shell when the projectile is, introduced into the breech of the gun.
  • the wing arms extend beyond the shell and they are disposed parallel with the axis of the gun when the gun is loaded with the projectile, so that the arms will pass in rifling channelsin the gun which are disposed straight outwardly from the breech and parallel with the axis of the gun.
  • Fig. 2 is a longitudinal sectional view of the projectile
  • Fig. 3 is a rea'r'view of Fig. 2'; and Fig. 4 is a sectional view on the line 44 of Fig. 1.
  • the projectile 5 has a plurality of longitudinally extendingv openings 6 spaced apart in its sides, there'being also rear openings 7 in the projectile 5,. one of these rear openings 7 being connected with each of the longitudinally extending openings 6.
  • a bearing 8 in the pr0jectile At the forward end of each of the longitudinally extending openings 6 there is a bearing 8 in the pr0jectile,"and 1n the forward portion of each of plugs 9, which are used to close the opening 7, there is a similar bearing 10, the bearings 10 being in alinement with the bearings journaled in these bearings 8 and 10.
  • spools 11 being diameter of each of the spools l1 tapers for- V wardly as illustrated, and on these spools there are wound steel sheet wings 12, the outer ends of these wings 12 being secured to arms 13 which have their forward ends coiled to form springs 14 which are disposed in openings 15 in the sides of the projectile, terminals 16, extending from the springs 14:, being disposed in recesses 17 by which means the springs 14 are held in place.
  • the arms 13 move forwardly when they are freed, and for this reason the spools 11 are tapered as has been stated, since the forward ends of the wings 12 will expose less surface than their rear ends when they are spread.
  • the arms 13 will be disposed close to the sides of the projectile 5 when the arms are in closed position, but nevertheless the arms 13 whicl1 are disposed parallel with each other and with the axis of the projectile, will be disposed slightly beyond the sides of the projectile, so that when the projectile is disposed in a gun the arms 13 will be disposed in rifling grooves which are parallel with each other and with the axis of the gun.
  • the wings 12 serve to prevent the projectile from tumbling.
  • the plugs 9 are preferably screwed in threads inthe openings 7, there being recesses 18 in the plugs 9.
  • the rear ends of the arms 18 are held in position by the powder casing 20 when the projectile is introduced into the gun and until it is fired.
  • a projectile having openings spaced apart around its sides, spools one jonrnaled- Ill each ofthe openings, Wings wound one on each of the spools, arms to which the wings are secured, means to move 'the arms outwardly to. spread the ⁇ VlllgS, the
  • a projectile having an opening in its side, there being an opening inthe rear .of the projectile extending to the first opening,
  • plug for closing the second opening and having a bearing in alincment with the first bearing, a spool journa'led in the bearings, a wing wound on the spool, and means for spreading the wing.
  • a projectile having a plurality of open-' ings in its side and a plurality of openings 1n-1ts rear one-of which extends to each of thefirst openings, beatings one at the front of each of the first lIlCIliZlOIlOd open1ngs,
  • plugs for closing the second mentioned open ings and each having a, bearing in ztlinement with one of the first mentioned bearngs, spools journaled in the bearings, wings ,Wound one on each of the spools, and resiliently held arms to which the wings are se- ,cnred.

Description

. DORE.
TILE.
LED FEB- 15, I
Patented 001;. 16,1917.
WIT IVESSES %lo h WILLIAM ROBBERT MOQBE, OF FAYETTEVILLE, ARKANSAS.
PBOJ'ECTILE.
Specification of Letters .Patent.
Patented Oct. 16. 1917.
Application filed February 15, 191?. Serial No. 148,739.
To all whom it may concern:
Be it known that 1, WILLIAM R. Moonn, a citizen of the United States, and a resident of Fayetteville, in the county of Washington and State of Arkansas, have invented a new and Improved Projectile, of which the following is a full, clear, and exact de scription. My invention has for its object to provide a projectile for field, siege, coast and v other guns, having wings which will open when the projectile leaves the gun to prevent tumbling, the wing arms to which the wings are secured being held close to the projectile by the powder shell when the projectile is, introduced into the breech of the gun. The wing arms extend beyond the shell and they are disposed parallel with the axis of the gun when the gun is loaded with the projectile, so that the arms will pass in rifling channelsin the gun which are disposed straight outwardly from the breech and parallel with the axis of the gun. When the shell is used, there is practically no frictionagainst the rifiing of the gun,
.and a longer range is obtained than is now possible with the spiral rifling in use:
; Additional objects of the invention will appear in the following specification, in wlich the preferred form of the invention is disclosed.
In the drawings similar reference characters denote similar parts in all the views, in which Figure 1 is a side elevation of the projectile and a portion of the powder casing;
. Fig. 2 is a longitudinal sectional view of the projectile;
Fig. 3 is a rea'r'view of Fig. 2'; and Fig. 4 is a sectional view on the line 44 of Fig. 1.
By referring to the drawings, it will be seen that the projectile 5 has a plurality of longitudinally extendingv openings 6 spaced apart in its sides, there'being also rear openings 7 in the projectile 5,. one of these rear openings 7 being connected with each of the longitudinally extending openings 6. At the forward end of each of the longitudinally extending openings 6 there is a bearing 8 in the pr0jectile,"and 1n the forward portion of each of plugs 9, which are used to close the opening 7, there is a similar bearing 10, the bearings 10 being in alinement with the bearings journaled in these bearings 8 and 10. The
8, spools 11 being diameter of each of the spools l1 tapers for- V wardly as illustrated, and on these spools there are wound steel sheet wings 12, the outer ends of these wings 12 being secured to arms 13 which have their forward ends coiled to form springs 14 which are disposed in openings 15 in the sides of the projectile, terminals 16, extending from the springs 14:, being disposed in recesses 17 by which means the springs 14 are held in place. The arms 13 move forwardly when they are freed, and for this reason the spools 11 are tapered as has been stated, since the forward ends of the wings 12 will expose less surface than their rear ends when they are spread.
As will be seen by referring to Fig. 1 of the drawings, the arms 13 will be disposed close to the sides of the projectile 5 when the arms are in closed position, but nevertheless the arms 13 whicl1 are disposed parallel with each other and with the axis of the projectile, will be disposed slightly beyond the sides of the projectile, so that when the projectile is disposed in a gun the arms 13 will be disposed in rifling grooves which are parallel with each other and with the axis of the gun. With this construction there is practically no friction against the riding grooyes of the gun when the projectile is fired, and this naturally increases the range of fire. The wings 12 serve to prevent the projectile from tumbling.
I prefer to provide the projectile 5 with four arms 13, each having a .wing 12 secured thereto, and to space these arms and wings apart around the projectile, with two laterally extending wings and arms of greater length than the upwardly and downwardly extending wings and arms.
The plugs 9 are preferably screwed in threads inthe openings 7, there being recesses 18 in the plugs 9.
The rear ends of the arms 18 are held in position by the powder casing 20 when the projectile is introduced into the gun and until it is fired.
Having thus described my invention, I claim as new and desire to secure by Letters Patent:
move the arm outwardly to spread the wing.
. 2. A projectile having openings spaced apart around its sides, spools one jonrnaled- Ill each ofthe openings, Wings wound one on each of the spools, arms to which the wings are secured, means to move 'the arms outwardly to. spread the \VlllgS, the
arms when in closed position being disposed at theouter Side of the pro ectile and paral- 'lel with the axis of the projectile.
3. A projectile having an opening in its side, there being an opening inthe rear .of the projectile extending to the first opening,
' a'bearing-at the front of the first opening, a
plug for closing the second opening and having a bearing in alincment with the first bearing, a spool journa'led in the bearings, a wing wound on the spool, and means for spreading the wing.
4'. A projectile having a plurality of open-' ings in its side and a plurality of openings 1n-1ts rear one-of which extends to each of thefirst openings, beatings one at the front of each of the first lIlCIliZlOIlOd open1ngs,
plugs for closing the second mentioned open ings and each having a, bearing in ztlinement with one of the first mentioned bearngs, spools journaled in the bearings, wings ,Wound one on each of the spools, and resiliently held arms to which the wings are se- ,cnred.
"5.'A projectile having anopening in its side, anarrn pivoted at its forward end to the forward end of-the pro ectile, a wing disposed in the opening in-the projectile and secured to the arm to be moved ont\\'ardly thereby, and means connected with the projectile 1n the breech of it gun which serves'to tllU'SPOOl, a n arm pivoteda-t its forward-end to the projectile, and-means connected with :the projectile in the breech ofa gun which serves tohold'the arm close to the pro ec-. tile, the1ar|n being freed to 'move outwardlyv when the projectile is fired, thereby severing the connection between the means and the side, an arm pivoted to the'projectilein Front of the openii'lg and having means for moving it ouhvardlj', the arm when the pro jectile is in a gun being disposed parallel With the axis of the projectile at the. outer 7. A-projectile having an opening in its side thereof for fitting the riding, a curtain v in the opening 'and secured to thezlrin, and means which may be .disposedwith the projectile in a. gun and which serves to hold the arm close to the projectile, the arm' being freed to move outwardly When the projectile is h red, thereby severing the' connection bet-weenthe means and the arm.
- WVILLIAM ROBBERT MOORE.
US14873917A 1917-02-15 1917-02-15 Projectile. Expired - Lifetime US1243542A (en)

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2666387A (en) * 1949-12-07 1954-01-19 United Aircraft Corp Stabilizing fins for missiles
US3177809A (en) * 1962-07-24 1965-04-13 Budd Co Semi-fixed artillery round
DE1203647B (en) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Fin tail, especially for rocket projectiles
US3507150A (en) * 1966-01-24 1970-04-21 Robert F Stengel Wind velocity probing device and method
US3690662A (en) * 1970-01-08 1972-09-12 Joseph Pasqualini Towed aerial target
US3826448A (en) * 1972-09-14 1974-07-30 Nasa Deployable flexible ventral fins for use as an emergency spin-recovery device in aircraft
US4030421A (en) * 1975-06-26 1977-06-21 Smith & Wesson Chemical Company, Inc. Dual purpose projectile and weapon combination
DE3026409A1 (en) * 1979-09-24 1982-03-04 General Dynamics Corp., St. Louis, Mo. DOUBLE-WALLED SINGLE AND AUTOMATIC FOLD-OUT FLOOR LEAF
US4586681A (en) * 1983-06-27 1986-05-06 General Dynamics Pomona Division Supersonic erectable fabric wings
US4955938A (en) * 1981-12-10 1990-09-11 Rheinmetall Gmbh Ammunition, preferably for use in high-angle fire
US5762291A (en) * 1996-10-28 1998-06-09 The United States Of America As Represented By The Secretary Of The Army Drag control module for stabilized projectiles
US5788178A (en) * 1995-06-08 1998-08-04 Barrett, Jr.; Rolin F. Guided bullet
US6502785B1 (en) * 1999-11-17 2003-01-07 Lockheed Martin Corporation Three axis flap control system
US7781709B1 (en) 2008-05-05 2010-08-24 Sandia Corporation Small caliber guided projectile
US7823510B1 (en) 2008-05-14 2010-11-02 Pratt & Whitney Rocketdyne, Inc. Extended range projectile
US7891298B2 (en) 2008-05-14 2011-02-22 Pratt & Whitney Rocketdyne, Inc. Guided projectile
US20110214582A1 (en) * 2010-03-04 2011-09-08 Glasser Alan Z High velocity ammunition round
US8291828B2 (en) 2010-03-04 2012-10-23 Glasser Alan Z High velocity ammunition round

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2666387A (en) * 1949-12-07 1954-01-19 United Aircraft Corp Stabilizing fins for missiles
US3177809A (en) * 1962-07-24 1965-04-13 Budd Co Semi-fixed artillery round
DE1203647B (en) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Fin tail, especially for rocket projectiles
US3507150A (en) * 1966-01-24 1970-04-21 Robert F Stengel Wind velocity probing device and method
US3690662A (en) * 1970-01-08 1972-09-12 Joseph Pasqualini Towed aerial target
US3826448A (en) * 1972-09-14 1974-07-30 Nasa Deployable flexible ventral fins for use as an emergency spin-recovery device in aircraft
US4030421A (en) * 1975-06-26 1977-06-21 Smith & Wesson Chemical Company, Inc. Dual purpose projectile and weapon combination
DE3026409A1 (en) * 1979-09-24 1982-03-04 General Dynamics Corp., St. Louis, Mo. DOUBLE-WALLED SINGLE AND AUTOMATIC FOLD-OUT FLOOR LEAF
US4955938A (en) * 1981-12-10 1990-09-11 Rheinmetall Gmbh Ammunition, preferably for use in high-angle fire
US4586681A (en) * 1983-06-27 1986-05-06 General Dynamics Pomona Division Supersonic erectable fabric wings
US5788178A (en) * 1995-06-08 1998-08-04 Barrett, Jr.; Rolin F. Guided bullet
US5762291A (en) * 1996-10-28 1998-06-09 The United States Of America As Represented By The Secretary Of The Army Drag control module for stabilized projectiles
US6502785B1 (en) * 1999-11-17 2003-01-07 Lockheed Martin Corporation Three axis flap control system
US7781709B1 (en) 2008-05-05 2010-08-24 Sandia Corporation Small caliber guided projectile
US7823510B1 (en) 2008-05-14 2010-11-02 Pratt & Whitney Rocketdyne, Inc. Extended range projectile
US7891298B2 (en) 2008-05-14 2011-02-22 Pratt & Whitney Rocketdyne, Inc. Guided projectile
US20110214582A1 (en) * 2010-03-04 2011-09-08 Glasser Alan Z High velocity ammunition round
US8096243B2 (en) * 2010-03-04 2012-01-17 Glasser Alan Z High velocity ammunition round
US8291828B2 (en) 2010-03-04 2012-10-23 Glasser Alan Z High velocity ammunition round

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