US399880A - James weir graydon - Google Patents
James weir graydon Download PDFInfo
- Publication number
- US399880A US399880A US399880DA US399880A US 399880 A US399880 A US 399880A US 399880D A US399880D A US 399880DA US 399880 A US399880 A US 399880A
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- US
- United States
- Prior art keywords
- guide
- graydon
- shell
- flexible
- gun
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000002965 rope Substances 0.000 description 6
- 239000002360 explosive Substances 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
Definitions
- My invention relates to a tail-guide for high-explosive shells designed to be thrown by pneumatic guns and it has for its object to provide such a shell with a simple and effective guide that will occupy but very lit tle space in the gun or in shipment or storage.
- Figure l is a view of my invention, the telescopic guide being shown in section and the flexible guide in elevation, and both represented in the positions assumed by them while the projectile is in 'flight.
- Fig. 2 is a partly-sectional View of my invention, showing the telescopic guide closed up and the flexible guide,which is in elevation, coiled upon it.
- A represents the casing of the shell
- B the screw-plug
- O represents a wire rope, one end of which is secured to a screw-ring, D, which is screwed into plug B of the shell.
- This rope constitutes the flexible tail-guide for the projectile, the length of which requisite to balance the projectile will of course depend on the caliber and weight of the latter and the size of the rope. It may be either of uniform size throughout its length or tapering toward its outer end.
- E represents a telescopic rigid guide.
- This telescopic guide incloses the flexible tailguide for a portion of its length, and thus, while acting as a guide itself, prevents the flexible tail-guide from becoming looped or tangled near the shell. It consists of a series of short metal tubes, 1 2 3 4 5, &c., telescoped one within the other in the well-known manner, the tube 1 being screwed into plug B.
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Telescopes (AREA)
Description
(No Model.)
J. W. GRAYDON.
TAIL GUIDE FOR PROJEGTILES.
No. 399,880. Patented Mar. 19, 1889.
q viiywcae-d N. PETERS, Plwmulm ra rm, Walhinglon, u. c
IINITED STATES PATENT OFFICE.
JAMES WEIR GRAYDON, OF \VASI'IINGTON, DISTRICT OF COLUMBIA, ASSIGNOR TO ROBERT SOUTHIVORTH LAIVRENOE, OF LONDON, ENGLAND.
TAIL-GUIDE FOR PROJECTILES.
SPECIFICATION forming part of Letters Patent No. 399,880, dated March 19, 1889.
Application filed October 9, 1888. Serial No. 287,632. (No model.)
To all whom it may concern.
Be it known that 1, JAMES WEIR GEAYDON, a citizen of the United States of America, residing at Vashington, District of Columbia, have invented certain new and useful Improvements in Tail-Guides for High-Explosive Shells, of which the following is a specification, reference being had therein to the accompanying drawings.
My invention relates to a tail-guide for high-explosive shells designed to be thrown by pneumatic guns and it has for its object to provide such a shell with a simple and effective guide that will occupy but very lit tle space in the gun or in shipment or storage.
It is well known that an elongated shell in order to be effective must maintain a pointon position in its flight, for if it tumbles its range will be uncertain and it will be liable to fall far short of its mark. The rotary motion imparted to such a shell when fired from a rifled gun prevents it from tumbling. Pneumatic guns, however, are necessarily smooth bore, and consequently their projectiles are not given a rotary motion. Therefore, in order to adapt an elongated shell for use in a pneumatic gun it must be provided with some means for guiding it in its flight, or, in other words, for keeping it point-on. Vhatever the means employed to this end regard should be had to the space the device will occupy in the gun, for as pneumatic guns are required to be of considerable length for a good range it is desirable that the guide for the shell shall occupy as little space as possible, so as not to require the gun to be made of any great additional length for its reception.
The invention will first be described in connection with the accompanying drawings and then pointed out in the claim.
Figure l is a view of my invention, the telescopic guide being shown in section and the flexible guide in elevation, and both represented in the positions assumed by them while the projectile is in 'flight. Fig. 2 is a partly-sectional View of my invention, showing the telescopic guide closed up and the flexible guide,which is in elevation, coiled upon it.
Referring to the drawings, A represents the casing of the shell, and B the screw-plug.
O represents a wire rope, one end of which is secured to a screw-ring, D, which is screwed into plug B of the shell. This rope constitutes the flexible tail-guide for the projectile, the length of which requisite to balance the projectile will of course depend on the caliber and weight of the latter and the size of the rope. It may be either of uniform size throughout its length or tapering toward its outer end.
E represents a telescopic rigid guide. This telescopic guide incloses the flexible tailguide for a portion of its length, and thus, while acting as a guide itself, prevents the flexible tail-guide from becoming looped or tangled near the shell. It consists of a series of short metal tubes, 1 2 3 4 5, &c., telescoped one within the other in the well-known manner, the tube 1 being screwed into plug B.
Vith this construction, when the shell is in flight, the parts will assume the positions shown in Fig. 1; but while the shell is in the gun, or while in shipment or storage, the telescopic guide will be folded up and the flexible tail-guide coiled upon it, as seen in Fig. 2.
Having thus described my invention, what I claim as new, and desire to secure by Letters Patent, is
The combination,with an elongated projectile for a pneumatic gun, of a flexible tailguide secured at one end to the screw-plug of the projectile, and a telescopic rigid guide secured in the screw-plug and surrounding a portion of the flexible guide, substantially as
Publications (1)
Publication Number | Publication Date |
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US399880A true US399880A (en) | 1889-03-19 |
Family
ID=2468842
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US399880D Expired - Lifetime US399880A (en) | James weir graydon |
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US (1) | US399880A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4489949A (en) * | 1982-03-04 | 1984-12-25 | Taylor Donald M | Featherless arrow |
US4674706A (en) * | 1986-02-21 | 1987-06-23 | Hall Robert C | Projectile with an extendable boattail |
US20030000901A1 (en) * | 1997-08-15 | 2003-01-02 | Batesville Services, Inc. | Display for a casket selection and/or viewing room |
US6657174B1 (en) * | 1999-11-10 | 2003-12-02 | Bofors Defence Ab | Method and design for increasing the firing range of artillery shells |
US20050173588A1 (en) * | 2002-11-08 | 2005-08-11 | Giat Industries | Method of correcting the trajectory of a spin-stabilised projectile and projectile implementing one such method |
US20110271864A1 (en) * | 2009-11-08 | 2011-11-10 | Omnitek Partners Llc | Speed-Adaptive Deployable Boat-Tailing Cone for Munitions for Range Extension |
US11549789B2 (en) * | 2015-04-21 | 2023-01-10 | The United States Of America, As Represented By The Secretary Of The Navy | Optimized subsonic projectiles |
-
0
- US US399880D patent/US399880A/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4489949A (en) * | 1982-03-04 | 1984-12-25 | Taylor Donald M | Featherless arrow |
US4674706A (en) * | 1986-02-21 | 1987-06-23 | Hall Robert C | Projectile with an extendable boattail |
US20030000901A1 (en) * | 1997-08-15 | 2003-01-02 | Batesville Services, Inc. | Display for a casket selection and/or viewing room |
US6657174B1 (en) * | 1999-11-10 | 2003-12-02 | Bofors Defence Ab | Method and design for increasing the firing range of artillery shells |
US20050173588A1 (en) * | 2002-11-08 | 2005-08-11 | Giat Industries | Method of correcting the trajectory of a spin-stabilised projectile and projectile implementing one such method |
US20110271864A1 (en) * | 2009-11-08 | 2011-11-10 | Omnitek Partners Llc | Speed-Adaptive Deployable Boat-Tailing Cone for Munitions for Range Extension |
US8487227B2 (en) * | 2009-11-08 | 2013-07-16 | Omnitek Partners Llc | Speed-adaptive deployable boat-tailing cone for munitions for range extension |
US11549789B2 (en) * | 2015-04-21 | 2023-01-10 | The United States Of America, As Represented By The Secretary Of The Navy | Optimized subsonic projectiles |
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