US17173A - Improvement in bomb-lances - Google Patents
Improvement in bomb-lances Download PDFInfo
- Publication number
- US17173A US17173A US17173DA US17173A US 17173 A US17173 A US 17173A US 17173D A US17173D A US 17173DA US 17173 A US17173 A US 17173A
- Authority
- US
- United States
- Prior art keywords
- wings
- lance
- gun
- barrel
- bomb
- 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
- 241001088417 Ammodytes americanus Species 0.000 description 32
- 230000000875 corresponding Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 241000283153 Cetacea Species 0.000 description 2
- 210000000614 Ribs Anatomy 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000007493 shaping process Methods 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
- F42B10/12—Stabilising arrangements using fins longitudinally-slidable with respect to the projectile or missile
Definitions
- A represents the gun-barrel, whichis about twenty inches in length, and has formed in its bore, say, three grooves, a a a, into which three ribs or projections, c c c, on the rear end of the projectile or lance B slide when said lance is inserted into the barrel and forced down upon the charge of powder therein.
- the muzzle of the gun is counterbored, so as to receive within it the cylinder part C of the wings.
- the part ot' the cylinder C which enters the bore of the gun is also furnished with slots e e e, corresponding with the grooves a ct a in the barrel, and when in place should bein line with the grooves in the barrel, so that when the lauceis discharged it shall pass through said cylinder C, its nibs or projections c c c passing through the grooves a a a into the slots e e e to their termination, and then they take the cylinder with its wings D.
- the lance takes its wings from the muzzle ot' the gun, the two things being' separate from each other, but held together by the projections, slots, and the cylinder surrounding the lance.
- the cylinder C may be so formed as that after it has left the gun it may spring around the lance, and thus hold itself iu place more firmly.
- the wings D may be straight or spiral, and are connected to the front end of the cylinder C, and cut under at their rear, so as to extend back from the point of the muzzle of the gun.
- the muzzle end of the barrel as shown in Fig. l, is also cut awa-y or tapered, to allow the wings to come back and close down to the barrel.
- the tube or cylinder C may have ni bs or projections ou its inside, and the bomb be grooved to within a short distance of the rear end and corresponding to the nibs in said tube; or these lances or projectiles may be fired from a gun without grooves, the bomb sliding through the tube until the nibs in the tube catch the ungrooved part of the bomb, and thus direct its passage, as heretofore described; but I prefer grooving the barrel as being less expensive than groov ing the bombs or lances.
- a single wing which may be used without a tube, and which also can be taken oft by a nib or projection on the lance or bomb; and the wings may be attached to the tube by strips of metal, and project so far rearward that they may spring together in rear of the lance when it enters a whale or other object.
- the wings may be taken from the gun by the lance or projectile and many obvious modif" be cut therein to allow the Wings to slide into,
- these grooves may be so cut or arranged as to correspond or bein line with the grooves in the barrel, and thus be a guide or directriz; to the proper placing of the projectile in the end of said barrel.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
- UNITED STATES PATENT OEEICII;O
RUFUS SIBLEY, CF GREENVILLE, CONNECTICUT.
IMPROVEM ENT IN BOMB-LANCES.
Specification forming part of Letters Patent No. 17,173, dated April 28, 1857.
To all whom it may concer/n:
Be it known that I, RUEUS SIBLEY, of Greenville, in the county of New London an d State of Connecticut, have invented certain new and useful Improvements in Boinb-Lances; and Iv do hereby declare the following to be a full, clear, and exact description of the same, ret'- erence being had to the accompanying drawings, making a part thereof, in which- Figure l represents, in section, a portion of the gun-barrel from which the lance or projectile is fired, and in full the lance with' the wings that are to direct it in place. Eig. 2 represents a portion of the barrel in perspective. Fig. 3 represents the wings and their cylinder detached and inverted to better show the slots in it. Fig. 4 represents a front view of the wings, and Fig. 5 represents amodited form of the wing.
Similar letters of reference, where they occur in the several figures, denote like parts of the bomb-lance or projectile in all of them.
Many forms of guiding-wings for bomblances have been essayed, all of which have been so arranged as to require to he put into the gun with the lance. These have many objections; but I need not enumerate them, and my object in referring to them is simply to more clearly point out my invention, which consists in causing a lance or projectile to take from the muzzle ofthe gun the wings that are to rotate and guide it through the air or water, and thus avoid the necessity of hingiug, folding, or loading the wings with the projectile, as heretofore done 5 and my invention also consists in so shaping the muzzle end of the barrel or gun from which the projectile is red as that the wings may come close down to the barrel.
To enable others skilled in the art to make and use my invention, I will proceed to describe the same with reference to the drawings.
A represents the gun-barrel, whichis about twenty inches in length, and has formed in its bore, say, three grooves, a a a, into which three ribs or projections, c c c, on the rear end of the projectile or lance B slide when said lance is inserted into the barrel and forced down upon the charge of powder therein. The muzzle of the gun is counterbored, so as to receive within it the cylinder part C of the wings. (Shown in Fig. 3.) The part ot' the cylinder C which enters the bore of the gun is also furnished with slots e e e, corresponding with the grooves a ct a in the barrel, and when in place should bein line with the grooves in the barrel, so that when the lauceis discharged it shall pass through said cylinder C, its nibs or projections c c c passing through the grooves a a a into the slots e e e to their termination, and then they take the cylinder with its wings D. Thus the lance takes its wings from the muzzle ot' the gun, the two things being' separate from each other, but held together by the projections, slots, and the cylinder surrounding the lance. If further attachment or connection between the lance and guiding-wings be necessary, the cylinder C may be so formed as that after it has left the gun it may spring around the lance, and thus hold itself iu place more firmly. The wings D may be straight or spiral, and are connected to the front end of the cylinder C, and cut under at their rear, so as to extend back from the point of the muzzle of the gun. The muzzle end of the barrel, as shown in Fig. l, is also cut awa-y or tapered, to allow the wings to come back and close down to the barrel.
I have represented three sets of grooves, projections, and slots. Of course, I do not limit the number nor restrict myself to any number, and, instead of arranging' these things specially, as represented, the tube or cylinder C may have ni bs or projections ou its inside, and the bomb be grooved to within a short distance of the rear end and corresponding to the nibs in said tube; or these lances or projectiles may be fired from a gun without grooves, the bomb sliding through the tube until the nibs in the tube catch the ungrooved part of the bomb, and thus direct its passage, as heretofore described; but I prefer grooving the barrel as being less expensive than groov ing the bombs or lances.
In Fig. 5 I have shown a single wing, which may be used without a tube, and which also can be taken oft by a nib or projection on the lance or bomb; and the wings may be attached to the tube by strips of metal, and project so far rearward that they may spring together in rear of the lance when it enters a whale or other object. There are various ways by which the wings may be taken from the gun by the lance or projectile and many obvious modif" be cut therein to allow the Wings to slide into,
and these grooves may be so cut or arranged as to correspond or bein line with the grooves in the barrel, and thus be a guide or directriz; to the proper placing of the projectile in the end of said barrel.
Having thus fully described the nature of my invention, what I claim therein as new, and desire to secure by Letters Patent, is-
l. Causing a bomb lance or projectile to take the Wings that are to guide it through the air or water from the muzzle of the gun from which it is discharged, substantially in the manner herein set forth and explained.
2. Sloping the muzzle of the gun so that the Wings may come back and close down to the barrel, substantially as set forth.
RUFUS SIBLEY. Witnesses:
- JOHN S. MoWRY,
CHARLES C. FULLER.
Publications (1)
Publication Number | Publication Date |
---|---|
US17173A true US17173A (en) | 1857-04-28 |
Family
ID=2079426
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US17173D Expired - Lifetime US17173A (en) | Improvement in bomb-lances |
Country Status (1)
Country | Link |
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US (1) | US17173A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4708304A (en) * | 1985-12-27 | 1987-11-24 | General Dynamics, Pomona Division | Ring-wing |
US20040130728A1 (en) * | 2002-03-29 | 2004-07-08 | Degertekin Fahrettin Levent | Highly-sensitive displacement-measuring optical device |
US20050224631A1 (en) * | 2004-03-05 | 2005-10-13 | The Boeing Company | Mortar shell ring tail and associated method |
-
0
- US US17173D patent/US17173A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4708304A (en) * | 1985-12-27 | 1987-11-24 | General Dynamics, Pomona Division | Ring-wing |
US20040130728A1 (en) * | 2002-03-29 | 2004-07-08 | Degertekin Fahrettin Levent | Highly-sensitive displacement-measuring optical device |
US20050224631A1 (en) * | 2004-03-05 | 2005-10-13 | The Boeing Company | Mortar shell ring tail and associated method |
US7262394B2 (en) * | 2004-03-05 | 2007-08-28 | The Boeing Company | Mortar shell ring tail and associated method |
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