US483126A - James h - Google Patents
James h Download PDFInfo
- Publication number
- US483126A US483126A US483126DA US483126A US 483126 A US483126 A US 483126A US 483126D A US483126D A US 483126DA US 483126 A US483126 A US 483126A
- Authority
- US
- United States
- Prior art keywords
- charge
- shell
- propelling
- torpedo
- james
- 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
- 241000251734 Torpedo Species 0.000 description 14
- 239000000203 mixture Substances 0.000 description 10
- 238000005192 partition Methods 0.000 description 10
- 239000000843 powder Substances 0.000 description 8
- 239000002360 explosive Substances 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- 241000239290 Araneae Species 0.000 description 4
- 241000251729 Elasmobranchii Species 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000010304 firing Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910001018 Cast iron Inorganic materials 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- JVTAAEKCZFNVCJ-UHFFFAOYSA-N lactic acid Chemical compound CC(O)C(O)=O JVTAAEKCZFNVCJ-UHFFFAOYSA-N 0.000 description 2
- 238000009527 percussion Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000003643 water by type Substances 0.000 description 2
- 239000002023 wood 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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/44—Boat-tails specially adapted for drag reduction
Definitions
- My invention relates to torpedoes for use in times of war.
- Figure 1 is a longitudinal section of the whole device.
- Iliig. 2 is a separate longitudinal section of the chamber for the propelling-powder.
- Figs. 3 and 4 are details.
- Fig 5 shows how the device will skip on the surface of the water.
- 1 is a chamber containing a power explosive, as dynamite 2. Behind chamber 1 is a second chamber 3 to contain the slow-burning propelling-powder 4.
- the two shells which form these chambers may be separately made and fastened together by bolts or rivets, as shown, or may .beotherwise or other suitable material.
- shell 3 is a pole of wood orgaspipe extending through the chamber 3 and secured to partition 5. At its rear end it is; provided with wings or vanes 8 to guide the torpedo; If desired, these guide-blades may extend forward to the body of the torpedoigs t.
- the rear end of shell 3 is a spider 10 to brace the stem 7.
- 11 is a loose piston in shell?) in 'front oftlie propelling-charge 4. It has an device may be used.
- a torpedo the combination, substantially as set forth, of two shells'connected together, one containing an explosive charge to be exploded atthedestination of the device and the other containing a propelling-charge of slow-burning powder to propel the device, and a stem projecting rearwardly from said shells to guide them in their course.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
Description
J.H.BATES.
(No Model.)
TORPE'DO.
No. 483,126. PatentedSept. 27,1892.
l constructed. 'The essential is that-they be separated by a sto'ut partition 5 of cast-iron indicated by the dotted line 9 in Fig. 1. '45
JAMES H. BATES, OF NEW YORK, N. Y.
" resence.
SIEEGIFIGATEQK forming part of Letters Patent No. $83,126, dated fieptember 2'7, 1892.
Application filed February 11, 1892.
To Q/ZZ whom it may concern.-
Be it known that I, JAMES H. BATES, of New York, N. L, have invented certain new and useful Improvements in Torpedoes, whereof the following is' a specification.
My invention relates to torpedoes for use in times of war.
It consists, in general terms, in a device with two chambers, one of which contains thehighpower. explosive yvhich does the damage, and the other contains a slow-burning powder or analogous material, whose combustion propels the device. 7
It consists, further, in other matters, chiefly of detail, which will be described in connection with the specific embodiment of the invention shown in the accompanying draw- IIl S.
In the drawings, Figure 1 is a longitudinal section of the whole device. Iliig. 2 is a separate longitudinal section of the chamber for the propelling-powder. Figs. 3 and 4 are details. Fig 5 shows how the device will skip on the surface of the water.
In the figures, 1 is a chamber containing a power explosive, as dynamite 2. Behind chamber 1 is a second chamber 3 to contain the slow-burning propelling-powder 4. The two shells which form these chambers may be separately made and fastened together by bolts or rivets, as shown, or may .beotherwise or other suitable material. In Fig. 2 I haveshown shell 3 as formed of sheet material wound'with wire 6 and then soldered, which makes a very strong, light, and cheap shell. 7 is a pole of wood orgaspipe extending through the chamber 3 and secured to partition 5. At its rear end it is; provided with wings or vanes 8 to guide the torpedo; If desired, these guide-blades may extend forward to the body of the torpedoigs t. the rear end of shell 3 is a spider 10 to brace the stem 7. 11 is a loose piston in shell?) in 'front oftlie propelling-charge 4. It has an device may be used.
air-space between it and partition 5 to bon-.
stitute acushion to prevent shockbeingtransc Serial No. 421,122. (No model.)
mitted from the propelling-charge to the ex- 5c ploding charge 2. 12 is a percussion firing device of the usual formg'but any other firing In practice the torpedo is propelled by the combustion of the propelling-charge, after the 5 5 manner of. a rocket. It may be used as a submarine or aerial projectile. In Fig. 51 have shown it as fired near the waters surface and skipping or ricochetting on the surface, 13 being the water surface or wave-line."-
1. In a torpedo, the combination, substantially as set forth, of two shells'connected together, one containing an explosive charge to be exploded atthedestination of the device and the other containing a propelling-charge of slow-burning powder to propel the device, and a stem projecting rearwardly from said shells to guide them in their course. c
2. In a torpedo, the combination, substan- -7c tially as set forth, of a double shell, one chamberof which contains an exploding charge and the other at propelling-charge, a cushion between the two charges to prevent the transmission of shock, and a stem projecting rearwardly from said shells to guide them in their course. a
3. The combination, substantially as set forth, ina torpedo, of the two,shells, with a loosepiston 11 in the after shell in frontof .80 the propelling-charge.
4. The' combination,- substantially as -set forth in a torpedo, of the shell containing the enplosive charge, the shell containing the propolling-charge, flOl'li said shells, and guide-blades on said sem.,.
- 5. The combination, substantially as set forth, in a torpedo, of the double shell witha partition between its chambers, the stem se- 9Q cured to said partition and extending rearwardly through the after shell,-th,6 spider. to brace the stem 'at the end oflthe after shell, and the guide-wings upon the stem.
. JAMES H. BATES. Witnesses:
WM. F. A: Sexton-rs, Emsros D. Moons.
a stem projecting rearwardly
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US483126A true US483126A (en) | 1892-09-27 |
Family
ID=2551977
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US483126D Expired - Lifetime US483126A (en) | James h |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US483126A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2487053A (en) * | 1944-11-16 | 1949-11-08 | Us Sec War | Obturator trap for rocket propellants |
| US2490349A (en) * | 1944-09-14 | 1949-12-06 | Golden Sidney | Rocket projectile |
| US2814250A (en) * | 1952-07-03 | 1957-11-26 | Wilhelm S Everett | Adjustable shock and vibration mount |
| US2996879A (en) * | 1954-07-13 | 1961-08-22 | Arthur H Miller | Grain immobilizer |
-
0
- US US483126D patent/US483126A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2490349A (en) * | 1944-09-14 | 1949-12-06 | Golden Sidney | Rocket projectile |
| US2487053A (en) * | 1944-11-16 | 1949-11-08 | Us Sec War | Obturator trap for rocket propellants |
| US2814250A (en) * | 1952-07-03 | 1957-11-26 | Wilhelm S Everett | Adjustable shock and vibration mount |
| US2996879A (en) * | 1954-07-13 | 1961-08-22 | Arthur H Miller | Grain immobilizer |
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