GB191405522A - Improvements relating to Torpedoes. - Google Patents
Improvements relating to Torpedoes.Info
- Publication number
- GB191405522A GB191405522A GB191405522DA GB191405522A GB 191405522 A GB191405522 A GB 191405522A GB 191405522D A GB191405522D A GB 191405522DA GB 191405522 A GB191405522 A GB 191405522A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shafts
- pair
- bevel
- turbines
- wheels
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
- F42B19/12—Propulsion specially adapted for torpedoes
- F42B19/14—Propulsion specially adapted for torpedoes by compressed-gas motors
- F42B19/18—Propulsion specially adapted for torpedoes by compressed-gas motors of turbine type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Gear Transmission (AREA)
- Retarders (AREA)
Abstract
5522. Whitehead & Co. April 12, 1913, [Convention date]. Driving and transmission mechanism, special applications of.-Relates to turbine-driven torpedoes in which a pair of co-axial shafts are coupled to the turbines by reduction gearing. According to the invention, a pair of turbinewheels are located in planes parallel to the longitudinal axis of the torpedo, and each one is coupled by a bevel-pinion to a pair of hemispherical bevel-wheels, fast one with each shaft. As shown in Fig. 1, parallel turbine-wheels a rotating in opposite directions are mounted on shafts c, d turning in bearings e, f. These shafts carry bevel-pinions g, h, gearing with toothed rings i, n, mounted respectively on hemispherical bodies j, o integral respectively with the shafts k, p of the propellers m, q. The injection nozzles r, Fig. 2, of the turbines are supplied with fluid through a pipe s passing through the gap between the rings i, n.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR191405522X | 1913-04-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191405522A true GB191405522A (en) | 1915-06-03 |
Family
ID=32526537
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191405522D Expired GB191405522A (en) | 1913-04-12 | 1914-03-04 | Improvements relating to Torpedoes. |
Country Status (2)
Country | Link |
---|---|
DE (2) | DE277556C (en) |
GB (1) | GB191405522A (en) |
-
1913
- 1913-07-18 DE DE1913277556D patent/DE277556C/de not_active Expired
-
1914
- 1914-03-04 GB GB191405522D patent/GB191405522A/en not_active Expired
-
1917
- 1917-06-20 DE DE1917336699D patent/DE336699C/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE336699C (en) | 1921-05-11 |
DE277556C (en) | 1914-08-19 |
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