US958990A - Torpedo. - Google Patents

Torpedo. Download PDF

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Publication number
US958990A
US958990A US46186408A US1908461864A US958990A US 958990 A US958990 A US 958990A US 46186408 A US46186408 A US 46186408A US 1908461864 A US1908461864 A US 1908461864A US 958990 A US958990 A US 958990A
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United States
Prior art keywords
powder
torpedo
envelop
chamber
tube
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Expired - Lifetime
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US46186408A
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Emile Bourdelles
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R21/02Occupant safety arrangements or fittings, e.g. crash pads
    • B60R21/16Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
    • B60R21/26Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow
    • B60R21/264Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow using instantaneous generation of gas, e.g. pyrotechnic
    • B60R21/2644Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow using instantaneous generation of gas, e.g. pyrotechnic using only solid reacting substances, e.g. pellets, powder

Definitions

  • My invention relates generally to self- I propelling submarine torpedoes, and has reference, especially, to the means employed for propelling such torpedoes through the water.
  • the invention contemplates an improvement in the class of propelling means employing'a powder charge in a chamber of the torpedo, and the principal object of the invention is to provide means whereby a constant area of combustion for the entire powder charge is provided, resulting in a reactive action of the gases to obtain a constant propelling force.
  • my invention consists in inclosing one or more blocks of powder, placed in the torpedo chamber in a sheath or covering of extensible material,
  • An embodiment of the invention is illusdrawing which shows a longitudinal sectional view of a powder charge such as herein referred to.
  • a suitable chamber into which is inserted a metallic envelop 0 which is preferably lined with a non-conductor of heat 6.
  • a metallic envelop 0 which is preferably lined with a non-conductor of heat 6.
  • One end of both envelop and lining is removable and has formed therein one or more gas exhaust orifices a, these orifices being so arranged that the resultant of the escaping gases coincides with the axis of the torpedo.
  • the lined envelop is adapted to contain the powder charge (Z, which may consist of a single block or a plurality of juxtaposed blocks of powder adapted to burn in parallel layers, Prior to the introduction of the powder into the envelop, the former is inserted into a tube 72, of extensible material such as rub her, the diameter of the tube being less than that of the powder whereby the tube is extended or stretched about the blocks.
  • the powder charge Z, which may consist of a single block or a plurality of juxtaposed blocks of powder adapted to burn in parallel layers
  • the outer surface of the powder block should be smooth. Should a block be employed which has a rough or uneven surface, the latter should be coated with a ma- I terial having about the same consistency as rubber solution.
  • the powder charge may, if desired, be ignited at both its ends, or one end only may be left free and the other protected by a layer or coating 2' of a material which is a non conductor of heat. WVhen the powder charge is ignited the same will burn in par allel layers, the combustion being uniform and not extending to the lateral surface of the cylinder, owing to the combined pressure of the gas in the cylinder and the rubber sheath h. The gases will pass 'out through the orifices a, and the reactions thereof in the water will be uniform and the forward propulsion of the torpedo will also be uniform.
  • the gas pressure prevailing in the entire envelop 0 is uniform, and is sufficiently great to counterbalance the pressure of any gas which might attempt to enter between the inner surface of the tube h and the outer surface of the block (Z.

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)

Description

E. BOURDELLES.
TORPEDO.
APPLIOATIDN FILED NOV. 10, 1908.
958,990. 4 Patented-May24,1910.
ANDREW a GRAHAM co Pnmaumucnn nms. WASHNGTON. c. c
' such as rubber for example, the rubber being tratively exemplified in the accompanying EMILE BOURDELLES,
OF PARIS, FRANCE.
TOBPEDO.
Specification of Letters Patent.
Patented May 24, 1910.
Application filed November 10, 1908. Serial No. 481,864.
T 0 all whom it may concern:
Be it known that I, EMILE BoURDELLEs, a citizen of the Republic of France, residing at Paris, France, have invented Improve ments in or Relating to Torpedoes, of which the following is a specification.
My invention relates generally to self- I propelling submarine torpedoes, and has reference, especially, to the means employed for propelling such torpedoes through the water.
The invention contemplates an improvement in the class of propelling means employing'a powder charge in a chamber of the torpedo, and the principal object of the invention is to provide means whereby a constant area of combustion for the entire powder charge is provided, resulting in a reactive action of the gases to obtain a constant propelling force.
Stated in general terms, my invention consists in inclosing one or more blocks of powder, placed in the torpedo chamber in a sheath or covering of extensible material,
tensioned about the powder.
An embodiment of the invention is illusdrawing which shows a longitudinal sectional view of a powder charge such as herein referred to.
In any suitable part of a torpedo, preferably its rear part, there is formed a suitable chamber into which is inserted a metallic envelop 0 which is preferably lined with a non-conductor of heat 6. One end of both envelop and lining is removable and has formed therein one or more gas exhaust orifices a, these orifices being so arranged that the resultant of the escaping gases coincides with the axis of the torpedo. The lined envelop is adapted to contain the powder charge (Z, which may consist of a single block or a plurality of juxtaposed blocks of powder adapted to burn in parallel layers, Prior to the introduction of the powder into the envelop, the former is inserted into a tube 72, of extensible material such as rub her, the diameter of the tube being less than that of the powder whereby the tube is extended or stretched about the blocks.
The outer surface of the powder block should be smooth. Should a block be employed which has a rough or uneven surface, the latter should be coated with a ma- I terial having about the same consistency as rubber solution.
After the powder has been inserted into the tube h, the entire charge is introduced into the envelop 0, appearing as shown in the drawing and being ready for ignition.
The powder charge may, if desired, be ignited at both its ends, or one end only may be left free and the other protected by a layer or coating 2' of a material which is a non conductor of heat. WVhen the powder charge is ignited the same will burn in par allel layers, the combustion being uniform and not extending to the lateral surface of the cylinder, owing to the combined pressure of the gas in the cylinder and the rubber sheath h. The gases will pass 'out through the orifices a, and the reactions thereof in the water will be uniform and the forward propulsion of the torpedo will also be uniform. The gas pressure prevailing in the entire envelop 0 is uniform, and is sufficiently great to counterbalance the pressure of any gas which might attempt to enter between the inner surface of the tube h and the outer surface of the block (Z.
Experience has shown that, if the rubber tube is from 1 to two millimeters thick and if the duration of combustion of the powder block is from 1 to two minutes, one part of the tube (the rear half or two thirds) remains intact in the casing. The tube presents traces of combustion and fusion, but continues to cover that part of the powderblock that has not been burned. The reason for the preservation, intact, of the tube on the unconsumed part of the powder block is based on the following facts: 1. As all powders, except pure nitroglycerin, are not completely combustible because of the insuflicient oxygen content of their molecules, the rubber, which is not readily inflammable, can burn only under the action of the combustible power of the powder. 2. Even though it be assumed that the rubber has in its molecules enough oyygen to burn, and that its own rate of combustion be equal to one half of that of the powder (and as a matter of fact the rate is less than that), it will be apparent that the combustion of powder will progress parallel to the axis twice as quickly as that of the rubber. Thus the tube will serve its intended purpose, namely, to prevent the combustion of the poiwder cylinder from extending on its outer s1 c.
Having thus described my invention what I claim as new and desire to secure by Letters Patent is 1. In a torpedo having a chamber formed therein, the combination with a powder charge in the chamber, of an extensible tensioned sheath about the powder charge.
2. In a torpedo having a chamber formed therein, the combination with a plurality of juxtaposed powder blocks in the chamber, of an extensible tensioned sheath about the powder blocks.
3. In a torpedo having a chamber formed therein, the combination with an orificed metallic envelop in said chamber, of a powder charge in said envelop, and an eX- tensible tensioned sheath about said powder charge.
4. In a torpedo having a chamber formed therein, the combination with an orificed metallic envelop in said chamber, of a lining of material in said envelop which is a non conductor of heat, a powder charge in said envelop, and a sheath of extensible tensioned material about said powder charge.
5. In a torpedo having a chamber formed therein, the combination with an insulation lined metallic envelop in said chamber, of a plurality of juxtaposed powder blocks in the envelop, and a tensioned rubber sheath about said powder blocks.
Signed at Paris, France this twenty-sixth day of October 1908.
EMILE 'BOURDELLES.
W'itnesses:
HENRI MONIN, H. C. Coxn.
US46186408A 1908-11-10 1908-11-10 Torpedo. Expired - Lifetime US958990A (en)

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US46186408A US958990A (en) 1908-11-10 1908-11-10 Torpedo.

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US46186408A US958990A (en) 1908-11-10 1908-11-10 Torpedo.

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2488154A (en) * 1944-10-17 1949-11-15 Us Sec War Strip propellant for rocket projectiles
US2539404A (en) * 1945-05-28 1951-01-30 Aerojet Engineering Corp Solid propellant charge for rocket motors
US2555333A (en) * 1948-05-27 1951-06-05 Joseph A Grand Solid fuel
US2597641A (en) * 1945-12-03 1952-05-20 Gen Electric Pressure-operated starting device
US2637274A (en) * 1946-11-29 1953-05-05 Ici Ltd Power-gas generating device
US2773448A (en) * 1954-01-21 1956-12-11 Brandt Soc Nouv Ets Rocket projectile
US2862447A (en) * 1953-09-14 1958-12-02 Lyon George Albert Rocket structure
US2864311A (en) * 1953-12-07 1958-12-16 Unexcelled Chemical Corp Flares
US2958288A (en) * 1960-11-01 campbell
US3069845A (en) * 1958-03-14 1962-12-25 Mini Of Supply Liner for cooling rocket motors
US3120184A (en) * 1960-04-22 1964-02-04 Universal Match Corp Pyrotechnical devices and methods of making the same
US4448130A (en) * 1982-07-15 1984-05-15 General Dynamics, Pomona Division Packaging kit for pyrotechnic materials loading

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2958288A (en) * 1960-11-01 campbell
US2488154A (en) * 1944-10-17 1949-11-15 Us Sec War Strip propellant for rocket projectiles
US2539404A (en) * 1945-05-28 1951-01-30 Aerojet Engineering Corp Solid propellant charge for rocket motors
US2597641A (en) * 1945-12-03 1952-05-20 Gen Electric Pressure-operated starting device
US2637274A (en) * 1946-11-29 1953-05-05 Ici Ltd Power-gas generating device
US2555333A (en) * 1948-05-27 1951-06-05 Joseph A Grand Solid fuel
US2862447A (en) * 1953-09-14 1958-12-02 Lyon George Albert Rocket structure
US2864311A (en) * 1953-12-07 1958-12-16 Unexcelled Chemical Corp Flares
US2773448A (en) * 1954-01-21 1956-12-11 Brandt Soc Nouv Ets Rocket projectile
US3069845A (en) * 1958-03-14 1962-12-25 Mini Of Supply Liner for cooling rocket motors
US3120184A (en) * 1960-04-22 1964-02-04 Universal Match Corp Pyrotechnical devices and methods of making the same
US4448130A (en) * 1982-07-15 1984-05-15 General Dynamics, Pomona Division Packaging kit for pyrotechnic materials loading

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