US2089853A - Propulsion device - Google Patents

Propulsion device Download PDF

Info

Publication number
US2089853A
US2089853A US100309A US10030936A US2089853A US 2089853 A US2089853 A US 2089853A US 100309 A US100309 A US 100309A US 10030936 A US10030936 A US 10030936A US 2089853 A US2089853 A US 2089853A
Authority
US
United States
Prior art keywords
tube
expansion chamber
diaphragm
chamber
propulsion
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
Application number
US100309A
Inventor
George S Nelson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US100309A priority Critical patent/US2089853A/en
Application granted granted Critical
Publication of US2089853A publication Critical patent/US2089853A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • B63H11/02Marine propulsion by water jets the propulsive medium being ambient water
    • B63H11/04Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
    • B63H11/06Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of reciprocating type

Definitions

  • This invention relates to improvements in propulsion devices for pumping liquids and for propelling boats; and the objects of my improvement are, rst, to provide more efficient and less expensive means for pumping liquids, and for propelling boats; second, to provide means for propelling boats in shallow water without the usual danger of damaging the propelling device; and third to simplify pumping devices and boat propelling mechanisms.
  • Figure 2 is a vertical section of a form of the device wherein certain automatic features are incorporated.
  • FigureS is a vertical section on line A--A in Figures l and 2.
  • Figure 4 is an enlarged part section through the upper and foreward part of the propulsion tube, showing stoppers 39 and 35 more in detail.
  • a propulsion tube I comprising an elongated expansion chamber 2, an elongated momentum chamber 3 which also serves as an inertia chamber, an inlet 4, an outlet 5, and a diaphragm 6, is immersed in a liquid l.
  • Diaphragm 6 is preferably a flexible, elastic and good insulating material.
  • Boiler 9 is sup-A ported'by legs Ill, and is provided with a rebox II, andv is used for producing a gas under pressure in the usual manner for boilers.
  • a cutoff valve is connected in tube 8.
  • Means such as valve I3 in fuel feed tube I4 is provided to regulate the flow of fuel from fuel reservoir I5 to i'lrebox I I.
  • Throttle I6 may be used to control valve I3.
  • valve I2 may be operated by handle I'I.
  • Diaphragm I5 is preferably stretched tightly across the upper part of tube 2 so that it will return more readily to its upper position after the gas is exhausted, thereby allowing a fresh supply of liquid to be drawn in through intake 4.
  • Momentum tube 3 will assist in drawing in a fresh supply of water at intake yl because the momentum of the mass of liquid which has been caused to move rearward in tube 3 will create a partial vacuum in tube 2 and thereby draw in more liquid.
  • valve I2 may again be opened for a moment and the propelling action will be repeated.
  • the propelling action is also a pumping action and Where the term propulsion device is used in this specification and the following claims, it is intended to comprehend therpump also, since the action of the device in each case is the same.
  • diaphragm 6 is preferably attached to the upper wall of tube 2 on all edges of the diaphragm.
  • An exhaust tube I8 connects the rear end of expansion tube 2 to a condenser I9.
  • a valve 29 is connected in tube I8. 35
  • Valve I2 is operated by sprocket 2 I, valve 20 by sprocket 23, and pump 25 by sprocket 22; and sprockets 2I, 22, and 23 are preferably connected by a chain 24 in such a manner that valve 20 will be closed at the moment valve I2 opens.
  • Means such as a paddle wheel 26 may be connected to sprocket 2l by spokes 2'I to rotate sprockets 2I, 22, and 23 when the boat is in motion.
  • Pump 25 is preferably used to draw the fluid up from the condenser through tube 28 and to force it back into boiler 9 through tube 29.
  • one or more elastic stopper bands such as bands 30 and 35, preferably having their foreward edges beveled and free to move, and their rear ends attached either to diaphragm 6 as shown for band 3U, or to tube I as shown for band 35, are stretched tightly Vacross the top of chamber 2 at spaced distances from its front edge. Said stopper bands will reduce the volume of the diaphragm inclosure necessary for closing off intake 4 and will prevent excessive backflow of gas in chamber 2 before intake 4 is closed.
  • stopper band 3B Until stopper band 3B is pulled away from its contact with the top side of tube I, by the down- 5 ward motion of diaphragm 6, said stopper band will be pressed tightly against tube I by the compressed gas in the foreward end of the expansion chamber, and practically no gas will be allowed to pass backward until the foreward end of diaphragm 6 has expanded sufficiently to close off intake l to tube I.
  • Stopper band 35 has a similar action and function to band 30,7the only difference being that the rear end of band 35 is attached to a wall of chamber 2 instead of to diaphragm 6. This will increase the useful back- Vward thrust of diaphragm 6.
  • Y f When high pressure gas is injected into tube 2 it is preferable to use a swinging, reinforcing backing 3
  • the device illustrated in Figure 2 will operate similar to the one illustrated in Figure 1 except for the following. lThe exhaust gas from tube 2 will be transmitted through tube I8 to condenser I9 where the gas Will be condensed to a liquid and pumped through tubes- 28 and 29 back into boiler 9 where it willbe reused.
  • the action of the device may be started by y30 turning sprocket 2I by hand, or by other means,
  • My propulsion device owes its increased-effif c iency over present propulsion mechanisms chiefly to the features mentioned above. Because of its simplicity it will be inexpensive to make.
  • tube I may be made to ⁇ extend a considerably shorter distance below the bottom of the boat than is required by an ordinary propeller blade. For this reason a boat equipped with my propulsion ldevice may be made to navigate in shallower water than is ordinarily possible for small boats. Furthermore my propulsion tube will not be as damageable as the ordinary screw propeller. Y
  • a propulsion tube comprising an expansion chamber having an inertia chamber joined thereto, a diaphragm disposed substantially across Vthe expansion chamber and having its foreward edges tightly attached thereto whereby said chamber is divided intoV a plurality of longitudinal sections, a stopper band having one edge attached to the diaphragm and having a beveled free moving edge, said stopper band being disposed substantially across the eX- pansion chamber a spaced distance from its ends, means whereby a compressed gas may be periodically injected into one section of the expansion chamber, and means whereby the gas'may be exhausted from the expansion chamber.
  • a propulsion tube comprising Aan expansion chamber. having an inertia chamber joined thereto; a diaphragm disposed substantially across the expansion chamber and having all'its edges tightly attached thereto whereby said chamber is divided into a plurality of longitudinal sections, a stopper band having one edge attached ⁇ to the diaphragmand having a beveled free moving edge, said stopper band being disposed substantially across the expansion chamber a spaced distance from its ends, means whereby a compressed Vgas may be periodically injected into oneY section ofthe expansion chamber, an-d means wherebythe gas may be exhausted from the expansion chamber.
  • a propulsion device having an expansion chamber, a diaphragm disposed substantially across the expansion chamber and having its forward edges tightly attached'thereto whereby said chamber is divided into a plurality of longitudinal sections, a stopperA band having one edge attached to the diaphragm andV having a beveled free moving edge, .said stopper band being disposed substantially across the expansion chamber a spaced distance from its ends, means whereby a compressed gas may be periodically injected into one section of the expansion chamber, and means whereby the gas may be exhausted from the expansion chamber.
  • a propulsion tube having an expansion chamber, a diaphragm disposed substantially across the expansion chamber and having its foreward edges tightly attached thereto whereby said chamber is divided into a plurality of longitudinal sections, means whereby a compressed gas may be periodically injected into the forward portion of one section of 'the expansion chamber, whereby the expansive action of the diaphragm will first close off said portion of the expansion chamber and thereafter force the liquid in the expansion chamber rearward as said diaphragm continues to expand progressively rearward, and means whereby the gas may be exhausted from the expansion chamber.
  • propulsion tube comprising an expansion chamber having an inertia chamber joined thereto, means whereby the expansion chamber is divided into a plurality of longitudinal sections, means whereby a compressed gas may be periodically injected into the forward portion of one section of the expansion chamber, whereby the expansive action of the diaphragm will rst close off said portion of the expansion chamber and thereafter force the liquid in the expansion chamber rearward as said diaphragm continues to expand progressively rearward, and means whereby the gas may be exhausted from the expansion chamber.
  • a propulsion tube having an expansion chamber, 'elastic means whereby the expansion chamber is divided into a plurality of longitudinal sections, means whereby compressed gas may be periodically injected into the forward portion of one section of the expansion chamber, whereby the expansive action of the elastic dividing means will rst close oif said portion of the expansion chamber and thereafter force the liquid in the expansion chamber rearward as said elastic dividing means continues to expand progressively rearward, and means whereby the gas may be exhausted from the expansion chamber.
  • a propulsion tube having an expansion chamber, a diaphragm disposed substantially across the expansion chamber and having its foreward edges tightly attached thereto whereby said chamber is divided into a plurality of longitudinal sections, a stopper band having one edge attached to the wall of the expansion chamber and having a beveled free moving edge, said stopper band being disposed substantially across the expansion chamber a spaced distance from its ends, means whereby a compressed gas may be periodically injected into one section of the expansion chamber, and means whereby the gas may be exhausted from the expansion chamber.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Reciprocating Pumps (AREA)

Description

ug. l0, E937., G. s. rlELsoN 2,089,853
PROPULSION DEVICE F11ed sept. 11, 1956 .Fiyi
4H 6 ,ga-@w25 2 6 5 LA f j Patented Aug. l0, 1937 UNITED STATES PATENT OFFICE 7 Claims.
This invention relates to improvements in propulsion devices for pumping liquids and for propelling boats; and the objects of my improvement are, rst, to provide more efficient and less expensive means for pumping liquids, and for propelling boats; second, to provide means for propelling boats in shallow water without the usual danger of damaging the propelling device; and third to simplify pumping devices and boat propelling mechanisms.
I attain these objects by mechanism illustrated in the accompanying drawing, in which- Figure 1 is a vertical section of a simple form of the device. y
, Figure 2 is a vertical section of a form of the device wherein certain automatic features are incorporated.
FigureS is a vertical section on line A--A in Figures l and 2.
Figure 4 is an enlarged part section through the upper and foreward part of the propulsion tube, showing stoppers 39 and 35 more in detail.
Similar numerals refer to similar parts throughout the several views.
In the present invention a propulsion tube I comprising an elongated expansion chamber 2, an elongated momentum chamber 3 which also serves as an inertia chamber, an inlet 4, an outlet 5, and a diaphragm 6, is immersed in a liquid l. Diaphragm 6 is preferably a flexible, elastic and good insulating material.
Near the foreward, or inlet, end of tube I another tube 8, such as a steam tube, connects propulsion tube I to boiler 9. Boiler 9 is sup-A ported'by legs Ill, and is provided with a rebox II, andv is used for producing a gas under pressure in the usual manner for boilers.
- A cutoff valve is connected in tube 8. Means such as valve I3 in fuel feed tube I4 is provided to regulate the flow of fuel from fuel reservoir I5 to i'lrebox I I. Throttle I6 may be used to control valve I3. Similarly valve I2 may be operated by handle I'I.
:When the device is beingused for propelling a boat the intake end 4 of the propulsion tube I is placed foreward.
.C The device illustrated in Figure 1 will operate as follows:
l The liquid in boiler 9 is heated until a high gas pressure is created in said boiler. Valve I2 is then opened for a moment thereby allowing a quantity of compressed gas to forcediaphragm 6 down to position 6a, thereby closing off the intake end 4 of tube I. In Figure 1 the foreward edges of diaphragm 6 are tightly attached to the upper side of expansion chamber 2 as indicated in Figure 3. As the compressed gas in expansion chamber 2 expands, diaphragm 6 will assume a series of positions indicated successively by 6a, 6b, and 6c and the uid in tube I will 5 be forced rearward and the boat will be propelled foreward with an equal force. The inertia of the mass of water in tube 3 will provide an effective force to back up the propelling force in tube 2.
When the diaphragm is in position Bc in Figure l the used gas will be exhausted. Diaphragm I5 is preferably stretched tightly across the upper part of tube 2 so that it will return more readily to its upper position after the gas is exhausted, thereby allowing a fresh supply of liquid to be drawn in through intake 4. Momentum tube 3 will assist in drawing in a fresh supply of water at intake yl because the momentum of the mass of liquid which has been caused to move rearward in tube 3 will create a partial vacuum in tube 2 and thereby draw in more liquid. When tube I is again lled with liquid, valve I2 may again be opened for a moment and the propelling action will be repeated. Clearly the propelling action is also a pumping action and Where the term propulsion device is used in this specification and the following claims, it is intended to comprehend therpump also, since the action of the device in each case is the same. 30
In Figure 2, diaphragm 6 is preferably attached to the upper wall of tube 2 on all edges of the diaphragm. An exhaust tube I8 connects the rear end of expansion tube 2 to a condenser I9. A valve 29 is connected in tube I8. 35
Valve I2 is operated by sprocket 2 I, valve 20 by sprocket 23, and pump 25 by sprocket 22; and sprockets 2I, 22, and 23 are preferably connected by a chain 24 in such a manner that valve 20 will be closed at the moment valve I2 opens. Means such as a paddle wheel 26 may be connected to sprocket 2l by spokes 2'I to rotate sprockets 2I, 22, and 23 when the boat is in motion. Pump 25 is preferably used to draw the fluid up from the condenser through tube 28 and to force it back into boiler 9 through tube 29. Preferably one or more elastic stopper bands such as bands 30 and 35, preferably having their foreward edges beveled and free to move, and their rear ends attached either to diaphragm 6 as shown for band 3U, or to tube I as shown for band 35, are stretched tightly Vacross the top of chamber 2 at spaced distances from its front edge. Said stopper bands will reduce the volume of the diaphragm inclosure necessary for closing off intake 4 and will prevent excessive backflow of gas in chamber 2 before intake 4 is closed. Until stopper band 3B is pulled away from its contact with the top side of tube I, by the down- 5 ward motion of diaphragm 6, said stopper band will be pressed tightly against tube I by the compressed gas in the foreward end of the expansion chamber, and practically no gas will be allowed to pass backward until the foreward end of diaphragm 6 has expanded sufficiently to close off intake l to tube I. Stopper band 35 has a similar action and function to band 30,7the only difference being that the rear end of band 35 is attached to a wall of chamber 2 instead of to diaphragm 6. This will increase the useful back- Vward thrust of diaphragm 6. a Y f When high pressure gas is injected into tube 2 it is preferable to use a swinging, reinforcing backing 3|, attached to the top foreward edge of tube 2, to support the foreward wall of diaphragm 6 against bursting. Y
The device illustrated in Figure 2 will operate similar to the one illustrated in Figure 1 except for the following. lThe exhaust gas from tube 2 will be transmitted through tube I8 to condenser I9 where the gas Will be condensed to a liquid and pumped through tubes- 28 and 29 back into boiler 9 where it willbe reused.
The action of the device may be started by y30 turning sprocket 2I by hand, or by other means,
trolled by throttle `I6 because the faster the fuel.
is supplied to thehrebox the greater will be the pressure in the boiler. To reverse the motion of the boat it is obvi ously only necessary to provide a system of tubes l that will inject the gas flowing through valve I2 into tube 2 through tube I8 and that will exhaust the gas from tube 2'to tube 8 on up through valveZ. Y .Y
In the drawing 32 isthe floor, 33 the bottom, and 34 the back of the boat, or ofthe container for the device. Y 4 Y Due to the fact that diaphragm" 6 and the top of chamber 2 may be made of good insulating material the heat loss of the compressed gas will be small. In the device illustrated in Figure 2, where there is no lossof boiler fluid, a uid having a low boiling point, and low heat of vaporization may be used to advantage. Y The size of chamber 3 may be made to contain a quantity of water of such mass-'as will utilize the energy from tube 2 most efficiently. To explain more fully, if chamber 3 ismade too short, the mass of the water therein will be so l'small that it will be forced out too rapidly for ecient propulsion at ordinary boat speeds; and if chamber 3 is made teo long the water friction against `the walls of the tube vwill be excessive.'Y f f It willv be observed that very few operating parts are necessary inthe present invention and the mechanical losses ordinarilyuaccompanying the use of screw propellers with gasolene or steam engines are entirely avoided.
My propulsion device owes its increased-effif c iency over present propulsion mechanisms chiefly to the features mentioned above. Because of its simplicity it will be inexpensive to make.
It is also evident that tube I may be made to` extend a considerably shorter distance below the bottom of the boat than is required by an ordinary propeller blade. For this reason a boat equipped with my propulsion ldevice may be made to navigate in shallower water than is ordinarily possible for small boats. Furthermore my propulsion tube will not be as damageable as the ordinary screw propeller. Y
No batteries or electric ignition system is necessary to this device.
It is not my intention to limit my device toI the specic form shown and described in this application since other forms involving the same invention will suggest themselves upon reading the abovespecication.
Having described my invention what I now claim as new and desire to secure by Letters Patent of the United States is as follows:
l. In a propulsion device a propulsion tube comprising an expansion chamber having an inertia chamber joined thereto, a diaphragm disposed substantially across Vthe expansion chamber and having its foreward edges tightly attached thereto whereby said chamber is divided intoV a plurality of longitudinal sections, a stopper band having one edge attached to the diaphragm and having a beveled free moving edge, said stopper band being disposed substantially across the eX- pansion chamber a spaced distance from its ends, means whereby a compressed gas may be periodically injected into one section of the expansion chamber, and means whereby the gas'may be exhausted from the expansion chamber.V
2. In a propulsion device a propulsion tube comprising Aan expansion chamber. having an inertia chamber joined thereto;a diaphragm disposed substantially across the expansion chamber and having all'its edges tightly attached thereto whereby said chamber is divided into a plurality of longitudinal sections, a stopper band having one edge attached `to the diaphragmand having a beveled free moving edge, said stopper band being disposed substantially across the expansion chamber a spaced distance from its ends, means whereby a compressed Vgas may be periodically injected into oneY section ofthe expansion chamber, an-d means wherebythe gas may be exhausted from the expansion chamber.
3. In a propulsion device Va propulsion tube having an expansion chamber, a diaphragm disposed substantially across the expansion chamber and having its forward edges tightly attached'thereto whereby said chamber is divided into a plurality of longitudinal sections, a stopperA band having one edge attached to the diaphragm andV having a beveled free moving edge, .said stopper band being disposed substantially across the expansion chamber a spaced distance from its ends, means whereby a compressed gas may be periodically injected into one section of the expansion chamber, and means whereby the gas may be exhausted from the expansion chamber. j i
4. In a propulsion device a propulsion tube'having an expansion chamber, a diaphragm disposed substantially across the expansion chamber and having its foreward edges tightly attached thereto whereby said chamber is divided into a plurality of longitudinal sections, means whereby a compressed gas may be periodically injected into the forward portion of one section of 'the expansion chamber, whereby the expansive action of the diaphragm will first close off said portion of the expansion chamber and thereafter force the liquid in the expansion chamber rearward as said diaphragm continues to expand progressively rearward, and means whereby the gas may be exhausted from the expansion chamber.
5. In a propulsion device a. propulsion tube comprising an expansion chamber having an inertia chamber joined thereto, means whereby the expansion chamber is divided into a plurality of longitudinal sections, means whereby a compressed gas may be periodically injected into the forward portion of one section of the expansion chamber, whereby the expansive action of the diaphragm will rst close off said portion of the expansion chamber and thereafter force the liquid in the expansion chamber rearward as said diaphragm continues to expand progressively rearward, and means whereby the gas may be exhausted from the expansion chamber.
6. In a propulsion device a propulsion tube having an expansion chamber, 'elastic means whereby the expansion chamber is divided into a plurality of longitudinal sections, means whereby compressed gas may be periodically injected into the forward portion of one section of the expansion chamber, whereby the expansive action of the elastic dividing means will rst close oif said portion of the expansion chamber and thereafter force the liquid in the expansion chamber rearward as said elastic dividing means continues to expand progressively rearward, and means whereby the gas may be exhausted from the expansion chamber.
'7. In a propulsion device a propulsion tube having an expansion chamber, a diaphragm disposed substantially across the expansion chamber and having its foreward edges tightly attached thereto whereby said chamber is divided into a plurality of longitudinal sections, a stopper band having one edge attached to the wall of the expansion chamber and having a beveled free moving edge, said stopper band being disposed substantially across the expansion chamber a spaced distance from its ends, means whereby a compressed gas may be periodically injected into one section of the expansion chamber, and means whereby the gas may be exhausted from the expansion chamber.
GEORGE S. NELSON.
US100309A 1936-09-11 1936-09-11 Propulsion device Expired - Lifetime US2089853A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US100309A US2089853A (en) 1936-09-11 1936-09-11 Propulsion device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US100309A US2089853A (en) 1936-09-11 1936-09-11 Propulsion device

Publications (1)

Publication Number Publication Date
US2089853A true US2089853A (en) 1937-08-10

Family

ID=22279129

Family Applications (1)

Application Number Title Priority Date Filing Date
US100309A Expired - Lifetime US2089853A (en) 1936-09-11 1936-09-11 Propulsion device

Country Status (1)

Country Link
US (1) US2089853A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062002A (en) * 1960-08-09 1962-11-06 Robert C Shaffer Underwater propulsion system
US4451210A (en) * 1982-05-14 1984-05-29 Thermacore, Inc. Diaphragm vapor pump
WO1992000221A1 (en) * 1990-07-02 1992-01-09 Pierre Ciraud Hydraulic pulse jet apparatus

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062002A (en) * 1960-08-09 1962-11-06 Robert C Shaffer Underwater propulsion system
US4451210A (en) * 1982-05-14 1984-05-29 Thermacore, Inc. Diaphragm vapor pump
WO1992000221A1 (en) * 1990-07-02 1992-01-09 Pierre Ciraud Hydraulic pulse jet apparatus

Similar Documents

Publication Publication Date Title
US3402555A (en) Steam-jet nozzle for propelling marine vessels
US2412825A (en) Jet propulsion apparatus
US2444318A (en) Jet propulsion system for aircraft
US3163980A (en) Water jet propulsion
US2089853A (en) Propulsion device
US2730065A (en) Hydraulic ship propulsion apparatus
US2696077A (en) Marine jet drive for watercraft
US2699644A (en) Hydropropeller
US2518621A (en) Pump
US2187074A (en) Submarine boat
US3062172A (en) Motor-driven water ski towing device
CN108639296A (en) A kind of hull perforation hydraulic propeller peculiar to vessel
US3079751A (en) Marine propulsion system
FR2428157A1 (en) Solar energy powered engine - uses expanding refrigerant to operate pump, with condenser in water tank to allow liquid refrigerant to return to radiant panel
US115425A (en) Improvement in propulsion of vessels
US3157992A (en) Flow controlling device
US1480836A (en) Propelling device
US2938481A (en) Jet propelled torpedo
US1061110A (en) Propelling mechanism.
US1841200A (en) Preheater for boiler feed water
US907086A (en) Propelling means for vessels.
US1790986A (en) a harris
US441965A (en) Propulsion of vessels
US733010A (en) Apparatus for the propulsion of vessels.
US3898800A (en) Heat engine in the form of a water pulse-jet