US2674946A - Control device for an electric circuit - Google Patents
Control device for an electric circuit Download PDFInfo
- Publication number
- US2674946A US2674946A US231139A US23113951A US2674946A US 2674946 A US2674946 A US 2674946A US 231139 A US231139 A US 231139A US 23113951 A US23113951 A US 23113951A US 2674946 A US2674946 A US 2674946A
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- United States
- Prior art keywords
- movable member
- control device
- movable
- stationary
- fluid
- 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
- 239000012530 fluid Substances 0.000 description 37
- 239000002360 explosive Substances 0.000 description 9
- 239000003792 electrolyte Substances 0.000 description 8
- 239000000126 substance Substances 0.000 description 6
- 238000005192 partition Methods 0.000 description 4
- 230000000977 initiatory effect Effects 0.000 description 3
- 239000011244 liquid electrolyte Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000009877 rendering Methods 0.000 description 2
- 101100072702 Drosophila melanogaster defl gene Proteins 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 235000011149 sulphuric acid Nutrition 0.000 description 1
- 239000001117 sulphuric acid Substances 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C14/00—Mechanical fuzes characterised by the ammunition class or type
- F42C14/04—Mechanical fuzes characterised by the ammunition class or type for torpedoes, marine mines or depth charges
- F42C14/045—Mechanical fuzes characterised by the ammunition class or type for torpedoes, marine mines or depth charges having electric igniters
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/28—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
- F42C15/30—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids of propellant gases, i.e. derived from propulsive charge or rocket motor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/38—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein arming is effected by chemical action
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/40—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected electrically
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/06—Electric contact parts specially adapted for use with electric fuzes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/12—Primers; Detonators electric
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M6/00—Primary cells; Manufacture thereof
- H01M6/30—Deferred-action cells
- H01M6/36—Deferred-action cells containing electrolyte and made operational by physical means, e.g. thermal cells
- H01M6/38—Deferred-action cells containing electrolyte and made operational by physical means, e.g. thermal cells by mechanical means
Definitions
- This invention relates to a control device for controlling an electric circuit, more particularly to a control device for controlling the ignition or detonator circuit for the explosive charge of projectiles, bombs, mines and. the like.
- One of the objects of the present invention is to provide a control device of the general type, above referred to, which is simple and reliable in operation.
- Another object of the invention is to provide a novel and improved control device which permits control of the aforesaid circuit from a remote point.
- Another object of the invention is to provide means for actuating the control device by a fluid under pressure such as gas either developed within the projectile, bomb, mine and the like itself or fed to the control device from an outside source.
- a fluid under pressure such as gas either developed within the projectile, bomb, mine and the like itself or fed to the control device from an outside source.
- Another object of the invention is to provide a a control device of the general type, above referred to, in which an electro-chemical battery,
- control device such as a storage battery
- a storage battery is employed to energize the circuit to be controlled, and which comprises means by which the battery is normally inoperative and is rendered operative for the aforesaid purpose only at the moment control of the circuit is desired.
- the control device can be stored for an indefinite period of time.
- electrochemical batteries whether of the primary or the secondary type, in a condition operative for the delivery of current cannot be stored for a long period of time without loosing their efficiency.
- the possibility of storing the control device for an indefinite period of time is of great importance for the use in explosive devices such as projectiles, bombs, mines, etc.
- the illustrated embodiment of the invention is shown as being mounted in a substantially cylindrical body I.
- This body- is provided with several axially aligned bores of varying diameter.
- Body I may be visualized as part of the rocket.
- the widest bore 2 is provided for an internal thread which serves to receive the war head of the rocket carrying the explosive charge.
- the lower portion 3 of body i (always as seen in the drawing) has an outer thread with which body I is screwed into the housing of the rocket.
- the control device proper comprises a stationary member 8 shown as a sleeve closed on one end.
- Sleeve 8 is fitted in a bore 2! and secured to body I by a bracket 28 threaded into the body I.
- a movable member 4 is fitted within the spaced defined by sleeve 8, and guided by the side wall of the sleeve.
- This movable member is shown as a substantially cylindrical element in which are formed two chambers 5 and B separated by a comparatively thin partition wall 29 made of fragile material.
- Chamber 5 houses a source of current generally designated by 9, in form of a battery either of the primary or the secondary type.
- the battery is shown as a storage battery formed by a plurality of horizontally stacked electrode plates 30. Respective plate terminals are interconnected.
- One set of terminals is connected by a wire l2 to a contact plate I3 and the other set of terminals is connected by a wire M to a contact plate l5.
- a pressure plate 32 having a plurality of spaced holes 33 is fitted between the uppermost electrode and a shoulder 34 of cylinder 4 for holding the electrodes in position.
- An electrolyte 1 for the battery such as diluted sulphuric acid is kept in the upper chamher 5.
- precautions must be taken to prevent a corrosion of the walls of chamber 6.
- These walls may be lined with ceramic or any other suitable material.
- the entire cylinder 4 or at least wall 29 thereof may be made of ceramic material.
- a control member generally designated by 35 serves to close chamber 6. This control memportion 36 from which radially extends a flange ing member 42' into "to openings 43.
- portion I l integral with cylinder 36, as shown, or fixed thereto by any suitable means.
- the upper end of cylinder 36 abuts against the closed end of sleeve 8 and the lower end of the cylinder faces wall 29 closely adjacent thereto or slightly touching wall 29.
- the outer rim of flange ii abuts against the face wall of cylinder 4 thereby holding the entire assembly in the illustrated position.
- Flange II includes a weakened portion indicated as a fracture initiating annular groove 31 near cylinder 36 the purpose of which will be more fully explained hereinafter.
- a filler screw 38 serves to fill chamber 6 with electrolyte.
- Contact plates I3 and l are secured to the upper face wall of flange i! and cooperate with contact pins 39 and 40. These contact pins are connected to wires I8 and I 9 which should be visualized as leading to the circuit to be controlled, such as a detonator circuit. Inasmuch as this control circuit is presumed to b of conventionaldesign it believed that a detailed description 'or illustrationjthereof, is not necessary for the'understanding' of the invention.
- This screw memberf is provided with 'a" pluralit y of spacedbores 43 through which fiuid'underpressure may be admitted into a space '44jtoactilpondeflection member 42.
- the deflection member is convexly curved towardopenings 43 and bore 25 provides 's'umcient space for deflecta concave position relative
- the operational fluid may be gas under' pressure developed within the rocket itselfor fed" through openings 43 from anoutside source.
- a passage between the two chambers can be established by other means than fracturing wall 29, for instance cylinder 36 may open a strong valve.
- fracturing of a wall appears to be the safest method.
- a control device for controllingan, electric circuit comprising a stationarily. mounted member, contact means included in said circuit to be controlled and supported on saidmember, a movable support member movablymounted relative to said stationarilysupportedmember, movable contact means mounted for movement in unison with the movable member, asource of current connected with saidfr'novable contact means, rigid retaining means abuttingag ainst th stationary member and against the movable member for rigidly retaining the latter in a position in which said two contactmeans are disengaged from each other, said retaining means being arranged to fracture in response to .a predetermined pressure applied to thesame, and fluid inlet means fol-admitting a flow of fluid under.
- said retaining means comprise a rigid member between the stationary member and the movable member holding the said members spaced apart in thecontact disengaging position and including a weakened portion designed to fracture by said fluid pressure for permitting movement of the movable member into the said contact engaging position, the said rigid. member supporting the movable. contact means.
- a control device as defined in Ql im v1 in combination with a stationarily mounted deflection member, one side of said deflection member being in movement transmitting engagement with said movable member, the other side of the defl'e ction member communicating with said fluid inlet means, whereby the aforesaid fluid pressure causes deflection of the deflection member resulting in movement of, the movable member upon a fracture of said retaining means, by the pressure exerted by the movable member.
- the said deflection member is in form or a disc which is normally biased into a position convexly curved toward the fluid inlet means and flexible into a concave position relative to the fluid inlet means by the pressure of said fluid.
- a control device for controlling an electric circuit comprising a stationary member, a movable member mounted for movement relative to the stationary member and including a chamber, electrodes of an electro-chemical battery housed within said second chamber, the pole terminals of said electrodes being adapted to be connected with said circuit to be controlled, said movable member being shaped and disposed in a rest po sition relative to the stationary member so as to form a second chamber between the two mem- 1 bers adapted to receive therein a liquid electrolyte for the battery, retaining means yieldably retaining the movable member in the aforesaid rest position, fluid inlet means for admitting a flow of fluid under pressure into the device, the
- a control device for controlling an electric circuit comprising a stationary member, a movable member mounted for movement relative to the stationary member and including a chamber, electrodes of an electro-chemical battery housed within said chamber, the pole terminals of said electrodes being adapted to be connected with said circuit to be controlled, said movable member being shaped and disposed in a rest position relative to the stationary member so as to form a second chamber between the two members adapted to receive therein a liquid electrolyte for the battery, a control member positioned between the stationary member and the movable member and abutting against the stationary member, said control member having a yieldable first portion engaging the movable member when the said member is in the rest position for yieldably holding the movable member in the said position and a rigid second portion engageable with the movable member in response to a movement thereof toward the stationary member, said second portion being arranged partially to fracture said movable member upon engagement therewith, thereby opening a passageway between the two chambers upon the aforesaid movement
- control member includes as yieldable first portion a weakened section for initiating a, fracture of said first portion in response to a predetermined pressure exerted upon said first portion by the movable member as a result of fluid pressure applied to the movable member.
- control member comprises a cylindrical element abutting with one end against said stationary member and facing with the other end said partition wall, said cylindrical element forming the said second portion engageable with the partition wall for fracturing the same, the said first portion being formed by a flange element secured to the cylindrical element radially extending therefrom, said flange member abutting against the movable element in the aforesaid rest position thereof and including said fracture initiating weakened section.
- a control device for controlling the detonator circuit of an explosive device of the type described comprising a stationarily mounted member, contact means included in said circuit to be controlled and supported on said member, a movable support member movably mounted relative to said stationarily supported member, second contact means movable in unison with the movable member, a source of current connected with said second contact means, retaining means abutting against the stationary member and against the movable member for retaining the latter in a "rest position in which said Contact means are disengaged from each other, said retaining means being arranged to fracture in response to a predetermined pressure applied to the same, and
- a control device for controlling the detonator circuit of an explosive device of the type described comprising a stationary member, a movable member mounted for movement relative to the stationary member and including a chamber, electrodes of an electro-chemical battery housed within said chamber, the pole terminals of said electrodes being adapted to be connected with said circuit to be controlled, said movable member being shaped and disposed in a rest position relative to the stationary member so as to form a chamber between the two members adapted to receive therein a liquid electrolyte for the battery, a control member positioned between the stationary member and the movable member and abutting against the stationary member, said control member having a yieldable first portion engaging the movable member when the said member is in the rest position for yieldably holding the movable member in the said position and a rigid second portion engageable with the movable the control device, the said flow of pressure fluid being applied to said movable member so as tomove the same toward the stationary member against the resistance of said first portion of the control member, said
- said stationary member comprises a sleeve closed on one end, and wherein said movable member is slidably guided within the sleeve,
- a control device as defined in claim 1 in combination with a deflection member in form of a rounded diaphragm stationarily held along its periphery, the inwardly curved side of the diaphragm being in movement transmitting engagement with said movable member and the outwardly curved side communicating with said fluid inlet means, application of fluid pressure above a predetermined value to said "outwardly curved side of the diaphragm causing the same abruptly to reverse its curvature resulting in a contact closing movement of the movable member upon a fracture of the retaining means by the pressure exerted by the movable member.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Ocean & Marine Engineering (AREA)
- Combustion & Propulsion (AREA)
- Filling, Topping-Up Batteries (AREA)
Description
April 3, 1954 K. E. w. HJELM CONTROL DEVICE FOR AN ELECTRIC CIRCUIT Filed June 12, 1951 INVENTOR. KARL ERIK WALDEMAR HJELM BY M453. my
ATTORNEY.
Patented Apr. 13, 1954 CONTROL DEVICE FOR AN ELECTRIC CIRCUIT Karl Erik Waldemar Hjelm, Bofors, Sweden, as-
signor to Aktiebolaget Bofors, Bofors, Sweden, a Swedish corporation Application June 12, 1951, Serial No. 231,139
20 Claims. 1
This invention relates to a control device for controlling an electric circuit, more particularly to a control device for controlling the ignition or detonator circuit for the explosive charge of projectiles, bombs, mines and. the like.
One of the objects of the present invention is to provide a control device of the general type, above referred to, which is simple and reliable in operation.
Another object of the invention is to provide a novel and improved control device which permits control of the aforesaid circuit from a remote point.
Another object of the invention is to provide means for actuating the control device by a fluid under pressure such as gas either developed within the projectile, bomb, mine and the like itself or fed to the control device from an outside source.
Another object of the invention is to provide a a control device of the general type, above referred to, in which an electro-chemical battery,
such as a storage battery, is employed to energize the circuit to be controlled, and which comprises means by which the battery is normally inoperative and is rendered operative for the aforesaid purpose only at the moment control of the circuit is desired. This has the advantage that the control device can be stored for an indefinite period of time. As is well known, electrochemical batteries, whether of the primary or the secondary type, in a condition operative for the delivery of current cannot be stored for a long period of time without loosing their efficiency. Obviously, the possibility of storing the control device for an indefinite period of time is of great importance for the use in explosive devices such as projectiles, bombs, mines, etc.
Other and further objects, features and advantages of the invention will be pointed out hereinafter and set forth in the appended claims forming part of the application.
In the single figure of the accompanying drawing a sectional fragmentary view of a projectile,
such as a rocket, equipped with a control device according to the invention is shown by way of illustration and not by way of limitation.
Referring now to the figure in detail, the illustrated embodiment of the invention is shown as being mounted in a substantially cylindrical body I. This body-is provided with several axially aligned bores of varying diameter. Body I may be visualized as part of the rocket. For
this purpose, the widest bore 2 is provided for an internal thread which serves to receive the war head of the rocket carrying the explosive charge. The lower portion 3 of body i (always as seen in the drawing) has an outer thread with which body I is screwed into the housing of the rocket.
The control device proper comprises a stationary member 8 shown as a sleeve closed on one end. Sleeve 8 is fitted in a bore 2! and secured to body I by a bracket 28 threaded into the body I. Within the spaced defined by sleeve 8, and guided by the side wall of the sleeve, a movable member 4 is fitted. This movable member is shown as a substantially cylindrical element in which are formed two chambers 5 and B separated by a comparatively thin partition wall 29 made of fragile material. Chamber 5 houses a source of current generally designated by 9, in form of a battery either of the primary or the secondary type. The battery is shown as a storage battery formed by a plurality of horizontally stacked electrode plates 30. Respective plate terminals are interconnected. One set of terminals is connected by a wire l2 to a contact plate I3 and the other set of terminals is connected by a wire M to a contact plate l5. Plates at rest upon a support plate 3| slidably fitted in a bore of body and supported by a second plate 20 also axially slidably fitted in the bore for plate 3|. A pressure plate 32 having a plurality of spaced holes 33 is fitted between the uppermost electrode and a shoulder 34 of cylinder 4 for holding the electrodes in position.
When the control device is in the illustrated inactive or rest position, space 5 in which the I electrode plates 30 are housed is dry. As a result, plates 30 can be stored for an indefinite period of time in a chemical condition ready for the delivery of current without undergoing any change. It is well known that a charged storage battery filled with electrolyte deteriorates in a comparatively short time. The same is true for so-called dry cell batteries.
An electrolyte 1 for the battery, such as diluted sulphuric acid is kept in the upper chamher 5. Of course, precautions must be taken to prevent a corrosion of the walls of chamber 6. These walls may be lined with ceramic or any other suitable material. The entire cylinder 4 or at least wall 29 thereof may be made of ceramic material.
A control member generally designated by 35 serves to close chamber 6. This control memportion 36 from which radially extends a flange ing member 42' into "to openings 43.
before described, is
Let it be assumed that the entire assembly is in the illustrated position and that the explosive plates 39.
portion I l integral with cylinder 36, as shown, or fixed thereto by any suitable means. The upper end of cylinder 36 abuts against the closed end of sleeve 8 and the lower end of the cylinder faces wall 29 closely adjacent thereto or slightly touching wall 29. The outer rim of flange ii abuts against the face wall of cylinder 4 thereby holding the entire assembly in the illustrated position. Flange II includes a weakened portion indicated as a fracture initiating annular groove 31 near cylinder 36 the purpose of which will be more fully explained hereinafter.
A filler screw 38 serves to fill chamber 6 with electrolyte.
Contact plates I3 and l are secured to the upper face wall of flange i! and cooperate with contact pins 39 and 40. These contact pins are connected to wires I8 and I 9 which should be visualized as leading to the circuit to be controlled, such as a detonator circuit. Inasmuch as this control circuit is presumed to b of conventionaldesign it believed that a detailed description 'or illustrationjthereof, is not necessary for the'understanding' of the invention.
As will be notedfcontats lt, as nd 15,, 40 respectively are disengaged from each other when the control 'device'is thejillustrated position. The aforementioned support plate abuts against one end of a ,pin Zl axially slidable in a bore 4| of body]. The lower end of pin 2| abuts against a deflection mer nber generally designated by 4'2." Ifhis deflection member comprises a flexible disc 24, sheathed on both sides by linings 22 and 23. g The deflection member 42 is fitted in a box-e of body I inwhich it is secured by' a' screw member 26. This screw memberfis provided with 'a" pluralit y of spacedbores 43 through which fiuid'underpressure may be admitted into a space '44jtoactilpondeflection member 42. Aswi ll be noted, the deflection member is convexly curved towardopenings 43 and bore 25 provides 's'umcient space for deflecta concave position relative The operational fluid may be gas under' pressure developed within the rocket itselfor fed" through openings 43 from anoutside source.
The operation of the control device, as hereinas follows:
charge of the rocketj shall be set off by energizing the detonator circuit. Then, gas under pressure is directed through openings 43 against deflection member' lz. Ifthis gaspressure is strong enough,
' nent contact connection would be provided a fracthe'deflection member, will be d fieetedintoits concave position thereby exerting an upward pressure upon pin 2 plates flfll and 3| and cylinder 4 with theelctrode plates housed, therein. Qbviously, controlpi'e' nbertfi cannot yield. As a result,'fiar'ige 'i I will break, us 3?. Cylinders and the'associatd parts will now move upwardly with the result: that'contact plates l3 and I5 come in engagement with contact pins 39 and 4c. Furthermore,-'the lower end bfcylinderiiifi which isli'e'ldstationa'ry will press against the 'thin wall ZSfthereby fracturing the same. The electrolyte 1 will now now through openings 33 of plate 32 and conic in contact with electrode Consequentlyfthe" battery 9 becomes operative for thedelivery of current and can energize the detonator circuit through wires l8 and I9. ,L 1,
It will be evident from the previous description that it would alsobe possible topro'vi'de a uall along groove ture of the electrolyte chamber alone would set oif the charge.
It will further be apparent that a passage between the two chambers can be established by other means than fracturing wall 29, for instance cylinder 36 may open a strong valve. However, again fracturing of a wall appears to be the safest method.
While theinventionhas. been. described in detail" with respect 'to a certain. now. preferredexample and embodiment of the invention it will jbe un derstood by those skilled in the an after understanding theinvention, that various changes and modifications may be made without departing from the spirit, and scope of theinvention, and it,is intended, therefore, to cover allsuch changes and 'modifications in the appended claims.
What is claimed. as new and desired tobe secured by Letters Patent is:
l. A control device for controllingan, electric circuit, comprising a stationarily. mounted member, contact means included in said circuit to be controlled and supported on saidmember, a movable support member movablymounted relative to said stationarilysupportedmember, movable contact means mounted for movement in unison with the movable member, asource of current connected with saidfr'novable contact means, rigid retaining means abuttingag ainst th stationary member and against the movable member for rigidly retaining the latter in a position in which said two contactmeans are disengaged from each other, said retaining means being arranged to fracture in response to .a predetermined pressure applied to thesame, and fluid inlet means fol-admitting a flow of fluid under. pressure into the device, the said flow of pressure fluid being applied to said movable member so as to cause a fracture of the retaining means and to move the movable member into a position in which said two contact meansrare in engagement with each other for connecting said source of current to said stationary contact means.
2. A control device as defined in claim 1, wherein said retaining means comprise a rigid member between the stationary member and the movable member holding the said members spaced apart in thecontact disengaging position and including a weakened portion designed to fracture by said fluid pressure for permitting movement of the movable member into the said contact engaging position, the said rigid. member supporting the movable. contact means.
3. A control device as defined in Ql im v1 in combination with a stationarily mounted deflection member, one side of said deflection member being in movement transmitting engagement with said movable member, the other side of the defl'e ction member communicating with said fluid inlet means, whereby the aforesaid fluid pressure causes deflection of the deflection member resulting in movement of, the movable member upon a fracture of said retaining means, by the pressure exerted by the movable member.
4. A control device as defined in claim 3.
. wherein the said deflection member is in form or a disc which is normally biased into a position convexly curved toward the fluid inlet means and flexible into a concave position relative to the fluid inlet means by the pressure of said fluid.
5. A control device as defined in claim 1, wherein the said source of current comprises an electro-chemical battery and is supported by the movable member for movement in unison therewith.
6. A control device for controlling an electric circuit, comprising a stationary member, a movable member mounted for movement relative to the stationary member and including a chamber, electrodes of an electro-chemical battery housed within said second chamber, the pole terminals of said electrodes being adapted to be connected with said circuit to be controlled, said movable member being shaped and disposed in a rest po sition relative to the stationary member so as to form a second chamber between the two mem- 1 bers adapted to receive therein a liquid electrolyte for the battery, retaining means yieldably retaining the movable member in the aforesaid rest position, fluid inlet means for admitting a flow of fluid under pressure into the device, the
said pressure fluid being applied to said movable member for moving the same toward the stationary member, and stationary abutment means engageable with the movable member upon the aforesaid movement thereof and arranged to open upon engagement with the movable member a passageway through said movable member connecting said chamber for the electrolyte with said chamber housing said electrodes, the said passageway providing for a discharge of the electrolyte into said chamber housing the electrodes, thereby rendering the battery operative for a fiow of current in the circuit to be controlled.
'7. A control device for controlling an electric circuit, comprising a stationary member, a movable member mounted for movement relative to the stationary member and including a chamber, electrodes of an electro-chemical battery housed within said chamber, the pole terminals of said electrodes being adapted to be connected with said circuit to be controlled, said movable member being shaped and disposed in a rest position relative to the stationary member so as to form a second chamber between the two members adapted to receive therein a liquid electrolyte for the battery, a control member positioned between the stationary member and the movable member and abutting against the stationary member, said control member having a yieldable first portion engaging the movable member when the said member is in the rest position for yieldably holding the movable member in the said position and a rigid second portion engageable with the movable member in response to a movement thereof toward the stationary member, said second portion being arranged partially to fracture said movable member upon engagement therewith, thereby opening a passageway between the two chambers upon the aforesaid movement of the movable member, opening of the said passageway providing for discharge of the electrolyte into the chamber housing the electrodes, thereby rendering the battery operative for a flow of current in the circuit to be controlled, and fluid inlet means for admitting a flow of fluid under pressure into said device, the said flow'of pressure fluid being applied to said movable member so as to move the same toward the stationary member against the resistance of the said first portion of the control member.
8. A control device as defined in claim 7, wherein said control member includes as yieldable first portion a weakened section for initiating a, fracture of said first portion in response to a predetermined pressure exerted upon said first portion by the movable member as a result of fluid pressure applied to the movable member.
9. A control device as defined in claim 8, wherein said movable member is substantially in form of a hollow cylinder including a transverse partition wall separating the said two chambers, and wherein said rigid second portion of the control member is positioned and arranged to engage said wall for fracturing the same in a response to the aforesaid movement of the movable member toward the stationary member, thereby establishing the said passageway between the two chambers.
10. A control device as defined in claim 9, wherein said control member comprises a cylindrical element abutting with one end against said stationary member and facing with the other end said partition wall, said cylindrical element forming the said second portion engageable with the partition wall for fracturing the same, the said first portion being formed by a flange element secured to the cylindrical element radially extending therefrom, said flange member abutting against the movable element in the aforesaid rest position thereof and including said fracture initiating weakened section.
11. A control device as defined in claim 6, wherein a stationarily mounted deflection member is disposed between said fluid inlet means and said movable member, said latter member being operatively coupled with the deflection member for transmitting movements of the latter to the movable member, said fluid inlet means being arranged to direct the fiow of fluid under pressure against the deflection member for deflecting the same, thereby causing the aforesaid movement of the movable member.
12. A control device as defined in claim 6, wherein a first contact means is supported on said stationary member and a second contact means is supported on said movable member for movement in unison therewith, the said second contact means being connected with said electrodes of the battery, the two contact means being disengaged one from the other when the movable member is in the aforesaid rest position and engage each other when the movable memher is moved toward the stationary member, thereby connecting the electrodes with the contact means on the stationary member, the said latter contact means being arranged to be connected with the circuit to be controlled.
13. A control device for controlling the detonator circuit of an explosive device of the type described, the said control device comprising a stationarily mounted member, contact means included in said circuit to be controlled and supported on said member, a movable support member movably mounted relative to said stationarily supported member, second contact means movable in unison with the movable member, a source of current connected with said second contact means, retaining means abutting against the stationary member and against the movable member for retaining the latter in a "rest position in which said Contact means are disengaged from each other, said retaining means being arranged to fracture in response to a predetermined pressure applied to the same, and
fluid inlet means for admitting a flow of fluid under pressure into the device, the said flow of pressure fluid being applied to said movable 'member so as to fracture the retaining means and to move the movable member into a position in which the two said contact means are in engagement with each other for connecting said source of current to said stationary contact means, said stationary member and said movable member being mounted in a body forming part of the explosive device.
14. A control device for controlling the detonator circuit of an explosive device of the type described, the said control device comprising a stationary member, a movable member mounted for movement relative to the stationary member and including a chamber, electrodes of an electro-chemical battery housed within said chamber, the pole terminals of said electrodes being adapted to be connected with said circuit to be controlled, said movable member being shaped and disposed in a rest position relative to the stationary member so as to form a chamber between the two members adapted to receive therein a liquid electrolyte for the battery, a control member positioned between the stationary member and the movable member and abutting against the stationary member, said control member having a yieldable first portion engaging the movable member when the said member is in the rest position for yieldably holding the movable member in the said position and a rigid second portion engageable with the movable the control device, the said flow of pressure fluid being applied to said movable member so as tomove the same toward the stationary member against the resistance of said first portion of the control member, said stationary member and said movable member being mounted in a body fbrming part or the explosive device, said pressure fluid being a gas developed by the explosive device.
15. A control device as defined in claim 14,
wherein said stationary member comprises a sleeve closed on one end, and wherein said movable member is slidably guided within the sleeve,
the closed end therof abutting against the control member.
16. A control device as defined in claim 1, in combination with a deflection member in form of a rounded diaphragm stationarily held along its periphery, the inwardly curved side of the diaphragm being in movement transmitting engagement with said movable member and the outwardly curved side communicating with said fluid inlet means, application of fluid pressure above a predetermined value to said "outwardly curved side of the diaphragm causing the same abruptly to reverse its curvature resulting in a contact closing movement of the movable member upon a fracture of the retaining means by the pressure exerted by the movable member.
17. A control device as defined in claim 7, wherein an abutment member is disposed on the side of the diaphragm opposite to the fluid inlet means and positioned so as to limit a further deflection of the diaphragm by fluid pressure upon completion of the contact closing movement of the movable member.
18. A control device as defined in claim 17, wherein the said diaphragm is initially convexly curved toward the fluid inlet means and flexible in a concave position relative to the fluid inlet means by fluid pressure applied to the outwardly curved side of the diaphragm.
19. A control device as defined in claim 7, in combination with a deflection member in form of a rounded diaphragm stationarily held along its periphery, the inwardly curved side of the dibeing in movement transmitt ng engagement with said movable member and the outwardly curved side communicating with said fluid inlet means, application of fluid pressure above a predetermined value to said outwardly curved side of the diaphragm causing the same abruptly to reverse its curvature resulting in a movement of the movable member causing engagement between the movable member and the said rigid portion of the control member effecting a partial fracture of the movable member.
20. A control device as defined in claim 19. wherein an abutment member is disposed on the side of the diaphragm opposite to the fluid inlet means and positioned so as to limit a further deflection of the diaphragm by fluid pressure upon completion of the movement of the movable member eiiecting a partial fracture of the same.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 1,474,548 Pape Nov. 20, 1923 FOREIGN PATENTS Number Country Date 156,814 Great Britain Jan. 20, 1921
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US231139A US2674946A (en) | 1950-06-14 | 1951-06-12 | Control device for an electric circuit |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE290618X | 1950-06-14 | ||
US231139A US2674946A (en) | 1950-06-14 | 1951-06-12 | Control device for an electric circuit |
Publications (1)
Publication Number | Publication Date |
---|---|
US2674946A true US2674946A (en) | 1954-04-13 |
Family
ID=26656221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US231139A Expired - Lifetime US2674946A (en) | 1950-06-14 | 1951-06-12 | Control device for an electric circuit |
Country Status (1)
Country | Link |
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US (1) | US2674946A (en) |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2787650A (en) * | 1953-11-20 | 1957-04-02 | Marie Bernard Recope De Hubert | Device for priming electric batteries |
US2798111A (en) * | 1952-12-20 | 1957-07-02 | Yardney International Corp | Electric power supply system |
US2814662A (en) * | 1953-12-14 | 1957-11-26 | Union Carbide Corp | Deferred action galvanic cell |
US2852592A (en) * | 1953-11-04 | 1958-09-16 | Accumulators Fixes Et De Tract | Deferred action primary cells |
US2905741A (en) * | 1956-05-01 | 1959-09-22 | Hughes Aircraft Co | Reserve primary battery |
US2937220A (en) * | 1956-10-23 | 1960-05-17 | Electric Storage Battery Co | Electrical batteries |
US2985702A (en) * | 1957-10-17 | 1961-05-23 | Union Carbide Corp | Deferred action battery |
US2989737A (en) * | 1959-11-17 | 1961-06-20 | Theodore J Collum | Fire alarm apparatus |
US3018314A (en) * | 1954-03-16 | 1962-01-23 | Yardney International Corp | Filling mechanism for deferred-action batteries |
US3075034A (en) * | 1958-06-09 | 1963-01-22 | Yardney International Corp | Activator for dry-charged electrochemical batteries and the like |
US3139356A (en) * | 1961-08-05 | 1964-06-30 | Yuasa Battery Co Ltd | Deferred-action type silver battery |
US3173811A (en) * | 1959-08-05 | 1965-03-16 | Yardney International Corp | Electric battery and activation device therefor |
US3284242A (en) * | 1961-11-21 | 1966-11-08 | Gen Motors Corp | Deferred action battery |
US3337370A (en) * | 1963-10-15 | 1967-08-22 | Union Carbide Corp | Deferred-action electric cell |
US3416451A (en) * | 1967-09-11 | 1968-12-17 | Air Force Usa | Battery activator system |
US4196264A (en) * | 1977-10-18 | 1980-04-01 | U.S. Philips Corporation | Acceleration activated battery |
EP0014401A1 (en) * | 1979-01-31 | 1980-08-20 | DIEHL GMBH & CO. | Electric igniter for igniting detonating cords, delay compositions and detonators |
EP1471326A1 (en) * | 2003-04-26 | 2004-10-27 | Rheinmetall W & M GmbH | Electric switch for a projectile fuze, which switch is activated by gas pressure |
DE10354012B4 (en) * | 2003-04-26 | 2005-06-30 | Rheinmetall W & M Gmbh | Gas pressure switch for an ignition and safety device of ammunition |
DE10001886B4 (en) * | 2000-01-19 | 2007-02-15 | Rheinmetall Waffe Munition Gmbh | From a gun fireable bullet with an acted upon by propellant gases, acting on a detonator activating device transmission element |
DE10026885B4 (en) * | 2000-05-30 | 2007-02-15 | Rheinmetall Waffe Munition Gmbh | From a gun fireable bullet with an acted upon by propellant gases, acting on a detonator activating device transmission element |
WO2020122803A1 (en) * | 2018-12-14 | 2020-06-18 | Saab Ab | Delay unit for a projectile |
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GB156814A (en) * | 1917-04-23 | 1921-01-20 | Sidney James Williams | Improvements in and relating to the ignition apparatus of sub-marine mines |
US1474548A (en) * | 1920-09-30 | 1923-11-20 | Firm Carbonit Ag | Fuse |
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Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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GB156814A (en) * | 1917-04-23 | 1921-01-20 | Sidney James Williams | Improvements in and relating to the ignition apparatus of sub-marine mines |
US1474548A (en) * | 1920-09-30 | 1923-11-20 | Firm Carbonit Ag | Fuse |
Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2798111A (en) * | 1952-12-20 | 1957-07-02 | Yardney International Corp | Electric power supply system |
US2852592A (en) * | 1953-11-04 | 1958-09-16 | Accumulators Fixes Et De Tract | Deferred action primary cells |
US2787650A (en) * | 1953-11-20 | 1957-04-02 | Marie Bernard Recope De Hubert | Device for priming electric batteries |
US2814662A (en) * | 1953-12-14 | 1957-11-26 | Union Carbide Corp | Deferred action galvanic cell |
US3018314A (en) * | 1954-03-16 | 1962-01-23 | Yardney International Corp | Filling mechanism for deferred-action batteries |
US2905741A (en) * | 1956-05-01 | 1959-09-22 | Hughes Aircraft Co | Reserve primary battery |
US2937220A (en) * | 1956-10-23 | 1960-05-17 | Electric Storage Battery Co | Electrical batteries |
US2985702A (en) * | 1957-10-17 | 1961-05-23 | Union Carbide Corp | Deferred action battery |
US3075034A (en) * | 1958-06-09 | 1963-01-22 | Yardney International Corp | Activator for dry-charged electrochemical batteries and the like |
US3173811A (en) * | 1959-08-05 | 1965-03-16 | Yardney International Corp | Electric battery and activation device therefor |
US2989737A (en) * | 1959-11-17 | 1961-06-20 | Theodore J Collum | Fire alarm apparatus |
US3139356A (en) * | 1961-08-05 | 1964-06-30 | Yuasa Battery Co Ltd | Deferred-action type silver battery |
US3284242A (en) * | 1961-11-21 | 1966-11-08 | Gen Motors Corp | Deferred action battery |
US3337370A (en) * | 1963-10-15 | 1967-08-22 | Union Carbide Corp | Deferred-action electric cell |
US3416451A (en) * | 1967-09-11 | 1968-12-17 | Air Force Usa | Battery activator system |
US4196264A (en) * | 1977-10-18 | 1980-04-01 | U.S. Philips Corporation | Acceleration activated battery |
EP0014401A1 (en) * | 1979-01-31 | 1980-08-20 | DIEHL GMBH & CO. | Electric igniter for igniting detonating cords, delay compositions and detonators |
DE10001886B4 (en) * | 2000-01-19 | 2007-02-15 | Rheinmetall Waffe Munition Gmbh | From a gun fireable bullet with an acted upon by propellant gases, acting on a detonator activating device transmission element |
DE10026885B4 (en) * | 2000-05-30 | 2007-02-15 | Rheinmetall Waffe Munition Gmbh | From a gun fireable bullet with an acted upon by propellant gases, acting on a detonator activating device transmission element |
EP1471326A1 (en) * | 2003-04-26 | 2004-10-27 | Rheinmetall W & M GmbH | Electric switch for a projectile fuze, which switch is activated by gas pressure |
DE10354012B4 (en) * | 2003-04-26 | 2005-06-30 | Rheinmetall W & M Gmbh | Gas pressure switch for an ignition and safety device of ammunition |
US20050188877A1 (en) * | 2003-04-26 | 2005-09-01 | Rheinmetall W & M Gmbh | Gas pressure switch |
US7150228B2 (en) | 2003-04-26 | 2006-12-19 | Rheinmetall W & M Gmbh | Gas pressure switch |
WO2020122803A1 (en) * | 2018-12-14 | 2020-06-18 | Saab Ab | Delay unit for a projectile |
US11598619B2 (en) | 2018-12-14 | 2023-03-07 | Saab Ab | Delay unit for a projectile |
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