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US2419685A - Electric switch - Google Patents

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US2419685A
US2419685A US568173A US56817344A US2419685A US 2419685 A US2419685 A US 2419685A US 568173 A US568173 A US 568173A US 56817344 A US56817344 A US 56817344A US 2419685 A US2419685 A US 2419685A
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Prior art keywords
switch
diaphragm
pressure
reservoir
chamber
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US568173A
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John H Leslie
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Stewart Warner Corp
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Stewart Warner Corp
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H35/00Switches operated by change of a physical condition
    • H01H35/24Switches operated by change of fluid pressure, by fluid pressure waves, or by change of fluid flow
    • H01H35/26Details
    • H01H35/2678Means to isolate oscillating component of pressure

Definitions

  • the present Vinvention relates to pressure actuated switches'andparticularly to verysensiltive pressure actuated ⁇ snap switches.
  • switches are ⁇ utilized to control heaters in aircraft.
  • the switchesv are in- .tended to prevent operation of the heater unless a certain lair pressurer exists to create a minimum .”ilowof air through the heating apparatus.
  • the switches may be setto turn theheater ⁇ on vwhen ⁇ the air pressurawhichmayybe the air blast (propeller blast) from thepropeller, hasy a pressure of At sirable fluttering, or intermittent operation 'of the switches.
  • the primary object of the present invention is to provide a new and improved sensitive pressure actuated switch.
  • Another object of the present invention is to provide a new and improved sensitive pressure l,actuated electrical switch which maybe actuated at very low pressures and which is prevented from operating intermittently in response .to vibrations.
  • cup-shaped' housing 22
  • Fig. 2 is a transverse lcross sectional view taken :along the line2-2 of Fig. l.
  • the switch of thepresent invention which is indicated as a Ywhole by reference character I0, includesV two mainrparts.
  • the firsty is a circuit controlling switch I2 and the second a hydraulic cushioningy meansr i4 located in cooperative relationship with theswitch actuating means and eiective to prevent operation of the switch in response to vibrations over a wide range of yangular positions lof the device.
  • the ⁇ switchIZvv may be a snap switch of conventional construction except that 'it should be designed to operate at'about-one and one-half or two inches of water pressure, and with a presrurerdifferential oiabout one-half inch. VIn other words, theswitch should be a sensitive one.
  • the circuit controlling contacts of the switch are not illustrated but they may be mounted within a suitable switch casing AI6 Yand are operable through suitable switchoperating means, such as a. finger I3 projecting above the casing, so that the cushioning means may be readily brought into cooperative 4relationship therewith.
  • the switch I2 is mounted within a iluidetight compartment -20 deiined in part by a generally
  • the switch is secured as a- U-shapedV mounting bracket 24, thetransverse 4portion of which. is secured to thebottom -of the housing.22 so that the switch may be secured between the r ⁇ upstanding arms of the bracket.
  • the circuit connections up to the switch extend through a suitable plug type tting 25 secured in fluid-tight manner tothe housing 22 and having apair of terminals 28 located within the compartment 20. 'The terminals areconn'ected as by c0nrkductors Bil to the switch.
  • the source of ⁇ air pressure is connected to the compartment y20 through a condui ⁇ t ⁇ 32 and a'ttingfd attached to the bottom oi the housing 22.
  • the conduit S2 may lead to the propeller blast from an airplane propeller. It should be understood however that the device may be used in other installations and lor other purposes.
  • the hydraulic cushioning means I4 is located above the switch l2, as is readily apparent from Fig. l.
  • the cushioning action is provided by a hydraulic fluid, indicated by reference character 36, which is located within a structure bearing against the switch actuating linger I 8 and moved in response to the pressures existing within compartment 2G.
  • the movement of the cushioning fluid is constrained or restricted by a relatively small tone 38 located between the two main parts of the cushioning means, which, for convenience, are termed a variable volume chamber 40 and a reservoir chamber 42.
  • the Variable volume chamber 4D comprises a diaphragm 44 made of some flexible material such as rubber. It is preferred that the diaphragm be substantially untensioned in order that it will not exert any influence upon the operation of the switch.
  • the diaphragm is circular in shape and is secured over the open top of the cup-shaped housing 22 to define with the latter the fluid compartment 20. Itis secured to the anged top of the housing in a suitable manner as by a plurality of screws 45 which serve also to secure to the housing a generally conical top 45.
  • a switch operating button or stud 48 is secured substantially centrally of the diaphragm so that it is located above yand in cooperative relationship with the switch operating finger I8.
  • the pressure setting at which the switch will operate may be readily varied, in accordance with another fea-ture of the invention, by varying the weight of the diaphragm assembly. This is conveniently done by utilizing different numbers of metallic plates preferably located at opposite sides of the diaphragm and secured to it by the switch operating button 48. In the instant embodiment one plate 53 is disposed underneath and two plates 52 and 54 are disposed above the diaphragm. Not only may diiierent numbers of plates be used but also-dii Schlt sizes may be used.
  • the plates may be of different diameters but preferably are somewhat less in diameter than the effective diameter of the diaphragm M so as to enable the diaphragm readily to move in response to pressure of the character for which the device is intended to be used.
  • the variable volume change 40 is constituted by the diaphragm and the previously referred to generally conical top 45.
  • the latter is provided with a central opening deiined by an upwardly extending flange 50 adapted to receive a short tube 58 defining the previously referred to liuid iiow restricting oriiice ⁇ 38.
  • the top is quite closely spaced to the diaphragm assembly and limits movement of the latter so that it will not be injured when subjected to higher pressures.
  • the iluid reservoir 42 is constituted by a generally cup-shaped receptacle having an inclined bottom 69 and having its upper end closed by a, closure plate 62 suitably secured to the flanged top of the receptacle.
  • a vent tube 64 extending Cil into the upper part of the reservoir is mounted substantially centrally of the closure plate 52.
  • an annular bracing structure located between the top 44 and the bottom 60 of the reservoir.
  • This structure includes a short piece of tubing 66 and a pair of annular flanges 68 and 'I0 securing the tube to the top M and bottom 60, respectively.
  • the hydraulic cushioning means I4 is constructed and arranged to be effective throughout a wide range of angular positions of the device. This is or importance in connection wih certain installations such as aircraft.
  • This desirable attribute of the device is obtained by making the dual chamber construction generally hour-glass shaped and by making the variable volume chamber relatively large in diameter but short in length, and having the flow-restricting oriiice located substantially centrally of the chamber.
  • flow of the cushioning fluid from the reservoir is prevented from escaping by extending the venting tube 64 a substantial distance within the reservoir and locating it centrally thereof. The amount of fluid should be limited so as not to rise above the inner end of the venting tube even if the device should be in an inverted position.
  • the switch of the present invention may be constructed readily and economically. It is also extremely sensitive to variations in the control pressure but will not operate in response to vibrations.
  • the compartment 20 is connected to the source of control pressure through the conduit 32, which may be the propeller blast of an airplane.
  • the switch I2 may be either of the normally closed or normally open type. In this description it is assumed to be of the normally open type. The diaphragm and amount of iiuid are so arranged that the switch remains in its open position until the pressure in chamber 20 rises to some predetermined value.
  • This value may be as low as one and one-half or two inches of water.
  • the switch itself may be of a character to operate with pressure differential of one-half inch. For example, if the switch closes at a pressure of two inches of water, at which time the diaphragm 44 moves upwardly to relieve the pressure on the switch operating finger I8 and then if the pressure decreases to one and one-half inches of water, the switch would be opened by the downward movement oi' the diaphragm and linger I 8.
  • the switch of the present invention is also effete over a wide range of angular positions.
  • lt is normally mounted vertically, i. e., in the position in which it is shown in Fig. l.
  • the fluid in the reservoir moves, but the liuid in the variable volume chamber 4 does not move, at least until the angular position has been considerably shifted.
  • some of the fluid in the chamber may drain to the liquid reservoir without affecting the operation of the device.
  • the variation in angular position does not pose much of a problem because the variations in angular position are not likely to occur until the airplane is in flight.
  • the air pressure eX- isting in chamber 20 may be above six or seven inches of water and as high as fifteen inches of water pressure so that there is then no danger of undesired operation of the switch.
  • the drainage of fluid from the variable volume chamber to the reservoir at this time would not affect the operation of the switch because such drainage would merely mea-n that the diaphragm may re lieve further the pressure applied to the operating finger. Movement of the diaphragm beyond a predetermined safe point is prevented by the top 44 which is located relatively close to the diaphragm.
  • a pressure actuated switch of the type including movable switch operating means, including in combination, a fluid-tight compartment for said switch, a diaphragm closing said compartment located in cooperative relation to and adapted to move said operating means, and means for opposing movement of the diaphragm, said last mentioned means including a variable volume chamber comprising said diaphragm, and a generally conical top spaced a short distance from the diaphragm to limit movement of the latter, a reservoir defining chamber, a flow-restricting suddenly located centrally of and interconnecting said chambers, and a Vent-defining tube located centrally of and extending into said reservoir.
  • a pressure actuated switch including in combination, a huid-tight compartment, a switch having a switch actuating element mounted in said compartment with the actuating element located near the upper end of the compartment, a flexible diaphragm closing the upper end of the compartment, means mounted upon said diaphragm adapted to engage said switch actuating element, means forming a variable volume chamber located at the upper side of the diaphragm and constituted in part by the diaphragm, a fluid reservoir located above said chamber and open to atmospheric pressure, and means including a flow-restricting orifice interconnecting the chamber and reservoir.
  • a lpressure actuated switch including in combination, a fluid-tight compartment, a switch having a switch actuating element mounted in said compartment with the actuating element located near the upper end of the compartment, a flexible diaphragm closing the upper end of the compartment, means mounted upon said diaphragm adapted to engage said switch actuating element, means forming a variable Volume chamber located at the upper side of the diaphragm and constituted in part by the diaphragm, a uid reservoir located above said chamber and open to atmospheric pressure, means including a flow-restricting tone interconnecting the chamber and reservoir, and a Weight attached to said diaphragm for resisting vibration thereof and determining the pressure at which the switch operates.

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Switches Operated By Changes In Physical Conditions (AREA)

Description

April 29, 1947. J. H. LESLIE, 2D 2,419,685
ELECTRIC SWITCH Filed Dec. 14, '1944 Aone and oneehalf or twoinches of water. Lthese pressures the rvibration produces unde- Patented Apr. 29, 1947 'John H. Leslie, 4vII, Winnetka,V lll., assigner y-to `Stewart-Warner Corporation, Chicago, Ill., a r.corporation of Virginia Application December 14, 1944, 'SerialNm 568,173
4 Claims. V1
The present Vinvention relates to pressure actuated switches'andparticularly to verysensiltive pressure actuated `snap switches.
There are many known `types yof sensitive switches. Mostgenerally they are of a typewhich `may be described as `over-center snap switches andsorne are operable at low pressures and in response to small pressure differences.
Difficulties have been encountered in the :use of the sensitive switches when they arefinstalled in equipment such,for instance, as airplanes where considerable vibration is present. When :the
switches'arefsubjected to a critical pressure, i. e., ythe approximate voperating-pressure, the vibrations :producean undesirable intermittent operation. This operation is sometimes called flutter- -ing and it has an objectionable eiect not only yupon ythe yswitches but `it'also defeats the purpose of the `control because the controlled apparatus is intermittently `operated as a result `of the intermittent 'operation of thesswitch.
j For exam-ple, sensitive switchesare `utilized to control heaters in aircraft. The switchesv are in- .tended to prevent operation of the heater unless a certain lair pressurer exists to create a minimum ."ilowof air through the heating apparatus. 'The switches may be setto turn theheater `on vwhen `the air pressurawhichmayybe the air blast (propeller blast) from thepropeller, hasy a pressure of At sirable fluttering, or intermittent operation 'of the switches.
The primary object of the present invention `is to provide a new and improved sensitive pressure actuated switch.
Another object of the present invention is to provide a new and improved sensitive pressure l,actuated electrical switch which maybe actuated at very low pressures and which is prevented from operating intermittently in response .to vibrations.
cushioned'r electrical switch wherein the hydraulic vcushioning means is effective throughoutawide Arange voi-angular positions of the switch. A "switch of this character is particularly vadvantageous for use in certain types of apparatus, of which aircraft is an outstanding example.
. cup-shaped' housing 22.
inside the housing-by any convenient means such Afstill further object of the present invention 4is `to provide a new and improved sensitive pres- Ysure actuated `switch which maybe readily constructed and arranged to'operate at desired pressures.
ther objects and advantages of the present invention' will' become apparent from the ensuing description in the courseof which reference is had to the accompanying drawing, in which- Fig. yl isa vertical cross sectional View through the switch of the present invention; and
Fig. 2 'is a transverse lcross sectional view taken :along the line2-2 of Fig. l.
The switch of thepresent invention, which is indicated as a Ywhole by reference character I0, includesV two mainrparts. The firsty is a circuit controlling switch I2 and the second a hydraulic cushioningy meansr i4 located in cooperative relationship with theswitch actuating means and eiective to prevent operation of the switch in response to vibrations over a wide range of yangular positions lof the device.
The `switchIZvv may be a snap switch of conventional construction except that 'it should be designed to operate at'about-one and one-half or two inches of water pressure, and with a presrurerdifferential oiabout one-half inch. VIn other words, theswitch should be a sensitive one. The circuit controlling contacts of the switch are not illustrated but they may be mounted within a suitable switch casing AI6 Yand are operable through suitable switchoperating means, such as a. finger I3 projecting above the casing, so that the cushioning means may be readily brought into cooperative 4relationship therewith.
The switch I2 is mounted within a iluidetight compartment -20 deiined in part by a generally The switch is secured as a- U-shapedV mounting bracket 24, thetransverse 4portion of which. is secured to thebottom -of the housing.22 so that the switch may be secured between the r`upstanding arms of the bracket.
The circuit connections up to the switch extend through a suitable plug type tting 25 secured in fluid-tight manner tothe housing 22 and having apair of terminals 28 located within the compartment 20. 'The terminals areconn'ected as by c0nrkductors Bil to the switch.
sures and specifically to air pressure. The source of` air pressure is connected to the compartment y20 through a condui`t`32 and a'ttingfd attached to the bottom oi the housing 22. As already indicated, the conduit S2 may lead to the propeller blast from an airplane propeller. It should be understood however that the device may be used in other installations and lor other purposes.
The hydraulic cushioning means I4 is located above the switch l2, as is readily apparent from Fig. l. The cushioning action is provided by a hydraulic fluid, indicated by reference character 36, which is located within a structure bearing against the switch actuating linger I 8 and moved in response to the pressures existing within compartment 2G. The movement of the cushioning fluid is constrained or restricted by a relatively small orice 38 located between the two main parts of the cushioning means, which, for convenience, are termed a variable volume chamber 40 and a reservoir chamber 42.
The Variable volume chamber 4D comprises a diaphragm 44 made of some flexible material such as rubber. It is preferred that the diaphragm be substantially untensioned in order that it will not exert any influence upon the operation of the switch. The diaphragm is circular in shape and is secured over the open top of the cup-shaped housing 22 to define with the latter the fluid compartment 20. Itis secured to the anged top of the housing in a suitable manner as by a plurality of screws 45 which serve also to secure to the housing a generally conical top 45.
The movements of the diaphragm are utilized to operate the switch I2. For this purpose a switch operating button or stud 48 is secured substantially centrally of the diaphragm so that it is located above yand in cooperative relationship with the switch operating finger I8.
The pressure setting at which the switch will operate may be readily varied, in accordance with another fea-ture of the invention, by varying the weight of the diaphragm assembly. This is conveniently done by utilizing different numbers of metallic plates preferably located at opposite sides of the diaphragm and secured to it by the switch operating button 48. In the instant embodiment one plate 53 is disposed underneath and two plates 52 and 54 are disposed above the diaphragm. Not only may diiierent numbers of plates be used but also-diiierent sizes may be used. The plates may be of different diameters but preferably are somewhat less in diameter than the effective diameter of the diaphragm M so as to enable the diaphragm readily to move in response to pressure of the character for which the device is intended to be used.
The variable volume change 40 is constituted by the diaphragm and the previously referred to generally conical top 45. The latter is provided with a central opening deiined by an upwardly extending flange 50 adapted to receive a short tube 58 defining the previously referred to liuid iiow restricting oriiice `38. The top is quite closely spaced to the diaphragm assembly and limits movement of the latter so that it will not be injured when subjected to higher pressures.
The iluid reservoir 42 is constituted by a generally cup-shaped receptacle having an inclined bottom 69 and having its upper end closed by a, closure plate 62 suitably secured to the flanged top of the receptacle. In order that the movement of the fluid within the reservoir, in response to variations in volume of the chamber 40, will not be impeded, a vent tube 64 extending Cil into the upper part of the reservoir is mounted substantially centrally of the closure plate 52.
Added rigidity is given the cushioning means I4 by an annular bracing structure located between the top 44 and the bottom 60 of the reservoir. This structure includes a short piece of tubing 66 and a pair of annular flanges 68 and 'I0 securing the tube to the top M and bottom 60, respectively.
It should be noted, in accordance with one of the features of the present invention, that the hydraulic cushioning means I4 is constructed and arranged to be effective throughout a wide range of angular positions of the device. This is or importance in connection wih certain installations such as aircraft. This desirable attribute of the device is obtained by making the dual chamber construction generally hour-glass shaped and by making the variable volume chamber relatively large in diameter but short in length, and having the flow-restricting oriiice located substantially centrally of the chamber. Furthermore, flow of the cushioning fluid from the reservoir is prevented from escaping by extending the venting tube 64 a substantial distance within the reservoir and locating it centrally thereof. The amount of fluid should be limited so as not to rise above the inner end of the venting tube even if the device should be in an inverted position.
The switch of the present invention may be constructed readily and economically. It is also extremely sensitive to variations in the control pressure but will not operate in response to vibrations. In operation, the compartment 20 is connected to the source of control pressure through the conduit 32, which may be the propeller blast of an airplane. The switch I2 may be either of the normally closed or normally open type. In this description it is assumed to be of the normally open type. The diaphragm and amount of iiuid are so arranged that the switch remains in its open position until the pressure in chamber 20 rises to some predetermined value.
This value may be as low as one and one-half or two inches of water. Furthermore, the switch itself may be of a character to operate with pressure differential of one-half inch. For example, if the switch closes at a pressure of two inches of water, at which time the diaphragm 44 moves upwardly to relieve the pressure on the switch operating finger I8 and then if the pressure decreases to one and one-half inches of water, the switch would be opened by the downward movement oi' the diaphragm and linger I 8.
Operation of the switch in response to vibrations occurring even at critical operating pressures is prevented by the hydraulic fluid 3B, the movement of which is restricted by the oriiice 38. The vibrations tending to operate the switch tend also to move the diaphragm 44, but such movement is prevented by the fluid 35 which cannot move rapidly because of the restriction offered by the orifice. Consequently the switch of the present invention is not only sensitive but is free of fluttering in response to vibrations.
The switch of the present invention is also efective over a wide range of angular positions. lt is normally mounted vertically, i. e., in the position in which it is shown in Fig. l. Should the angular position of the device change, the fluid in the reservoir moves, but the liuid in the variable volume chamber 4 does not move, at least until the angular position has been considerably shifted. Furthermore, some of the fluid in the chamber may drain to the liquid reservoir without affecting the operation of the device.
In the instant embodiment of the invention, wherein the diaphragm is moved away from the switch operating finger at higher pressures the variation in angular position does not pose much of a problem because the variations in angular position are not likely to occur until the airplane is in flight. When in Hight the air pressure eX- isting in chamber 20 may be above six or seven inches of water and as high as fifteen inches of water pressure so that there is then no danger of undesired operation of the switch. The drainage of fluid from the variable volume chamber to the reservoir at this time would not affect the operation of the switch because such drainage would merely mea-n that the diaphragm may re lieve further the pressure applied to the operating finger. Movement of the diaphragm beyond a predetermined safe point is prevented by the top 44 which is located relatively close to the diaphragm.
The foregoing detailed description of the present invention is intended to be illustrative and not limitative of the invention, except insofar as particularly set forth in the accompanying claims.
Having thus described my invention, what I claim as new and desire to secure by United States Letters Patent is:
1. A pressure actuated switch of the type including movable switch operating means, including in combination, a fluid-tight compartment for said switch, a diaphragm closing said compartment located in cooperative relation to and adapted to move said operating means, and means for opposing movement of the diaphragm, said last mentioned means including a variable volume chamber comprising said diaphragm, and a generally conical top spaced a short distance from the diaphragm to limit movement of the latter, a reservoir defining chamber, a flow-restricting orice located centrally of and interconnecting said chambers, and a Vent-defining tube located centrally of and extending into said reservoir.
2. A switch as claimed in claim 1, wherein the chamber and orifice have a generally hour-glass shape and means including annular bracing structure engaging both chambers and surrounding the orice are provided to give added strength.
3. A pressure actuated switch, including in combination, a huid-tight compartment, a switch having a switch actuating element mounted in said compartment with the actuating element located near the upper end of the compartment, a flexible diaphragm closing the upper end of the compartment, means mounted upon said diaphragm adapted to engage said switch actuating element, means forming a variable volume chamber located at the upper side of the diaphragm and constituted in part by the diaphragm, a fluid reservoir located above said chamber and open to atmospheric pressure, and means including a flow-restricting orifice interconnecting the chamber and reservoir.
4. A lpressure actuated switch, including in combination, a fluid-tight compartment, a switch having a switch actuating element mounted in said compartment with the actuating element located near the upper end of the compartment, a flexible diaphragm closing the upper end of the compartment, means mounted upon said diaphragm adapted to engage said switch actuating element, means forming a variable Volume chamber located at the upper side of the diaphragm and constituted in part by the diaphragm, a uid reservoir located above said chamber and open to atmospheric pressure, means including a flow-restricting orice interconnecting the chamber and reservoir, and a Weight attached to said diaphragm for resisting vibration thereof and determining the pressure at which the switch operates.
JOHN H. LESLIE', II.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,033,417 Dezotell Mar. 10,1936 2,112,059 Arthur Mar. 22, 1938 2,182,450 Clarkson Dec. 5, 1939
US568173A 1944-12-14 1944-12-14 Electric switch Expired - Lifetime US2419685A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2794088A (en) * 1953-06-16 1957-05-28 Burton K Ostby Automatic switch
US2867706A (en) * 1954-05-17 1959-01-06 Statham Instrument Inc Pressure sensitive resistor
US3260816A (en) * 1963-09-25 1966-07-12 Murdock Associates Inc Pressure switch
US3553401A (en) * 1967-08-10 1971-01-05 Philips Corp Salt-supply container and switch for a softening device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2033417A (en) * 1934-08-07 1936-03-10 United Electric Controls Co Pressure controlled switch
US2112059A (en) * 1933-08-28 1938-03-22 Gen Motors Corp Control apparatus for engine starters
US2182450A (en) * 1938-11-28 1939-12-05 Clarkson Alick Fluid pressure controlled switch

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2112059A (en) * 1933-08-28 1938-03-22 Gen Motors Corp Control apparatus for engine starters
US2033417A (en) * 1934-08-07 1936-03-10 United Electric Controls Co Pressure controlled switch
US2182450A (en) * 1938-11-28 1939-12-05 Clarkson Alick Fluid pressure controlled switch

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2794088A (en) * 1953-06-16 1957-05-28 Burton K Ostby Automatic switch
US2867706A (en) * 1954-05-17 1959-01-06 Statham Instrument Inc Pressure sensitive resistor
US3260816A (en) * 1963-09-25 1966-07-12 Murdock Associates Inc Pressure switch
US3553401A (en) * 1967-08-10 1971-01-05 Philips Corp Salt-supply container and switch for a softening device

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