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US2311900A - Barometer - Google Patents

Barometer
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Publication number
US2311900A
US2311900AUS443693AUS44369342AUS2311900AUS 2311900 AUS2311900 AUS 2311900AUS 443693 AUS443693 AUS 443693AUS 44369342 AUS44369342 AUS 44369342AUS 2311900 AUS2311900 AUS 2311900A
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United States
Prior art keywords
bellows
post
barometer
bar
support
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Expired - Lifetime
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US443693A
Inventor
Arthur T Newell
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Kenyon Instrument Co Inc
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Kenyon Instrument Co Inc
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Publication date
Application filed by Kenyon Instrument Co IncfiledCriticalKenyon Instrument Co Inc
Priority to US443693ApriorityCriticalpatent/US2311900A/en
Application grantedgrantedCritical
Publication of US2311900ApublicationCriticalpatent/US2311900A/en
Anticipated expirationlegal-statusCritical
Expired - Lifetimelegal-statusCriticalCurrent

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Description

Feb. 23, 1943. A, NEWELL 2,311,900
BAROMETER Filed May 20, 1942 INVENTOR. Eff/flit! Z Nerve/Z Fl TTORNE Y Patented Feb. 23, 1943 2,311,900 I BAROMETER Arthur T. Newell,
Kenyon Instrument 00., Inc.,
N. Y., a corporation 01' tion,
Huntington, N. Y., assign'or to Huntington Sta- New York Application May 20, 1942, Serial No. 443,693
7 Claims.
This invention relates to barometers and has for an object to provide a sensitive, temperature corrected barometer having novel and improved details of construction and features of operation.
Various other objects and advantages will be apparent as the nature of the'invention is more fully disclosed.
Although the novel features which are believed to be characteristic of this invention are pointed out more particularly in the claims appended hereto, the invention itself may be better understood by referring to the following description, taken in connection with the accompanying drawing in which a specific embodiment thereof has been set forth for purposes of illustration.
In the drawing,
Fig. l is a top plan view of a barometer embodying the present invention;
Fig. 2 is a vertical longitudinal section thereof taken on the line 2-2 of Fig. 1;
Fig. 3 is a rear elevation of the barometer; and Fig. 4 is a detail view of the post support.
In the following description and in the claims.
certain specific terms have been used for convenience in referring to various details of the invention. These terms, however, are to be given as broad an interpretation as the state of the art will permit.
Referring to the drawing more in detail, the barometer is shown as comprising a frame formed by a front plate I0, bar l2. The front plate l may constitute a dial or may comprise a part of an instrument panel. The cross-bar I2 is rigidly attached to one of the side posts H as by a screw l3 and is adjustably attached to the other side post II by ascrew 14. A compression spring I5 is seated around the screw l4 between the end of the post II and the cross-bar l2 and serves to maintain the cross-bar tight against the head of thescrew 14.
A collapsible bellows is shown as mounted on ahead 2| and as having adiaphragm 22 to which it is joined to form an air-tight closure. Thehead 2| is attached to the front plate In by suitable means, shown as ascrew 23 and is positioned as desired by aspacer 24. A port 25 is provided for evacuating the chamber within thebellows 20. This port is shown as sealed by a sealing member 26.
In order to compensate for temperature variations, a pair of springs and 3| are mounted concentrically within thebellows 20 between thediaphragm 22 and thehead 2|. Thesesprings 30 and 3| preferably have difierent temperature side posts I I, and a rear crossmoduli. Preferably, one spring is made of ametal having a positive temperature modulus and the other spring is made of'a metal having a negative temperature modulus and are so designed that the combined moduli of the two springs and of thebellows 20 itself becomes zero, so that the barometer reading remains constant at any particular barometric pressure regardless of variations in temperature. It is to be understood that thesprings 30 and 3| may be made of suitable metals or bimetals having the desired temperature moduli. A single corrective spring may be used in certain instances to compensate for the temperature effect of the bellows and'of the other parts, although correction is usually facilitated by suitable selection of two springs having different characteristics.
The barometer is provided with anindicathig pointer 35 which is mounted on the front of the front plate ill on ashaft 36, which extends through said front plate and carries adrum 31 to which anoperating cord 38 is attached. Aspring 39 is connected between theshaft 36 and 41 which is slidably adjustable on apost 48. Aset screw 49 is shown as provided for securing the lug 41 in adjusted position.
Thepost 48 is attached to asupport 52, the ends of which are secured to the cross-bar l2 by means of a pair ofspring members 53. Thespring members 53 are made of such flexibility that practically frictionless pivotal movement of thesupport 52 takes place. Thediaphragm 22 of thebellows 20 is connected to thesupport 52 by means of a spring finger engaging ascrew 62 which is mounted in said support and is so arranged that horizontal movement of thediaphragm 22 causes pivotal movement of said support, thereby causingpost 48 to rock forwardly and rearwardly. Acounterweight 64 is adjustably mounted on thepost 48 and may be adjusted to provide substantially frictionless and inertialess operation of the barometer.
In the operation of this device, with thebellows 20 evacuated, thediaphragm 22 moves in response to changes in atmospheric pressure. These movements are transmitted through linkages above described to thecord 38 and thence to thepointer 35. By means of the compound spring arrangement, the barometer may be made of extreme sensitivity and the counterweight the lug 41 may be adjusted to their optimum position for securing practically inertialess operation of the device. The position of the lug 41 also controls the amount of movement of thepointer 35. The sensitiveness of response of thepointer 35 may thus be controlled as desired.
The above described barometer is primarily intended for use on airplanes, in which event, the device may be calibrated as an altimeter. Inasmuch as planes at high altitudes are subjected to extremely low temperatures, it is important to provide a barometer in which variations due to temperature changes are eliminated. The present invention accomplishes this in an eiflcient and dependable manner and provides a barometer which is suited to commercial production for the purpose above specified.
Although a specific embodiment of the invention has been shown for purposes of illustration, it is to be understood that various changes and modifications may be made therein as will be readily apparent to a person skilled in the art.
What is claimed is:
l. A temperature compensated barometer comprising an expansible bellows having a predetermined temperature modulus, spring means located within said bellows having a temperature modulus suited to compensate for the temperature modulus of said bellows to produce a zero over-all temperature response, and mechanism connected to be actuated by the expansionand contraction of said bellows.
2. A temperature compensated barometer comprising a closed, evacuated bellows, spring means within said bellows made of a material diiierent from that of said bellows and selected to compensate for temperature variations thereof to produce a zero over-all temperature response, and mechanism connected to be actuated by the expansion and contraction of said bellows.
3. A barometer comprising an expansible bellows, a frame carrying said bellows and having a front plate to which one end of said bellows is secured and a rear bar extending across the movable end of said bellows but spaced therefrom, a post extending upwardly with respect to said rear bar, means attaching said post to said bar for rocking movement comprising a post support and a spring member extending from said support to said bar, said spring member having suflicient flexibility to provide practically frictionless rocking movement of said post, a member connecting the movable end of said bellows to said support to cause rocking movement thereof in response to movement of said bellows and mechanism actuated by rocking movement of said post.
4. A barometer comprising an expansible bellows, a frame carrying said bellows and having a front plate to which one end of said bellows is secured and a rear bar extending across the movable end of said bellows but spaced therefrom, a post extending upwardly with respect to said rear bar, means attaching said post to said bar for rocking movement comprising a post support and a spring member extending from said support to said bar, said spring member having suflicient flexibility to provide practically frictionless rocking movement of said post, a member connecting the movable end of said bellows to said support to cause rocking movement thereof in response to movement of said bellows, a
counterweight adjustably supported by said post to adjust the inertia of operation thereof. and mechanism actuated by rocking movement of said post.
5. A barometer comprising an expansible bellows, a frame carrying said bellows and having a front plate to which one end of said bellows is secured and a rear bar extending across the movable end of said bellows but spaced therefrom, a post extending upwardly with respect to aid rear bar, means attaching said post to said bar for rocking movement comprising a post support and a spring member extending from said support to said bar, said spring member having sufflcient flexibility to provide practically frictionless rocking movement of said post, a member connecting the movable end of said bellows to said support to cause rocking movement thereof in response to movement of said bellows, a pointer mounted for rotation, a flexible member actuating aid pointer, means attaching said flexible member to said post to be actuated by rocking movement thereof, and means adjusting the point of attachment of said flexible member along said post to vary the sensitivity of said barometer.
6. A barometer comprising an expansible bellows, a coiled spring within said bellows having a temperature modulus different from that of said bellows and selected to compensate therefor to produce a zero over-all temperature response, a frame carrying said bellows and having a front plate to which one end of said bellows is secured and a rear bar extending across the movable end of said bellows but spaced therefrom, a post extending upwardly with respect to said rear bar, means attaching said post to said bar for rocking movement comprising a post support and a spring member extending from said support to said bar, said spring member having suflicient flexibility to provide practically frictionles rocking movement of said post, a member connecting the movable end of said bellows to said support to cause rocking movement thereof in response to movement of said bellows and mechanism actuated by rocking movement of said post.
7. A barometer comprising an expansible bellows, a coiled spring within said bellows having a temperature modulus different from that of said bellows and selected to compensate therefor to produce a zero over-all temperature response,
a frame carrying said bellows and having a front plate to which one end of said bellows is secured and a. rear bar extending across the movable end of said bellows but spaced therefrom, a post extending upwardly with respect to said rear bar, means attaching said post to said bar for rocking movement comprising a post support and a spring member extending from said support to said bar, said spring member having suflicient flexibility to provide practically frictionless rocking movement of said post, a member connecting the movable end of said bellows to said support to cause rocking movement thereof in response to movement of said bellows, a pointer mounted for rotation, a flexible member actuating said pointer, means attaching said flexible member to said post to be actuated by rocking movement thereof, and means adjusting the point of attachment of said flexible member along said post to vary the sensitivity of said barometer.
ARTHUR T. NEWELL.
US443693A1942-05-201942-05-20BarometerExpired - LifetimeUS2311900A (en)

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US443693AUS2311900A (en)1942-05-201942-05-20Barometer

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US443693AUS2311900A (en)1942-05-201942-05-20Barometer

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2468906A (en)*1945-01-041949-05-03Celanese CorpPrecision measuring instrument having a thread for a motion transmission link
US2507326A (en)*1945-10-041950-05-09Norden Lab CorpPressure responsive speed controller
US2603973A (en)*1947-03-151952-07-22Wallace & Tiernan IncFlexible chamber pressure gauge
US2664917A (en)*1947-04-261954-01-05Bristol CompanyApparatus for measuring absolute pressure
US2698633A (en)*1952-05-091955-01-04American Machine & MetalsEvacuated capsule for aneroid barometers
US2759361A (en)*1952-10-271956-08-21Bendix Aviat CorpDynamically balanced gauge
US2772569A (en)*1951-07-301956-12-04Baldwin Lima Hamilton CorpFluid pressure measuring device
US2890588A (en)*1954-09-081959-06-16Genisco IncFluid pressure detector
US3805618A (en)*1972-08-111974-04-23Springfield Instr Co IncPressure-responsive instrument
US3874242A (en)*1972-08-111975-04-01Springfield Instr Company IncPressure-responsive instrument

Cited By (10)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2468906A (en)*1945-01-041949-05-03Celanese CorpPrecision measuring instrument having a thread for a motion transmission link
US2507326A (en)*1945-10-041950-05-09Norden Lab CorpPressure responsive speed controller
US2603973A (en)*1947-03-151952-07-22Wallace & Tiernan IncFlexible chamber pressure gauge
US2664917A (en)*1947-04-261954-01-05Bristol CompanyApparatus for measuring absolute pressure
US2772569A (en)*1951-07-301956-12-04Baldwin Lima Hamilton CorpFluid pressure measuring device
US2698633A (en)*1952-05-091955-01-04American Machine & MetalsEvacuated capsule for aneroid barometers
US2759361A (en)*1952-10-271956-08-21Bendix Aviat CorpDynamically balanced gauge
US2890588A (en)*1954-09-081959-06-16Genisco IncFluid pressure detector
US3805618A (en)*1972-08-111974-04-23Springfield Instr Co IncPressure-responsive instrument
US3874242A (en)*1972-08-111975-04-01Springfield Instr Company IncPressure-responsive instrument

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