US2652859A - High altitude pressure responsive capsule - Google Patents

High altitude pressure responsive capsule Download PDF

Info

Publication number
US2652859A
US2652859A US27755A US2775548A US2652859A US 2652859 A US2652859 A US 2652859A US 27755 A US27755 A US 27755A US 2775548 A US2775548 A US 2775548A US 2652859 A US2652859 A US 2652859A
Authority
US
United States
Prior art keywords
pressure
partition
pressure responsive
bellows
pressures
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US27755A
Inventor
Murphy Donald Francis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bendix Aviation Corp filed Critical Bendix Aviation Corp
Priority to US27755A priority Critical patent/US2652859A/en
Application granted granted Critical
Publication of US2652859A publication Critical patent/US2652859A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L7/00Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements

Definitions

  • This invention relates to devices for converting pressure variations into mechanical displacements and more particularly to a device of this nature having arelatively large deflection-pressure modulus in the presence of low pressures and a relatively small deflection-pressure modulus in the presence of pressures exceeding a predeter mined. level.
  • the mechanical pressure sensing unit be characterized by a large displacement for a small pressure change.
  • the satisfaction of this requirement with a unit having a constant deflection-pressure modulus results in an assembly having an excessive travel which may be diflicult to accommodate in an indicating unitintended to provide accurate indications'in a limited low pressure range.
  • stops disengaging the lever arm or other transmission link from the pressure driving unit whenever its deflections fell without a predetermined range. Such stops, however, being separate from the pressure responsive driving unit and usually associated witha lever system burdened by variable and unpredictable amounts of play, have not proven entirely satisfactory.
  • the capsule assembly includes a base disk I I having an apertured boss I] located centrally thereof.
  • the bellows side of the base disk II is also provided with a central elevated land 20 which is circular in form.
  • the mounting disk II is apertured at the point I0, radially displaced outwardly of the land 20, to receive an exhaust'tubulation I8. If the mounting disk I I is of brass or some other material to which solder adheres readily, the exhaust tubulation I8 may be hermetically sweated in place.
  • An inner Sylphon bellows I6 of substantially cylindrical form has its open end sweated to the mounting disk II along the periphery of the circular land 20.
  • the inner bellows I6 may be formed of a single sheet of material and have a closed end which is a continuation of that matecritical elements at spaced points in the instrument structure, rendering it sensitive to mechanical distortions arising from thermal changes and rough handling.
  • Still another object of the invention is to provide a new and novel pressurecapsule assemblyin which the threshold of pressure indication may be conveniently adjusted.
  • the driving disk I2 is similarly provided with an apertured boss whose aperture does not, however, extend through the driving member I2. This aperture may be tapped to receive a suitably threaded screw for easy connection with a driving link conveying the capsule motion to an indicator assembly.
  • the inner Sylphon bellows I6, mounting disk II, outer Sylphon bellows I5, and the driving disk I2 define a sealed chamber venting to the exhaust tubulation I8. Thishermetically enclosed volume may be exhausted to any desired pressure by connecting the tubulation I8 with an evacuating system and sealing ofi the tubulation when the desired residual pressure within the sealed volume has been secured.
  • the outer bellows I5 is relatively soft and is characterized by a large deflection-pressure modulus
  • the flexible outer bellows i5 is driven toward the mounting disk H to firmly engage the driving disk l2 with the limiting table formed by the inner bellows I6.
  • the force maintaining these two members in engagement decreases correspondingly until the pressure force equals the distortion-induced restoring force built up within the outer bellows l5.
  • A-continuing reduction in pressure permits the bellows spring force to move the driving disk I2 outwardly away from the limiting table formed by inner bellows I 6.
  • the displacement characteristic of the composite pressure capsule assembly is graphically illustrated in Figure 2 in which increasing pressures are indicated by increasing displacements to the right on the abscissa and increasing displacements are indicated by increasing distances along the ordinate axis.
  • the pressure exceeds the critical value at 22, the driving disk and limiting table or abutment are in engagement and there is no travel of the driving disk as is at once evident from an inspection of the figure.
  • a decrease in the pressure below the value corresponding to point 22 permits the bellows spring force to overcome the pressure-induced force with consequent increase in displacement along the line 23 until a travel corresponding to the point 2
  • the composite assembly just described is a compact pressure responsive driving unit satisfying the requirements developed earlier in this specification. It may be beneficially employed wherever a high deflection rate over a limited range of low pressures is required without the possibility of imparting excessive motions to sensitive lever systems in the presence of very high pressures.
  • a pressure responsive device having a substantially large deflection-pressure modulus in the presence of pressures not exceeding a predetermined pressure level and having means to prevent defiection in the presence of pressures greater than said predetermined level, comprising, in combination, a first flexible sealing partition having a substantially cylindrical form with one closed and one open end, a second flexible sealing partition having a smaller substantially cylindrical form with one closed and one open end situated within said first partition with its closed end adjacent the closed end of said first partition, a base member hermetically engaging said open ends and having an aperture within the region bounded by said second partition, and a member passing through said aperture adapted to maintain the closed end of said second partition at a desired distance from said base member, the volume between said partitions being evacuated to a residual pressure of very nearly zero absolute pressure.
  • a pressure responsive device having a substantially large deflection-pressure modulus in the presence of pressures not exceeding a. predetermined pressure level and having means to prevent deflection in the presence of pressures greater than said predetermined level, comprising, in combination, a first flexible sealing partition having a substantially cylindrical form with one closed and one open end, a second flexible sealing partition having a smaller substantially cylindrical form with one closed and one open end coaxially situated within said first partition with said closed ends adjacent, a base member hermetically engaging said open ends and having a threaded aperture coaxially situated with respect to said cylindrical partitions and a correspondingly threaded member extending through said aperture to a point adjacent the closed end of said second partition, the volume between said partitions being evacuated to a residual pressure of very nearly zero absolute pressure.
  • a pressure responsive device having a substantially large deflection-pressure modulus in the presence of pressures not exceeding a predetermined pressure level and having means to prevent deflection in the presence of pressures greater than said predetermined level, comprising, in combination, a first flexible sealing partition having a substantially cylindrical form, a disk sealingly engaging one end of said first partition, a second flexible sealing partition having a small er substantially cylindrical form with one closed and one open end coaxially situated within said first partition with said closed end adjacent said sealing disk, 2.
  • DONALD FRANCIS MU RPHY DONALD FRANCIS MU RPHY.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Fluid Pressure (AREA)

Description

Sept. 22, 1953 D. F. MURPHY 2,652,859
HIGH ALTITUDE PRESSURE RESPONSIVE CAPSULE Filed May 18, 1948 I RY 10 )6 o PRESSURE DOnaldIMurphy At to rlzey Patented Sept. 22,
UNITED STATE HIGH ALTITUDE PRESSURE RESPONSIVE CAPSULE Donald Francis Murphy, Baltimore, Md., assignor to Bendix Aviation Corporation, Baltimore, Md.,
a. corporation of Delaware Application May 18, 1948, Serial No. 27,755
3 Claims. 1
This invention relates to devices for converting pressure variations into mechanical displacements and more particularly to a device of this nature having arelatively large deflection-pressure modulus in the presence of low pressures and a relatively small deflection-pressure modulus in the presence of pressures exceeding a predeter mined. level.
In making precise pressure controlled measurements at relatively low pressures, it is desired that the mechanical pressure sensing unit be characterized by a large displacement for a small pressure change. The satisfaction of this requirement with a unit having a constant deflection-pressure modulus results in an assembly having an excessive travel which may be diflicult to accommodate in an indicating unitintended to provide accurate indications'in a limited low pressure range. It has previously been the practice to employ stops disengaging the lever arm or other transmission link from the pressure driving unit whenever its deflections fell without a predetermined range. Such stops, however, being separate from the pressure responsive driving unit and usually associated witha lever system burdened by variable and unpredictable amounts of play, have not proven entirely satisfactory. Further, it is fundamental in instrumentation that an increase in the number of elements participating in a given observation must inevitably vitiate the over-all accuracy to be obtained. Such an arrangement further distributes 2 capsule assembly embodying the principles of the invention and Figure 2 illustrates graphically the deflectionpressure characteristic of the improved pressure capsule.
The capsule assembly includes a base disk I I having an apertured boss I] located centrally thereof. The bellows side of the base disk II is also provided with a central elevated land 20 which is circular in form. In. addition, the mounting disk II is apertured at the point I0, radially displaced outwardly of the land 20, to receive an exhaust'tubulation I8. If the mounting disk I I is of brass or some other material to which solder adheres readily, the exhaust tubulation I8 may be hermetically sweated in place.
An inner Sylphon bellows I6 of substantially cylindrical form has its open end sweated to the mounting disk II along the periphery of the circular land 20. The inner bellows I6 may be formed of a single sheet of material and have a closed end which is a continuation of that matecritical elements at spaced points in the instrument structure, rendering it sensitive to mechanical distortions arising from thermal changes and rough handling.
Accordingly, it is an object of the present invention to provide a new and novel pressure responsive mechanical driving unit intrinsically possessing a relatively large deflection-pressure modulus in the presence of low pressures and having means therein to preventv deflection in the presence of pressures exceeding a predetermined level.
It is an'other object of the invention to provide a new and novel pressure capsule assembly having a high deflection modulus in low pressure regions and having means to prevent deflection v for pressures exceeding a selected value.
Still another object of the invention is to provide a new and novel pressurecapsule assemblyin which the threshold of pressure indication may be conveniently adjusted.
Other objects and advantages of the invention will in part be obvious and in part be described when the following specification is read in conjunction with the drawings in which rial. The aperture of boss Il may be tapped and a threaded rod I3 with an enlarged end inserted therein with the enlarged end adjacent the end of the inner bellows I6 remote from the mounting disk I I: A collar I4 is slipped over the shank I3 and sweated into I of the threaded member place at the closed end of the inner bellows I6 in a position retaining the enlarged head of the threaded adjusting member I3 in engagement with a spring washer I9. It may be noted from I If more convenient, the order of assembly may be Figure 1 is a sectionalview through a pressure reversed. The driving disk I2 is similarly provided with an apertured boss whose aperture does not, however, extend through the driving member I2. This aperture may be tapped to receive a suitably threaded screw for easy connection with a driving link conveying the capsule motion to an indicator assembly. The inner Sylphon bellows I6, mounting disk II, outer Sylphon bellows I5, and the driving disk I2 define a sealed chamber venting to the exhaust tubulation I8. Thishermetically enclosed volume may be exhausted to any desired pressure by connecting the tubulation I8 with an evacuating system and sealing ofi the tubulation when the desired residual pressure within the sealed volume has been secured. The outer bellows I5 is relatively soft and is characterized by a large deflection-pressure modulus,
bellows l and the table formed thereby. A
partial withdrawal of the adjustment screw l3 permits the beginning of deflection at a relatively high pressure while its advancement, with consequent similar displacement of the limiting table formed by the inner bellows l6, decreases the pressure at which displacement beings in the presence of diminishing ambient pressure.
At the relatively high pressure corresponding to ground level, the flexible outer bellows i5 is driven toward the mounting disk H to firmly engage the driving disk l2 with the limiting table formed by the inner bellows I6. As the pressure is decreased, the force maintaining these two members in engagement decreases correspondingly until the pressure force equals the distortion-induced restoring force built up within the outer bellows l5. A-continuing reduction in pressure permits the bellows spring force to move the driving disk I2 outwardly away from the limiting table formed by inner bellows I 6.
The displacement characteristic of the composite pressure capsule assembly is graphically illustrated in Figure 2 in which increasing pressures are indicated by increasing displacements to the right on the abscissa and increasing displacements are indicated by increasing distances along the ordinate axis. When the pressure exceeds the critical value at 22, the driving disk and limiting table or abutment are in engagement and there is no travel of the driving disk as is at once evident from an inspection of the figure. A decrease in the pressure below the value corresponding to point 22 permits the bellows spring force to overcome the pressure-induced force with consequent increase in displacement along the line 23 until a travel corresponding to the point 2| has been attained at zero pressure.
The composite assembly just described is a compact pressure responsive driving unit satisfying the requirements developed earlier in this specification. It may be beneficially employed wherever a high deflection rate over a limited range of low pressures is required without the possibility of imparting excessive motions to sensitive lever systems in the presence of very high pressures.
There will be obvious to those skilled in the art many minor variations and modifications not departing materially from the principles of the invention, as they are capable of wide application.
What is claimed and desired to be secured by United States Letters Patent is:
1. A pressure responsive device having a substantially large deflection-pressure modulus in the presence of pressures not exceeding a predetermined pressure level and having means to prevent defiection in the presence of pressures greater than said predetermined level, comprising, in combination, a first flexible sealing partition having a substantially cylindrical form with one closed and one open end, a second flexible sealing partition having a smaller substantially cylindrical form with one closed and one open end situated within said first partition with its closed end adjacent the closed end of said first partition, a base member hermetically engaging said open ends and having an aperture within the region bounded by said second partition, and a member passing through said aperture adapted to maintain the closed end of said second partition at a desired distance from said base member, the volume between said partitions being evacuated to a residual pressure of very nearly zero absolute pressure.
2. A pressure responsive device having a substantially large deflection-pressure modulus in the presence of pressures not exceeding a. predetermined pressure level and having means to prevent deflection in the presence of pressures greater than said predetermined level, comprising, in combination, a first flexible sealing partition having a substantially cylindrical form with one closed and one open end, a second flexible sealing partition having a smaller substantially cylindrical form with one closed and one open end coaxially situated within said first partition with said closed ends adjacent, a base member hermetically engaging said open ends and having a threaded aperture coaxially situated with respect to said cylindrical partitions and a correspondingly threaded member extending through said aperture to a point adjacent the closed end of said second partition, the volume between said partitions being evacuated to a residual pressure of very nearly zero absolute pressure.
3. A pressure responsive device having a substantially large deflection-pressure modulus in the presence of pressures not exceeding a predetermined pressure level and having means to prevent deflection in the presence of pressures greater than said predetermined level, comprising, in combination, a first flexible sealing partition having a substantially cylindrical form, a disk sealingly engaging one end of said first partition, a second flexible sealing partition having a small er substantially cylindrical form with one closed and one open end coaxially situated within said first partition with said closed end adjacent said sealing disk, 2. base member hermetically engaging the other end of said first partition and said open end of said second partition and having a threaded aperture coaxially situated with respect to said cylindrical partitions, a correspondingly threaded member extending through said aperture and having an enlarged portion adjacent the closed end of said second partition, and a collar secured to said closed end of said second partition embracing said enlarged end of said threaded member, the volume between said partitions being evacuated to a residual pressure of very nearly zero absolute pressure.
DONALD FRANCIS MU RPHY.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,345,547 Roth Mar. 28, 1944 2,454,423 Baak Nov. 23, 1948 FOREIGN PATENTS Number Country Date 611,546 Great Britain of 1948 698,427 Germany Nov. 9, 1940
US27755A 1948-05-18 1948-05-18 High altitude pressure responsive capsule Expired - Lifetime US2652859A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US27755A US2652859A (en) 1948-05-18 1948-05-18 High altitude pressure responsive capsule

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US27755A US2652859A (en) 1948-05-18 1948-05-18 High altitude pressure responsive capsule

Publications (1)

Publication Number Publication Date
US2652859A true US2652859A (en) 1953-09-22

Family

ID=21839595

Family Applications (1)

Application Number Title Priority Date Filing Date
US27755A Expired - Lifetime US2652859A (en) 1948-05-18 1948-05-18 High altitude pressure responsive capsule

Country Status (1)

Country Link
US (1) US2652859A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2727705A (en) * 1953-08-11 1955-12-20 Westinghouse Electric Corp Pressure sensitive systems and apparatus
US2763450A (en) * 1953-08-11 1956-09-18 Westinghouse Electric Corp Pressure sensitive systems and apparatus
US2784729A (en) * 1952-02-24 1957-03-12 Schoffel Ludwig Valve device for independent pressure control of plural outlet bores
US2850871A (en) * 1954-01-11 1958-09-09 Marquardt Aircraft Co Automatic constant mach number control system
US5401069A (en) * 1993-05-04 1995-03-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Inflatable rescue device
WO2014152807A1 (en) * 2013-03-14 2014-09-25 Teleflex Medical Incorporated Rotary needle and expanding bellows pressure indicator
US11573163B2 (en) * 2018-04-03 2023-02-07 Trafag Ag Density monitor with integrated low pressure indicator

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE698427C (en) * 1936-10-31 1940-11-09 Aeg Pressure regulator with a large adjustment range
US2345547A (en) * 1942-02-09 1944-03-28 Pesco Products Co Tank valve assembly
GB611546A (en) * 1943-12-28 1948-11-01 Bendix Aviat Corp Pressure breathing oxygen regulator
US2454423A (en) * 1942-12-02 1948-11-23 Honeywell Regulator Co Safety switch for airplanes

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE698427C (en) * 1936-10-31 1940-11-09 Aeg Pressure regulator with a large adjustment range
US2345547A (en) * 1942-02-09 1944-03-28 Pesco Products Co Tank valve assembly
US2454423A (en) * 1942-12-02 1948-11-23 Honeywell Regulator Co Safety switch for airplanes
GB611546A (en) * 1943-12-28 1948-11-01 Bendix Aviat Corp Pressure breathing oxygen regulator

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2784729A (en) * 1952-02-24 1957-03-12 Schoffel Ludwig Valve device for independent pressure control of plural outlet bores
US2727705A (en) * 1953-08-11 1955-12-20 Westinghouse Electric Corp Pressure sensitive systems and apparatus
US2763450A (en) * 1953-08-11 1956-09-18 Westinghouse Electric Corp Pressure sensitive systems and apparatus
US2850871A (en) * 1954-01-11 1958-09-09 Marquardt Aircraft Co Automatic constant mach number control system
US5401069A (en) * 1993-05-04 1995-03-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Inflatable rescue device
WO2014152807A1 (en) * 2013-03-14 2014-09-25 Teleflex Medical Incorporated Rotary needle and expanding bellows pressure indicator
US11573163B2 (en) * 2018-04-03 2023-02-07 Trafag Ag Density monitor with integrated low pressure indicator

Similar Documents

Publication Publication Date Title
US3967504A (en) Differential pressure transmitter with low side overrange protection
US2652859A (en) High altitude pressure responsive capsule
US2443252A (en) Pressure operated rheostat
US3587515A (en) Pressure differential indicating means
US2761411A (en) Pressure indicating device
US2725749A (en) Pressure gage protector
US2502776A (en) Pressure gauge
US2426663A (en) Method of charging temperature
US2411796A (en) Pressure actuated electrical switch
US2648741A (en) Pressure operated temperature responsive switch
US2477801A (en) Air pressure switch
US3168826A (en) Atmospheric pressure compensation of load cells
US3094876A (en) Differential pressure gauge
US3271542A (en) Maximum safe speed indicating switch with contact shaped as the speed curve
US2648732A (en) Hermetically sealed pressure switch
US2367087A (en) Seal for differential pressure gauges
US2147108A (en) Rate of climb indicator
US3254573A (en) Support for pressure measuring diaphragm
US3091123A (en) Pressure gauge
US2159703A (en) Rate of climb indicator
US2431674A (en) Differential pressure switch
US2779838A (en) Absolute pressure switch
US2639616A (en) Compensated pressure gauge
US2272950A (en) Apparatus for the distant indication of displacements or deformations, and their applications
GB507992A (en) Improvements in rate of change of pressure indicating instruments such as rate of climb indicators for aircraft