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US1631262A - Variable-pressure-operated expansion device - Google Patents

Variable-pressure-operated expansion device Download PDF

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Publication number
US1631262A
US1631262A US83294A US8329426A US1631262A US 1631262 A US1631262 A US 1631262A US 83294 A US83294 A US 83294A US 8329426 A US8329426 A US 8329426A US 1631262 A US1631262 A US 1631262A
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United States
Prior art keywords
pressure
variable
expansion device
operated expansion
chamber
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Expired - Lifetime
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US83294A
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Gourdou Charles Edouard Pierre
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D16/00Control of fluid pressure
    • G05D16/04Control of fluid pressure without auxiliary power
    • G05D16/06Control of fluid pressure without auxiliary power the sensing element being a flexible membrane, yielding to pressure, e.g. diaphragm, bellows, capsule
    • G05D16/0616Control of fluid pressure without auxiliary power the sensing element being a flexible membrane, yielding to pressure, e.g. diaphragm, bellows, capsule the sensing element being a bellow
    • G05D16/0625Control of fluid pressure without auxiliary power the sensing element being a flexible membrane, yielding to pressure, e.g. diaphragm, bellows, capsule the sensing element being a bellow acting indirectly on the obturator, e.g. by a lever
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/1842Ambient condition change responsive
    • Y10T137/1939Atmospheric
    • Y10T137/2012Pressure
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7781With separate connected fluid reactor surface
    • Y10T137/7793With opening bias [e.g., pressure regulator]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7781With separate connected fluid reactor surface
    • Y10T137/7793With opening bias [e.g., pressure regulator]
    • Y10T137/7822Reactor surface closes chamber

Definitions

  • the object of my invention is to provide a variable pressure operated expansion device essentially characterized by the fact that, for the purpose of modifying the adjustment of the expansion gear, I use a variable auxiliary pressure.
  • This inlet is more or less closed by means of a clapper valve 2 kept in position by links 3 and 4. y
  • Said links are assembled in a rod 5 adapted to be moved up and down by the action of springs 6, 7, of an aneroid cap 8, 8 and of a more or less complex diaphragm 9.
  • the expansion device ispartitioned by the tight diaphragm '9 into two compartments, i. e., a lower compartment A, and an upper compartment B.
  • p be the expansion pressure in the lower compartment
  • 'H the pressure in the upper compartment
  • s and S the surfaces of diaphragm 9 and of cap 8
  • R the action of springs 6 and 7.
  • the multlphcation rat1o 1s v following characteristic, viz, to cause an eX- pausion pressure to be varied by the action measuring standard p.
  • the compressed gas admission valve could, in this case, be different from the one shown, for it would have to operate only within the limits ascribed to p, such limits determining the useful compression.
  • the diaphragms might be made directly to control the valves.
  • Such an embodiment is an application of Pascals principle, wherein pistons are replaced by diaphragms, equilibrium being lobtained when the pressures on the opposite operative surfaces are inversely proportional to said Surfaces.
  • the above described device may serve to supply an airman with expanded oxygen in sufficient quantity at any given altitude.
  • delivery through a calibrate-d aperture 10 is proportional to the square root 'of the difference between inside pressure p and outside pressure H.
  • the high pressure bottle is connected with the nozzle l.
  • the atmospheric pressure since the opening 10'is always open to the atmosphere crushes the aneroid capsules 8 and the inlet opening 1 is closed.
  • the pressure in A. is the same as the outer latmospheric pressure.
  • the spring 7 has expanded sulliciently to open the inlet l.
  • the apparatus begins to deliver.
  • the apparatus rises if the action of the undulated capsules 9 were neglected, the operation of the aneroid capsules 8 would result in maintaining on the inside of the chamber A a constant pressure as regards absolute value, since there is a. vacuum in the capsules 8.
  • the inside pressure is therefore regulated by the play of the springs 6 and 7 and by the size of the surfaces of the capsules 8 and 9 and their dif-
  • the openin and closing of vinlet 1 are due to the actlon of the outer ressure on the capsules 8 and the spring the outer pressure being communicated through opening 10.
  • the closing andv opening'ot ⁇ inlet 1" occur for the same value of the outer pressure and, at that'moment, the corrective capsule 9 is inactive.
  • a variable pressure operated expansion device comprising a fluid tight chamber closed on one side by a diaphragmon top of which va fluid under variable pressure exerts action, an inlet for the admission into the said chamber of the Huid to be expanded, a valvefor controlling said admission, and an outlet for the expanded fluid from the said chamber, members connected with the diaphragm and operating on said valve to reguate the admission of the iuid to be exanded into the chamber, said members bemg submitted to the action of springs and of an aneroid cap located within the chamber.
  • a variable pressure o crate-d expansion device comprising aflui tight chamber closed on one side by a diaphragm on the top of which a fluid under Variable pressure exerts action, a rod integral with said diaphragm, an aneroid cap and springs exertmg' their action on the said rod, links controlled by the said rod, a valve operated by one of said links to control the admission of the Huid to be expanded into the cl'mmloer ⁇ and an outlet from the chamber for the Huid expanded therein.

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Fluid Pressure (AREA)

Description

June 7, 1927.
l C. E. P. GOURDOU VARIABLE PRESSURE OPERATED EXPANSION DEVICE Filed Jan. 23. 1926 @zartes-Edouard Pierre Gourdon.
'Hy 6 Arm/em.
Patented June 7, 1927.
UNITED STATES 1,631,262 PATENT OFFICE.
CHARLES EDOUARD PIERRE GoURDoU, or sr. MANDE, FRANGE. l
'VARIABLE-PRESSURE-OPERATED EXPANSION DEVICE. 'l
Application led January 23, 1926,VSeria1 No.'83,294, and in France February 5, 1925.
The object of my invention is to provide a variable pressure operated expansion device essentially characterized by the fact that, for the purpose of modifying the adjustment of the expansion gear, I use a variable auxiliary pressure.
In order to make` my invention more clearly understood, I have illustrated, as an example, an embodiment thereof in the drawing appended hereto.
Referring to said drawing: The compressed gasintended to be expanded under variable 4,pressure is led through a duct tothe inlet 1 of the expansion device.
This inlet is more or less closed by means of a clapper valve 2 kept in position by links 3 and 4. y
Said links are assembled in a rod 5 adapted to be moved up and down by the action of springs 6, 7, of an aneroid cap 8, 8 and of a more or less complex diaphragm 9.
As shown by the drawing, the expansion device ispartitioned by the tight diaphragm '9 into two compartments, i. e., a lower compartment A, and an upper compartment B. l Let, then, p be the expansion pressure in the lower compartment, 'H the pressure in the upper compartment, s and S, the surfaces of diaphragm 9 and of cap 8, R the action of springs 6 and 7.
The balance equation on the whole of the membranes will read: v
p(8-S)+Hs-Rs=0 or l . s P+ S{RH) neglecting the effect of the pressure of the compressed gas on clapper valve 2, a pressure-transmitted with very high reduction ratio by links 3 and 4 to rod 5.
As will be apparent, p (the expansion pressure) is linear function of H.
p decreases when H increases. The multlphcation rat1o 1s v following characteristic, viz, to cause an eX- pausion pressure to be varied by the action measuring standard p.
The compressed gas admission valve could, in this case, be different from the one shown, for it would have to operate only within the limits ascribed to p, such limits determining the useful compression.
In this case, the diaphragms might be made directly to control the valves.
Such an embodiment is an application of Pascals principle, wherein pistons are replaced by diaphragms, equilibrium being lobtained when the pressures on the opposite operative surfaces are inversely proportional to said Surfaces.
More particularly, the above described device may serve to supply an airman with expanded oxygen in sufficient quantity at any given altitude.
In fact, delivery through a calibrate-d aperture 10 is proportional to the square root 'of the difference between inside pressure p and outside pressure H.
Apparently, to obtain suitable deliveries proportional toaltitude, one has but suitably to select expansion remain constant, and to select the caliber or gauge of the aperture so as to ensure both inception of -delivery at an altitude corresponding to pressure p and any value thereof at another altitude.
In practice, however, the apertures having to be minute, viscosity intervenes and delivery tends to become constant and even to decrease when Hy decreases.
I am, therefore, led to try and increase P when H decreases.
The above described device enables me to to do so, pressure H getting established on diaphragm 9 through aperture 11.
I thus obtain any required delivery.
Adjustment is possible by tightening cap 12, which sets spring 6, and by positioning stop 13, which adjusts the position of 3 and 4.
In operation the high pressure bottle is connected with the nozzle l. On the ground level the atmospheric pressure since the opening 10'is always open to the atmosphere crushes the aneroid capsules 8 and the inlet opening 1 is closed. Itshould be noted that as long as there is no delivery, the pressure in A. is the same as the outer latmospheric pressure. At the altitude chosen for the beginning of the supply, the spring 7 has expanded sulliciently to open the inlet l. At that moment the apparatus begins to deliver. As the apparatus rises, if the action of the undulated capsules 9 were neglected, the operation of the aneroid capsules 8 would result in maintaining on the inside of the chamber A a constant pressure as regards absolute value, since there is a. vacuum in the capsules 8. Now, what the inventor desires, as has been explained at the beginning of the description, is that the pressure on the inside of the sole chamber progressively increases as there is an ascent in the atmosphere.
Let us suppose we are in a state of equilibrium at a given altitude, capsule 9 being considered as entirely rigid. If, at this moment, the said capsule becomes soft, the difference in pressure between the inside and the outside will collapse it and, under these conditions, the springy 6 will be compressed. Consequently, the levers 3 and 4 will open the inlet opening 1 still further. The result i will be that the pressure on the inside of A 'ference in area.
will rise to a new state of equilibrium, and so forth thereafter. The inside pressure is therefore regulated by the play of the springs 6 and 7 and by the size of the surfaces of the capsules 8 and 9 and their dif- As a matter of fact, the openin and closing of vinlet 1 are due to the actlon of the outer ressure on the capsules 8 and the spring the outer pressure being communicated through opening 10. The closing andv opening'ot` inlet 1" occur for the same value of the outer pressure and, at that'moment, the corrective capsule 9 is inactive.
Having now fully ascertained and disclosed the nature of my said invention as well as the manner in which the same is to be performed, I declare thatv what I claim 1s:
1. A variable pressure operated expansion device comprising a fluid tight chamber closed on one side by a diaphragmon top of which va fluid under variable pressure exerts action, an inlet for the admission into the said chamber of the Huid to be expanded, a valvefor controlling said admission, and an outlet for the expanded fluid from the said chamber, members connected with the diaphragm and operating on said valve to reguate the admission of the iuid to be exanded into the chamber, said members bemg submitted to the action of springs and of an aneroid cap located within the chamber.
2. A variable pressure o crate-d expansion device comprising aflui tight chamber closed on one side by a diaphragm on the top of which a fluid under Variable pressure exerts action, a rod integral with said diaphragm, an aneroid cap and springs exertmg' their action on the said rod, links controlled by the said rod, a valve operated by one of said links to control the admission of the Huid to be expanded into the cl'mmloer` and an outlet from the chamber for the Huid expanded therein.
In testlmony whereof I aix myr signature.
CHARLES EDOUARD PIERRE GOUR'DOU.
US83294A 1925-02-05 1926-01-23 Variable-pressure-operated expansion device Expired - Lifetime US1631262A (en)

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2544991A (en) * 1945-11-08 1951-03-13 Bendix Aviat Corp Pressure breathing regulator
US2560210A (en) * 1941-04-09 1951-07-10 Wright Aeronautical Corp Engine pressure control mechanism having housing containing an evacuated bellows and vented bellows
US2593046A (en) * 1944-05-29 1952-04-15 Albert E Mckee Oxygen administration
US2599956A (en) * 1946-06-08 1952-06-10 Wallace & Tiernan Inc Absolute pressure controlling apparatus
US2699174A (en) * 1950-02-18 1955-01-11 Rochette Rene Etienne Gas delivery regulator
US2706885A (en) * 1948-01-15 1955-04-26 Mcdonnell Aircraft Corp Fuel regulator responsive to speed and atmospheric pressure
US2861588A (en) * 1954-12-30 1958-11-25 Worthington Corp Fluid pressure regulators
US3094839A (en) * 1958-09-29 1963-06-25 Bendix Corp Bellows arrangement providing failure protection
US3143134A (en) * 1960-12-12 1964-08-04 John J Karpis Fluid regulator
US3219309A (en) * 1962-05-09 1965-11-23 Holley Carburetor Co Pressure ratio device
US3706270A (en) * 1969-12-09 1972-12-19 Westland Aircraft Ltd Pressure control systems
US20100317276A1 (en) * 2006-12-06 2010-12-16 Nord-Micro Ag & Co. Ohg Control unit for actuating a pressure valve, in particular a differential pressure valve of an aircraft cabin

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2560210A (en) * 1941-04-09 1951-07-10 Wright Aeronautical Corp Engine pressure control mechanism having housing containing an evacuated bellows and vented bellows
US2593046A (en) * 1944-05-29 1952-04-15 Albert E Mckee Oxygen administration
US2544991A (en) * 1945-11-08 1951-03-13 Bendix Aviat Corp Pressure breathing regulator
US2599956A (en) * 1946-06-08 1952-06-10 Wallace & Tiernan Inc Absolute pressure controlling apparatus
US2706885A (en) * 1948-01-15 1955-04-26 Mcdonnell Aircraft Corp Fuel regulator responsive to speed and atmospheric pressure
US2699174A (en) * 1950-02-18 1955-01-11 Rochette Rene Etienne Gas delivery regulator
US2861588A (en) * 1954-12-30 1958-11-25 Worthington Corp Fluid pressure regulators
US3094839A (en) * 1958-09-29 1963-06-25 Bendix Corp Bellows arrangement providing failure protection
US3143134A (en) * 1960-12-12 1964-08-04 John J Karpis Fluid regulator
US3219309A (en) * 1962-05-09 1965-11-23 Holley Carburetor Co Pressure ratio device
US3706270A (en) * 1969-12-09 1972-12-19 Westland Aircraft Ltd Pressure control systems
US20100317276A1 (en) * 2006-12-06 2010-12-16 Nord-Micro Ag & Co. Ohg Control unit for actuating a pressure valve, in particular a differential pressure valve of an aircraft cabin
US8808071B2 (en) * 2006-12-06 2014-08-19 Nord-Micro Ag & Co. Ohg Control unit for actuating a pressure valve, in particular a differential pressure valve of an aircraft cabin

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