US20010002596A1 - Liquid circuit reservoir - Google Patents
Liquid circuit reservoir Download PDFInfo
- Publication number
- US20010002596A1 US20010002596A1 US09/725,565 US72556500A US2001002596A1 US 20010002596 A1 US20010002596 A1 US 20010002596A1 US 72556500 A US72556500 A US 72556500A US 2001002596 A1 US2001002596 A1 US 2001002596A1
- Authority
- US
- United States
- Prior art keywords
- reservoir
- liquid
- partition
- bottom chamber
- deaerator
- 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.)
- Granted
Links
- 239000007788 liquid Substances 0.000 title claims abstract description 41
- 238000005192 partition Methods 0.000 claims abstract description 29
- 238000007872 degassing Methods 0.000 claims abstract description 14
- 230000005484 gravity Effects 0.000 claims abstract description 12
- 238000010276 construction Methods 0.000 description 4
- 239000000839 emulsion Substances 0.000 description 2
- 239000012141 concentrate Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/14—Filling or emptying
- B64D37/20—Emptying systems
- B64D37/22—Emptying systems facilitating emptying in any position of tank
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/0753—Control by change of position or inertia of system
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/0753—Control by change of position or inertia of system
- Y10T137/0874—Vent opening or closing on tipping container
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2931—Diverse fluid containing pressure systems
- Y10T137/3003—Fluid separating traps or vents
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2931—Diverse fluid containing pressure systems
- Y10T137/3003—Fluid separating traps or vents
- Y10T137/3084—Discriminating outlet for gas
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/86292—System with plural openings, one a gas vent or access opening
- Y10T137/86324—Tank with gas vent and inlet or outlet
Definitions
- the invention relates to a reservoir for a liquid circuit, and more particularly to a reservoir construction for ensuring correct feeding of the circuit under all circumstances, even when the reservoir is inverted.
- Reservoirs in liquid circuits act to collect the excess liquid in the circuit for recirculation. They communicate with the circuit by way of an inlet conduit which returns the liquid from the remainder of the circuit, and by way of an outlet conduit through which liquid for the circuit is aspirated by pumps. Since reservoirs of this kind are only partly full the outlet conduit draws from the bottom of the reservoir. However, when the reservoir is inverted, as occurs when it is part of a liquid circuit in an aircraft and the aircraft flies upside-down, or more generally when it is subjected to conditions of gravity reversal, the liquid flows to the other side of the reservoir and leaves the outlet conduit dry, so that the supply of liquid to the circuit is temporarily interrupted.
- FIG. 1 shows a reservoir 1 which is divided into two chambers by a perforated horizontal partition 2 .
- the inlet conduit 4 opens into the top chamber 5 and the outlet conduit 6 is at the bottom of the lower chamber 7 .
- a valve 8 is installed below the partition 2 and consists of a flexible diaphragm riveted at its centre to the partition 2 by an element 3 .
- the liquid entering from the inlet conduit 4 accumulates on the partition 2 , flows through the perforations therein and bends the valve 8 into an umbrella shape to allow it into the lower chamber 7 .
- the liquid filling the lower chamber 7 weighs on the valve 8 , which thus closes and prevents the liquid from returning to the top chamber 5 .
- the outlet conduit 6 is extended by a tube 9 which projects into the lower chamber 7 , and is able to aspirate liquid provided the liquid level in the chamber 7 is above the edge 10 of the tube 9 —i.e. provided the liquid occupies substantially the volume 11 indicated in FIG. 1.
- supply of liquid to the circuit is still interrupted when the volume 11 falls, so that in practice the reservoir 1 must be larger than the conventional reservoirs in order to accommodate the tube 9 and the required volume of liquid around it, such volume remaining stagnant and unused under normal flight conditions.
- the reservoir comprises a partition which divides the reservoir to define a bottom chamber therein and which is provided with at least one aperture.
- the liquid inlet and outlet conduits both open into the bottom chamber and the partition aperture is arranged to remain permanently open whatever the position or orientation of the reservoir—i.e., the partition is valveless. Since the bottom of the reservoir is fairly close to the partition, the reservoir volume is reduced. The bottom chamber is normally completely full and the excess liquid forms a reserve in the top chamber.
- the inlet conduit continues to feed liquid into the bottom chamber so that the outlet conduit cannot run dry even during a long period of inversion. Liquid leakage from the bottom chamber is tolerated but total emptying of the bottom chamber is avoided if the partition is constructed as an inverted tray or if the apertures in the partition are bounded by edges extending from the partition towards the bottom of the reservoir.
- the invention provides a reservoir for a liquid circuit, comprising a partition dividing said reservoir to define a bottom chamber therein, means defining at least one aperture in said partition adapted to remain open in any position of said reservoir, a liquid inlet conduit opening into said bottom chamber, a liquid outlet conduit leading from said bottom chamber, a deaerator mounted on said partition in communication with said bottom chamber, said deaerator having a degassing orifice which opens outside said bottom chamber, and a valve which is operable by gravity to close said degassing orifice when said reservoir is inverted or subjected to negative gravity.
- the deaerator extends through the partition with its degassing orifice disposed outside the bottom chamber, with the result that the contents of the bottom chamber remain completely liquid and the feed to the circuit is of good quality. Also, leakage of liquid through the degassing orifice in the event of inversion is prevented by the valve which is associated with the orifice and which closes under gravity in the event of inversion or negative gravity.
- FIG. 1 is a schematic sectional view of a prior art reservoir
- FIG. 2 is a schematic sectional view of a preferred embodiment of a reservoir according to the invention.
- the deaerator 19 has a centrifugal action, the inlet conduit 18 delivering the liquid-gas emulsion tangentially into the domed top 20 of the deaerator to impart a whirling motion to the liquid-gas emulsion which concentrates the liquid towards the wall and the gas towards the centre of the deaerator.
- the gas rises towards the top of the dome 20 and leaves through a degassing orifice 21 provided at the top of the dome 20 , whereas the degassed liquid drops downwards into the bottom chamber 15 .
- the degassing orifice 21 opens into the top chamber 16 since the dome 20 of the deaerator projects through the partition 13 . Separation of the gas and liquid is enhanced since they are discharged on opposite sides of the partition 13 .
- the deaerator is normally totally immersed because the top chamber 16 is partly full, but that does not alter its operation.
- the partition 13 is continuous across the reservoir 12 except for a small aperture 22 which is surrounded by a wall 23 which extends from the partition 13 almost as far as the reservoir bottom 14 .
- This wall 23 co-operates with the partition 13 to form an inverted tray 24 in which liquid can accumulate when the reservoir is inverted, and the outlet conduit 17 opens above the lower end of the wall 23 .
- the entrance to the outlet conduit 17 therefore remains immersed in the liquid filling the bottom chamber 15 , which continues to be fed by the inlet conduit 18 , when the reservoir is inverted.
- the deaerator has a valve 28 which opens or closes the degassing orifice 21 .
- the valve 28 basically consists of a ball 29 which is movable within a vertical sleeve 30 by gravity, the sleeve 30 surrounding the degassing aperture 21 at the top and extending axially downwards within the deaerator.
- the ball 29 sits at the bottom of the sleeve so that gas is able to enter the sleeve 30 through an aperture 31 in its side wall and then to be discharged through the open degassing orifice 21 .
- the ball 29 moves to the top of the sleeve 30 where it closes the degassing orifice 21 .
- the reference 32 denotes an external pressure connection at the top of the reservoir 12 , the connection 32 serving to vent gas accumulating in the reservoir 12 but playing no direct part in the operation of the invention.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
- Degasification And Air Bubble Elimination (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
Abstract
Description
- 1. Field of the Invention
- The invention relates to a reservoir for a liquid circuit, and more particularly to a reservoir construction for ensuring correct feeding of the circuit under all circumstances, even when the reservoir is inverted.
- 2. Summary of the Prior Art
- Reservoirs in liquid circuits act to collect the excess liquid in the circuit for recirculation. They communicate with the circuit by way of an inlet conduit which returns the liquid from the remainder of the circuit, and by way of an outlet conduit through which liquid for the circuit is aspirated by pumps. Since reservoirs of this kind are only partly full the outlet conduit draws from the bottom of the reservoir. However, when the reservoir is inverted, as occurs when it is part of a liquid circuit in an aircraft and the aircraft flies upside-down, or more generally when it is subjected to conditions of gravity reversal, the liquid flows to the other side of the reservoir and leaves the outlet conduit dry, so that the supply of liquid to the circuit is temporarily interrupted.
- An arrangement for obviating this disadvantage is disclosed in French patent No. 2621662, from which FIG. 1 of the attached drawings is taken. FIG. 1 shows a reservoir1 which is divided into two chambers by a perforated horizontal partition 2. The inlet conduit 4 opens into the top chamber 5 and the
outlet conduit 6 is at the bottom of the lower chamber 7. A valve 8 is installed below the partition 2 and consists of a flexible diaphragm riveted at its centre to the partition 2 by an element 3. The liquid entering from the inlet conduit 4 accumulates on the partition 2, flows through the perforations therein and bends the valve 8 into an umbrella shape to allow it into the lower chamber 7. When the reservoir 1 is inverted, the liquid filling the lower chamber 7 weighs on the valve 8, which thus closes and prevents the liquid from returning to the top chamber 5. Theoutlet conduit 6 is extended by a tube 9 which projects into the lower chamber 7, and is able to aspirate liquid provided the liquid level in the chamber 7 is above theedge 10 of the tube 9—i.e. provided the liquid occupies substantially thevolume 11 indicated in FIG. 1. However, supply of liquid to the circuit is still interrupted when thevolume 11 falls, so that in practice the reservoir 1 must be larger than the conventional reservoirs in order to accommodate the tube 9 and the required volume of liquid around it, such volume remaining stagnant and unused under normal flight conditions. - Constructions are also known in which the reservoir comprises a partition which divides the reservoir to define a bottom chamber therein and which is provided with at least one aperture. The liquid inlet and outlet conduits both open into the bottom chamber and the partition aperture is arranged to remain permanently open whatever the position or orientation of the reservoir—i.e., the partition is valveless. Since the bottom of the reservoir is fairly close to the partition, the reservoir volume is reduced. The bottom chamber is normally completely full and the excess liquid forms a reserve in the top chamber. When the reservoir is inverted the inlet conduit continues to feed liquid into the bottom chamber so that the outlet conduit cannot run dry even during a long period of inversion. Liquid leakage from the bottom chamber is tolerated but total emptying of the bottom chamber is avoided if the partition is constructed as an inverted tray or if the apertures in the partition are bounded by edges extending from the partition towards the bottom of the reservoir.
- However, this construction cannot ensure that liquid leaving the reservoir through the outlet conduit is completely free from gas bubbles, because bubbles introduced into the reservoir through the inlet conduit accumulate below the partition under normal conditions and rise through the bottom chamber towards the outlet conduit when the reservoir is inverted. Also, hydraulic control circuits for engines, a field in which the invention is particularly applicable, are usually well degassed except in special circumstances such as purging or abrupt manoeuvring, when large gas bubbles may be formed and may therefore occupy much of the bottom chamber and be aspirated through the outlet line even if positive gravity is maintained. The apertures with which the partition is sometimes provided for gradually removing the gas from the bottom chamber are then ineffective, and they still have the disadvantage of allowing the bottom chamber to empty during a prolonged period of negative gravity. Because of this, the construction in unacceptable and the prevent invention aims to overcome these disadvantages.
- Accordingly, the invention provides a reservoir for a liquid circuit, comprising a partition dividing said reservoir to define a bottom chamber therein, means defining at least one aperture in said partition adapted to remain open in any position of said reservoir, a liquid inlet conduit opening into said bottom chamber, a liquid outlet conduit leading from said bottom chamber, a deaerator mounted on said partition in communication with said bottom chamber, said deaerator having a degassing orifice which opens outside said bottom chamber, and a valve which is operable by gravity to close said degassing orifice when said reservoir is inverted or subjected to negative gravity.
- The deaerator extends through the partition with its degassing orifice disposed outside the bottom chamber, with the result that the contents of the bottom chamber remain completely liquid and the feed to the circuit is of good quality. Also, leakage of liquid through the degassing orifice in the event of inversion is prevented by the valve which is associated with the orifice and which closes under gravity in the event of inversion or negative gravity.
- FIG. 1 is a schematic sectional view of a prior art reservoir; and,
- FIG. 2 is a schematic sectional view of a preferred embodiment of a reservoir according to the invention.
- The reservoir shown in FIG. 2 has the
general reference 12, and apartition 13 near thebottom 14 of the reservoir divides it into abottom chamber 15 which is smaller than the bottom chamber of the reservoir shown in FIG. 1, and atop chamber 16. Anoutlet conduit 17 leads from thebottom chamber 15 through thebottom 14 of the reservoir in a conventional manner. Aninlet conduit 18 also communicates with thebottom chamber 15 of thereservoir 12, theconduit 18 opening into a deaerator 19 which is mounted on and extends through thepartition 13. The deaerator 19 has a centrifugal action, theinlet conduit 18 delivering the liquid-gas emulsion tangentially into thedomed top 20 of the deaerator to impart a whirling motion to the liquid-gas emulsion which concentrates the liquid towards the wall and the gas towards the centre of the deaerator. The gas rises towards the top of thedome 20 and leaves through adegassing orifice 21 provided at the top of thedome 20, whereas the degassed liquid drops downwards into thebottom chamber 15. Thedegassing orifice 21 opens into thetop chamber 16 since thedome 20 of the deaerator projects through thepartition 13. Separation of the gas and liquid is enhanced since they are discharged on opposite sides of thepartition 13. The deaerator is normally totally immersed because thetop chamber 16 is partly full, but that does not alter its operation. - The
partition 13 is continuous across thereservoir 12 except for asmall aperture 22 which is surrounded by awall 23 which extends from thepartition 13 almost as far as thereservoir bottom 14. Thiswall 23 co-operates with thepartition 13 to form an invertedtray 24 in which liquid can accumulate when the reservoir is inverted, and theoutlet conduit 17 opens above the lower end of thewall 23. The entrance to theoutlet conduit 17 therefore remains immersed in the liquid filling thebottom chamber 15, which continues to be fed by theinlet conduit 18, when the reservoir is inverted. - To limit leakage of liquid into the
top chamber 16 when the reservoir is inverted, the deaerator has avalve 28 which opens or closes thedegassing orifice 21. Thevalve 28 basically consists of aball 29 which is movable within a vertical sleeve 30 by gravity, the sleeve 30 surrounding thedegassing aperture 21 at the top and extending axially downwards within the deaerator. When the reservoir is oriented the right way up, theball 29 sits at the bottom of the sleeve so that gas is able to enter the sleeve 30 through anaperture 31 in its side wall and then to be discharged through the opendegassing orifice 21. However, when the reservoir is inverted or is subjected to negative gravity, theball 29 moves to the top of the sleeve 30 where it closes thedegassing orifice 21. - Tests have showed that the deaerator19 is satisfactorily sealed by the
valve 28 when fully immersed and can deal effectively with a large incoming gas bubble. - The
reference 32 denotes an external pressure connection at the top of thereservoir 12, theconnection 32 serving to vent gas accumulating in thereservoir 12 but playing no direct part in the operation of the invention. - An important application for the invention is the reservoirs in the hydraulic circuits of aircraft flight controls and other aircraft equipment.
Claims (1)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP99204094 | 1999-12-02 | ||
EP99204094.9 | 1999-12-02 | ||
EP99204094A EP1104742B1 (en) | 1999-12-02 | 1999-12-02 | Tank for liquid supply |
Publications (2)
Publication Number | Publication Date |
---|---|
US20010002596A1 true US20010002596A1 (en) | 2001-06-07 |
US6394123B2 US6394123B2 (en) | 2002-05-28 |
Family
ID=8240964
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/725,565 Expired - Lifetime US6394123B2 (en) | 1999-12-02 | 2000-11-30 | Liquid circuit reservoir |
Country Status (3)
Country | Link |
---|---|
US (1) | US6394123B2 (en) |
EP (1) | EP1104742B1 (en) |
DE (1) | DE69909799T2 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050173297A1 (en) * | 2002-05-22 | 2005-08-11 | Yasuhiro Toida | Adsorption desulfurization agent for desulfurizing petroleum fraction and desulfurization method using the same |
US20100065374A1 (en) * | 2008-09-18 | 2010-03-18 | United Technologies Corporation | Continuous supply fluid reservoir |
EP2535097A1 (en) * | 2011-06-17 | 2012-12-19 | Hamilton Sundstrand Corporation | Deaerator and conduit assembly |
CN104389684A (en) * | 2014-12-04 | 2015-03-04 | 江西洪都航空工业集团有限责任公司 | Rotatably flexible oil extractor |
US20210331089A1 (en) * | 2020-04-28 | 2021-10-28 | Ariston Thermo S.P.A. | Deaerator for the evacuation of gases in fluid based heat exchange systems |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6913040B2 (en) * | 2003-03-24 | 2005-07-05 | Visteon Global Technologies, Inc. | Hydraulic fluid reservoir |
US20080173362A1 (en) * | 2007-01-19 | 2008-07-24 | Wong Albert C | Hydraulic reservoir with baffle |
CN101761394B (en) * | 2008-12-23 | 2013-07-24 | 江西洪都航空工业集团有限责任公司 | Negative overload resistant double-chamber oil supply device and method thereof |
US8529668B2 (en) | 2012-01-13 | 2013-09-10 | Hamilton Sundstrand Corporation | Deaerator outlet diffuser |
US8500869B1 (en) | 2012-06-21 | 2013-08-06 | Hamilton Sundstrand Corporation | Anti-rotation deaerator outlet diffuser |
US9341115B2 (en) * | 2012-06-26 | 2016-05-17 | United Technologies Corporation | Valve for controlling flow of a turbomachine fluid |
US9206741B2 (en) | 2012-11-30 | 2015-12-08 | United Technologies Corporation | Fluid system with gravity controlled valve |
US9981752B2 (en) | 2016-09-27 | 2018-05-29 | Pratt & Whitney Canada Corp. | Liquid tank system with over pressure protection |
FR3114861B1 (en) * | 2020-10-01 | 2022-08-19 | Airbus Helicopters | Lubrication system with an emergency tank |
US20220316361A1 (en) * | 2021-03-31 | 2022-10-06 | Pratt & Whitney Canada Corp. | Oil tank for aircraft engine |
EP4296476A1 (en) * | 2022-06-24 | 2023-12-27 | Safran Aero Boosters | Oil tank for turbine engine with negative-compatible cyclonic circulation |
EP4296491A1 (en) * | 2022-06-24 | 2023-12-27 | Safran Aero Boosters | Oil reservoir for a turbine engine with lower compartment with negative g compatible oil outlet duct |
EP4296475A1 (en) * | 2022-06-24 | 2023-12-27 | Safran Aero Boosters | Oil tank with lower compartment having negative g compatible oil-discharging conduit |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2942612A (en) * | 1959-05-21 | 1960-06-28 | United Aircraft Prod | Liquid storage tank |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB580006A (en) * | 1943-04-20 | 1946-08-23 | George Howard Farmer | Improvements in or relating to tanks for liquid fuel or other liquids especially for use in aircraft |
US2860648A (en) * | 1955-12-28 | 1958-11-18 | Gen Electric | Anti "g" liquid reservoir |
US2975793A (en) * | 1959-09-08 | 1961-03-21 | United Aircraft Prod | Liquid storage tank |
KR100265136B1 (en) * | 1995-12-27 | 2001-01-15 | 정몽규 | Vent valve of fuel tank for vehicle |
-
1999
- 1999-12-02 EP EP99204094A patent/EP1104742B1/en not_active Expired - Lifetime
- 1999-12-02 DE DE69909799T patent/DE69909799T2/en not_active Expired - Lifetime
-
2000
- 2000-11-30 US US09/725,565 patent/US6394123B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2942612A (en) * | 1959-05-21 | 1960-06-28 | United Aircraft Prod | Liquid storage tank |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050173297A1 (en) * | 2002-05-22 | 2005-08-11 | Yasuhiro Toida | Adsorption desulfurization agent for desulfurizing petroleum fraction and desulfurization method using the same |
US20100065374A1 (en) * | 2008-09-18 | 2010-03-18 | United Technologies Corporation | Continuous supply fluid reservoir |
US8181746B2 (en) * | 2008-09-18 | 2012-05-22 | United Technologies Corporation | Continuous supply fluid reservoir |
US20120181112A1 (en) * | 2008-09-18 | 2012-07-19 | United Technologies Corporation | Continuous supply fluid reservoir |
US8602165B2 (en) | 2008-09-18 | 2013-12-10 | United Technologies Corporation | Continuous supply fluid reservoir |
US8997935B2 (en) * | 2008-09-18 | 2015-04-07 | United Technologies Corporation | Continuous supply fluid reservoir |
EP2535097A1 (en) * | 2011-06-17 | 2012-12-19 | Hamilton Sundstrand Corporation | Deaerator and conduit assembly |
US8444751B2 (en) | 2011-06-17 | 2013-05-21 | Hamilton Sundstrand Corporation | Deaerator and conduit assembly |
CN104389684A (en) * | 2014-12-04 | 2015-03-04 | 江西洪都航空工业集团有限责任公司 | Rotatably flexible oil extractor |
US20210331089A1 (en) * | 2020-04-28 | 2021-10-28 | Ariston Thermo S.P.A. | Deaerator for the evacuation of gases in fluid based heat exchange systems |
US12017156B2 (en) * | 2020-04-28 | 2024-06-25 | Ariston S.P.A. | Deaerator for the evacuation of gases in fluid based heat exchange systems |
Also Published As
Publication number | Publication date |
---|---|
EP1104742A1 (en) | 2001-06-06 |
DE69909799T2 (en) | 2004-05-27 |
EP1104742B1 (en) | 2003-07-23 |
DE69909799D1 (en) | 2003-08-28 |
US6394123B2 (en) | 2002-05-28 |
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