US2943841A - Storage tank for liquid circulating system - Google Patents

Storage tank for liquid circulating system Download PDF

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Publication number
US2943841A
US2943841A US733347A US73334758A US2943841A US 2943841 A US2943841 A US 2943841A US 733347 A US733347 A US 733347A US 73334758 A US73334758 A US 73334758A US 2943841 A US2943841 A US 2943841A
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United States
Prior art keywords
oil
storage tank
tank
shell
hopper
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Expired - Lifetime
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US733347A
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Paul R Hughes
Jr Walter C Klank
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United Aircraft Products Inc
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United Aircraft Products Inc
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Priority to US733347A priority Critical patent/US2943841A/en
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Publication of US2943841A publication Critical patent/US2943841A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16NLUBRICATING
    • F16N39/00Arrangements for conditioning of lubricants in the lubricating system
    • F16N39/04Arrangements for conditioning of lubricants in the lubricating system by heating
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/342Tank with heat exchanger
    • Y10S165/348Heat exchanger within tank
    • Y10S165/349Supported by cover for tank
    • 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
    • Y10T137/7287Liquid level responsive or maintaining systems
    • Y10T137/731With control fluid connection at desired liquid level

Definitions

  • This invention relates to systems circulating a congealable liquid, and particularly to a storage tank therein providing a reservoir whereby a portion of the circulating liquid is available for use as a hydraulic fluid.
  • An object of the invention is to adapt a known storage tank of the prior art, reference being had in particular to the storage tank disclosed in Patent No. 2,733,050 issued January 31, 1956, to Harry T. Booth, to incorporate therein a reservoir as described.
  • Another object of the invention is to provide a reser voir as described occupying a relatively small part of the storage tank 'but so situated in the tank as to insure an ample supply of hydraulic fluid both for repeated withdrawals, as for example in. a repeated exercising of a propeller feathering mechanism, and for emergency use, it being contemplatedthat an adequate supply of liquid will remain in the reservoir for emergency use even though the total'supply ofliquid in the circulating system is seriously depleted.
  • the storage tank thereof is one found in the engine lubricant circulating systems of aircraft and functions to hold a supply of replacement lubricant or oil while a portion of the lubricant continuously is circulated to and from the engine and through a hopper device installed within the tank.
  • a storage tank for lubricating oil is seen to comprise an outer shell holding the main body 11 of stored lubricant.
  • a hopper assembly 12 comprising concentric, cylindrical inner and outer shells 13 and 14 spaced apart to define therebetween an annular space 15.
  • the upper end or top of the outer shell 14 extends above the corresponding end of the inner shell 13 and may be closed by a cap 16, with restricted communication between the upper end of the outer shell 14 and the interior of the tank 10 proper being provided by small diameter openings 17 in the shell.
  • the openings 17 provide for overflow from the hopper system into the tank and may serve also to obtain a pressurizing of the hopper system in a manner and for purposes which it is unnecessary here to consider.
  • the outer shell 14 has a conical bottom portion 18.
  • the inner shell 13 has a similar bottom portion 19 which is, however, in non-parallel relation to the bottom 18 and in relatively widely spaced relation thereto in such manner as to define in the bottom of the outer shell 14 a relatively deep chamber 21 communicating at its upper periphery with the annular passage 15.
  • An outlet conductor 24 communicates at, its one end with the chamber 21 and extends at its other end to and through the plate 23.
  • the conductor 24 Extending beyond the plate 23 to a place lie of utilization of a hydraulic fluid, as for example to a propeller feathering mechanism, the conductor 24 has a selectively operable pump 25 therein and it will be under,- stood that upon operation of the pump 25 liquid is drawn from the chamber 21 and directed under pressure through the conductor 24 to aplace of use.
  • the adapter plate 23 provides a mounting for a valve unit 26.
  • the latter may be a valve as shown in F. E. Carroll, Ir., Patent No. 2,745,424, issued May :15, 1956, since it operates to the same end and purpose in controlling oil flow to and from the storage tank.
  • oil returning from the engine enters the valve unit 26 by way of an inlet opening 27 and is directed alternatively to ducts .28 and 29 extending through the plate 23 into the interior of the storagev tank.
  • vDuct 28 opens as shown through the conical bottom 18 of the outer shell 14 of the hopper assembly. Oil admitted to the hopper assembly through duct 28, therefore, enters the space 21 in the bottom of the outer shell 14 and rises through annular passage 15 to the top of the hopper.
  • duct 31 which extends downwardly through the space 21 and through the conical bottom 18 of the outer shell and through the adapter 23 to the valve unit 26 where it is discharged by way of an opening 32 for passage to-the engine.
  • the duct 29 rises as a stand pipe within the tank 10 outside the hopper assembly. It terminates atv its upper end above the normal oil level and so provides for return flow into the tank proper outside the hopper assembly.
  • Theducts 28 and 29 haverespective check valves 33 and 34 therein preventing, back-flow from the hopper and from the tank to the valve 26 by way of these ducts.
  • a further duct 35 continuously communicates the lower part of the tank 10 with the valve unit 26 and outlet opening 32 therein.
  • oil returning from the system is placed under pressure by the engine scavenge pumps, and, subject to temperature control, is directed either through the duct 28 or through the duct 29 or through both thereof.
  • the oil entering duct 28 is directed as described to the inner shell 13 of the hopper assembly, and, in flowing through the annular path 15, tends to raise the temperature of shell 14 with a consequent warming effect upon the oil in the tank 10 in contact with the exterior of the shell.
  • the oil directed through duct 29 is discharged into the upper part of the tank 18.
  • duct 35 supplies make up oil from the tank to replace that lost in the circulating system.
  • duct 35 serves as the main return means to the valve 26 and the engine.
  • a hopper adapted to be vertically positioned in said tank 'to provide a 'flowpath'for heated oil in 'heat exchange relationtwith a main body of oil in said tank, said hopper including closely spaced concentric cylindricalinner and outersliells' "defining'an annular path for flow of oil therebetween' and being in interior communication with one another at theirupper ends, each of said shells having a conical bottom and 'said conical bottoms of said inner and outer shells being spaced apart tofdefine a relatively deep space at thebottom of the hopper communicating at its upper periphery with said annular path, the conical bottom of said inner shell being provided with a discharge; connection communicating the interior of said inner 'shell and extending through said'deepi space and the bottorn of said outer shell to the exterior of said 7 r hopper, and the .bottomofsaid outer 'shell' being formed f with .separate inletand outlet connections, the latter .pro-
  • said inner shell having an opening 7 intermediate its top-and'bottoin'and' above-said deep v V ited' 'flow to said space' i om'the interior of said inner shell.
  • a storage tank of an to provide a flow path for heated oil in heat exchange relation withra main body of oil in' said tank said hopper comprising closely spaced nested inner and outer 'shells defining a narrow path for flow of oil therebetween, said outer shell being provided near its bottom with an inlet I connection communicating with said narrow path and W said inner shell being provided near its bottom with a discharge connection extending through said outer shell to the exterior ofsaidhopper, the upper endof 'said outer shell terminating at a point above saidinner shell, whereby oil flowing through said inlet connection'and said nar row path can flow overrthe upper periphery :of said inner shell into the interior of s aid in'nershell, said outer shell being further provided with anoutlet connection for selective use of the space between said shells as a reser ⁇ voir of hydraulic fluid, and an opening in said inner shell intermediate its top' and bottom whereby said reservoir may be supplied to a limitedextent from the interiorof sai'dzin'ner shell.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)

Description

July 5, 1960 P. R. HUGHES EIAL 2,943,841
STORAGE TANK FOR LIQUID cmcuuams SYSTEM Filed May 6. 1958 n .3 x 0 A Y 2% w m m W w e A 5 Z STORAGE TANK FOR LIQUID 'CIRCULATING SYSTEM Filed May 6, 1958, Ser. No. 733,347
2 Claims. (Cl. 257-195) This invention relates to systems circulating a congealable liquid, and particularly to a storage tank therein providing a reservoir whereby a portion of the circulating liquid is available for use as a hydraulic fluid.
An object of the invention is to adapt a known storage tank of the prior art, reference being had in particular to the storage tank disclosed in Patent No. 2,733,050 issued January 31, 1956, to Harry T. Booth, to incorporate therein a reservoir as described.
Another object of the invention is to provide a reser voir as described occupying a relatively small part of the storage tank 'but so situated in the tank as to insure an ample supply of hydraulic fluid both for repeated withdrawals, as for example in. a repeated exercising of a propeller feathering mechanism, and for emergency use, it being contemplatedthat an adequate supply of liquid will remain in the reservoir for emergency use even though the total'supply ofliquid in the circulating system is seriously depleted.
Other objects and structural details of the invention will appear from the following description when read in connection with the accompanying drawing, which is a view, partly in diagram, of a storage tank in accordance with the illustrated embodiment of the invention.
Referring to the drawing, the storage tank thereof is one found in the engine lubricant circulating systems of aircraft and functions to hold a supply of replacement lubricant or oil while a portion of the lubricant continuously is circulated to and from the engine and through a hopper device installed within the tank.
As shown, a storage tank for lubricating oil is seen to comprise an outer shell holding the main body 11 of stored lubricant. Received in the outer shell, in spaced relation to the walls thereof is a hopper assembly 12 comprising concentric, cylindrical inner and outer shells 13 and 14 spaced apart to define therebetween an annular space 15. The upper end or top of the outer shell 14 extends above the corresponding end of the inner shell 13 and may be closed by a cap 16, with restricted communication between the upper end of the outer shell 14 and the interior of the tank 10 proper being provided by small diameter openings 17 in the shell. The openings 17 provide for overflow from the hopper system into the tank and may serve also to obtain a pressurizing of the hopper system in a manner and for purposes which it is unnecessary here to consider.
The outer shell 14 has a conical bottom portion 18. The inner shell 13 has a similar bottom portion 19 which is, however, in non-parallel relation to the bottom 18 and in relatively widely spaced relation thereto in such manner as to define in the bottom of the outer shell 14 a relatively deep chamber 21 communicating at its upper periphery with the annular passage 15. In the bottom of the tank 10, beneath the hopper assembly 12, is an opening 22 closed by an adapter plate 23. An outlet conductor 24 communicates at, its one end with the chamber 21 and extends at its other end to and through the plate 23. Extending beyond the plate 23 to a place lie of utilization of a hydraulic fluid, as for example to a propeller feathering mechanism, the conductor 24 has a selectively operable pump 25 therein and it will be under,- stood that upon operation of the pump 25 liquid is drawn from the chamber 21 and directed under pressure through the conductor 24 to aplace of use.
The adapter plate 23 provides a mounting for a valve unit 26. The latter may be a valve as shown in F. E. Carroll, Ir., Patent No. 2,745,424, issued May :15, 1956, since it operates to the same end and purpose in controlling oil flow to and from the storage tank. Thus, oil returning from the engine enters the valve unit 26 by way of an inlet opening 27 and is directed alternatively to ducts .28 and 29 extending through the plate 23 into the interior of the storagev tank. vDuct 28 opens as shown through the conical bottom 18 of the outer shell 14 of the hopper assembly. Oil admitted to the hopper assembly through duct 28, therefore, enters the space 21 in the bottom of the outer shell 14 and rises through annular passage 15 to the top of the hopper. assembly where it spills over into inner shell .13 and descends to the bottom thereof. At the bottom of the inner shell 13 is a duct 31 which extends downwardly through the space 21 and through the conical bottom 18 of the outer shell and through the adapter 23 to the valve unit 26 where it is discharged by way of an opening 32 for passage to-the engine. The duct 29 rises as a stand pipe within the tank 10 outside the hopper assembly. It terminates atv its upper end above the normal oil level and so provides for return flow into the tank proper outside the hopper assembly. Theducts 28 and 29 haverespective check valves 33 and 34 therein preventing, back-flow from the hopper and from the tank to the valve 26 by way of these ducts. A further duct 35 continuously communicates the lower part of the tank 10 with the valve unit 26 and outlet opening 32 therein.
In the operation of the system, oil returning from the system is placed under pressure by the engine scavenge pumps, and, subject to temperature control, is directed either through the duct 28 or through the duct 29 or through both thereof. The oil entering duct 28 is directed as described to the inner shell 13 of the hopper assembly, and, in flowing through the annular path 15, tends to raise the temperature of shell 14 with a consequent warming effect upon the oil in the tank 10 in contact with the exterior of the shell. Descending within the shell 13, the oil leaves the hopper assembly by way of conductor 31 and is returned to the engine by way of valve 26 and opening 32 therein. The oil directed through duct 29 is discharged into the upper part of the tank 18.
When the principal flow is by way of duct 28 and the a hopper system the duct 35 supplies make up oil from the tank to replace that lost in the circulating system. When the principal flow is by way of duct 29, duct 35 serves as the main return means to the valve 26 and the engine.
The construction and arrangement of parts accordingly is one which finds the space 21 normally filled with oil, and it will be understood that the size of the space 21 is determined to provide suflicient fluid for at least one emergency operation of the system to which outlet conductor 24 leads. In this regard, there is located in the inner shell 13, intermediate the ends thereof, an opening 36 communicating annular path 15 with the interior of inner shell 13. According to the concept of use and location of the opening 36 there is made available thereby the whole of the space above such opening and within the shell 13 as a source of oil to replenish the space 21 should the liquid be drawn out of this space by an actuation of the pump 25. Thus, a repeated exercising of the pump 25, as might be done in training or test work, will not exhaust the space 21, the liquid used being replaced by other liquid drawn from the inner shell 13 space providing for 'and flowingdo wnward through the opening36 into the 7' space 21. Further in accordance with such location, howevergthe oil in the lower part of the inner shell 13, beneath'the opening 36, cannot;be drawn or]? by actuation,
' 'j'of the'pumpj25 so that'thehopper system-cannot be evacuated by egrcessive use of the pump 25. Similarly a seriously depleted hopper system cannot drain the liquid 7 from space 2 1-since the opening' 36 lies' above'such space.
An amount 'of'liquid in the space 21 always'will remain,
therefore, suflicient for an operationof the hydraulic actu ating system irrespective of the condition of the hopper system.- I V I V i 7 What is claimed is: r
' '1-i In a storage tank of an enginelubrication system,"
a hopper adapted to be vertically positioned in said tank 'to provide a 'flowpath'for heated oil in 'heat exchange relationtwith a main body of oil in said tank, said hopper including closely spaced concentric cylindricalinner and outersliells' "defining'an annular path for flow of oil therebetween' and being in interior communication with one another at theirupper ends, each of said shells having a conical bottom and 'said conical bottoms of said inner and outer shells being spaced apart tofdefine a relatively deep space at thebottom of the hopper communicating at its upper periphery with said annular path, the conical bottom of said inner shell being provided with a discharge; connection communicating the interior of said inner 'shell and extending through said'deepi space and the bottorn of said outer shell to the exterior of said 7 r hopper, and the .bottomofsaid outer 'shell' being formed f with .separate inletand outlet connections, the latter .pro-
viding forselective use of'said deep space as a reservoir of hydraulic fluid, said inner shell having an opening 7 intermediate its top-and'bottoin'and' above-said deep v V ited' 'flow to said space' i om'the interior of said inner shell. i 1 r "2,943,841 h V V a V I :1
2. In a storage tank of an to provide a flow path for heated oil in heat exchange relation withra main body of oil in' said tank, said hopper comprising closely spaced nested inner and outer 'shells defining a narrow path for flow of oil therebetween, said outer shell being provided near its bottom with an inlet I connection communicating with said narrow path and W said inner shell being provided near its bottom with a discharge connection extending through said outer shell to the exterior ofsaidhopper, the upper endof 'said outer shell terminating at a point above saidinner shell, whereby oil flowing through said inlet connection'and said nar row path can flow overrthe upper periphery :of said inner shell into the interior of s aid in'nershell, said outer shell being further provided with anoutlet connection for selective use of the space between said shells as a reser} voir of hydraulic fluid, and an opening in said inner shell intermediate its top' and bottom whereby said reservoir may be supplied to a limitedextent from the interiorof sai'dzin'ner shell. 8 1
, References'iCited in the fileof this patent 7' 7 LUNlT ED STATES PATENTS 1 1,845,608 Harnett Mar: 1,21932 engine lubrication system, a hopper adapted to be vertically'positioned in said tank I
US733347A 1958-05-06 1958-05-06 Storage tank for liquid circulating system Expired - Lifetime US2943841A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3229445A (en) * 1961-06-21 1966-01-18 Automatic Process Control Inc Method and apparatus for continuously degassing a liquid
US4363214A (en) * 1980-07-07 1982-12-14 Kiser Robert W Turbo-lubrication system

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1847608A (en) * 1929-02-08 1932-03-01 Buckeye Blower Company Radiator
US2117337A (en) * 1934-11-03 1938-05-17 Lobl Karel Evaporator
US2435359A (en) * 1945-10-19 1948-02-03 United Aircraft Prod Oil tank for lubricating systems
US2584877A (en) * 1945-04-30 1952-02-05 United Aircraft Prod Oil tank and system
FR1010282A (en) * 1950-02-03 1952-06-09 Improvements to heat exchangers
US2733050A (en) * 1956-01-31 Reservoir for congealable liquids
US2767732A (en) * 1955-02-03 1956-10-23 Infilco Inc Float control device
US2840068A (en) * 1956-12-20 1958-06-24 United Aircraft Prod Oil tank with pressurized hopper

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2733050A (en) * 1956-01-31 Reservoir for congealable liquids
US1847608A (en) * 1929-02-08 1932-03-01 Buckeye Blower Company Radiator
US2117337A (en) * 1934-11-03 1938-05-17 Lobl Karel Evaporator
US2584877A (en) * 1945-04-30 1952-02-05 United Aircraft Prod Oil tank and system
US2435359A (en) * 1945-10-19 1948-02-03 United Aircraft Prod Oil tank for lubricating systems
FR1010282A (en) * 1950-02-03 1952-06-09 Improvements to heat exchangers
US2767732A (en) * 1955-02-03 1956-10-23 Infilco Inc Float control device
US2840068A (en) * 1956-12-20 1958-06-24 United Aircraft Prod Oil tank with pressurized hopper

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3229445A (en) * 1961-06-21 1966-01-18 Automatic Process Control Inc Method and apparatus for continuously degassing a liquid
US4363214A (en) * 1980-07-07 1982-12-14 Kiser Robert W Turbo-lubrication system

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