[go: up one dir, main page]

US3415277A - Ullage control - Google Patents

Ullage control Download PDF

Info

Publication number
US3415277A
US3415277A US62456767A US3415277A US 3415277 A US3415277 A US 3415277A US 62456767 A US62456767 A US 62456767A US 3415277 A US3415277 A US 3415277A
Authority
US
United States
Prior art keywords
ullage
tank
housing
bellows
liquid
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
Inventor
William H Mitchell
Fishman Bernard
Charles G Sage
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.)
ATK Launch Systems LLC
Original Assignee
Thiokol 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 Thiokol Corp filed Critical Thiokol Corp
Priority to US62456767 priority Critical patent/US3415277A/en
Application granted granted Critical
Publication of US3415277A publication Critical patent/US3415277A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/605Reservoirs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0138Shape tubular
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • 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
    • Y10T137/8593Systems
    • Y10T137/86381Head-establishing standpipe or expansion chamber [e.g., surge tanks]

Definitions

  • This invention relates to fuel tanks and more particularly to means for ullage control.
  • the space between the surface of a liquid contained in a tank and the walls of the tank is referred to as ullage.
  • ullage When the ullage is large, sloshing of the liquid can occur, which in some instances, such as in the flight of rockets, is undesirable.
  • pressurized gas when utilized for expulsion of the liquid, increases the time required to attain a predetermined operational liquid flow rate. If a large pressurizing gas flow is used to reduce flow rate under high ullage conditions, the pressurizing gas flow will be too high for low ullage conditions. In the art, absence of ullage is referred to as zero ullage.
  • the present invention provides zero ullage by the action of a bellows mounted on a diaphragm which rolls to expel the liquid.
  • a liquid for example, a liquid fuel or oxidizer
  • tank 10 One end of a rolling diaphragm 12 is attached to the wall 14 of the tank, and the other end of the diaphragm is attached to a tubular housing 16, which is provided with a first end 18 and a second end 20 each having an aperture 22, 24 therein.
  • a bellows 26 is disposed inside housing 16, and inside this bellows is a spring 28 which is under compression, thereby biasing the closed end 30 of bellows 26 toward first end 18 of housing 16.
  • a gas generator 32 is centered at the bottom of tank 10. Although the burning charge 34 in the gas generator is illustrated as being a resin or plastic, other means for obtaining pressurizing gases could be employed.
  • pressurizing gas from gas generator 32 enters bellows 26 through orifice 24 in second end 20 of housing 16.
  • the pressurizing gas inside bellows 26 is at a higher pressure than the pressure of the liquid contained between the exterior of bellows 26 and the interior of housing 16, because a differential pressure is necessary to cause rolling of expulsion diaphragm 12.
  • the differential pressure across bellows 26 therefore forces liquid through orifice 22 in first end 18 into tank 10.
  • An ullage control apparatus comprising:
  • tubular housing disposed in said tank and formed with first and second ends each having an aperture therein;
  • a bellows disposed inside said housing with one end thereof fixed to said first end of said housing so that the aperture in said first end communicates with the interior of said bellows, the other end of said bellows being closed and free to move to vary the volume defined by the interior surface of said housing and the exterior surface of said bellows;
  • seal means sealingly engaging said housing and the interior surface of said tank and allowing said housing to move relative to said tank;
  • pressurizing means for moving said housing to thereby expel liquid from said tank.
  • seal means comprises a tubular rolling diaphragm bonded at one end to the interior surface rolling diaphragm bonded at one end to the interior surface of said tank and at its other end to said housing circumjacent said first end thereof.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Diaphragms And Bellows (AREA)

Description

Dec. 10, 1968 w c ET AL 3,415,277
ULLAGE CONTROL Filed March 20, 1967 INVENTQRS 5E'QNAPO FISH/WAN W/LL IAN H. MITCHELL BY CHAR/.55 6. SAGE United States Patent 3,415,277 ULLAGE CONTROL William H. Mitchell, Dover, Bernard Fishman, Fort Lee,
and Charles G. Sage, Caldwell, NJ., assignors to Thiokol Chemical Corporation, Bristol, Pa., a corporation of Delaware Filed Mar. 20, 1967, Ser. No. 624,567 3 Claims. (Cl. 137593) ABSTRACT OF THE DISCLOSURE Ullage in a tank is eliminated by means of a device having a bellows that expands or contracts to compensate for change in liquid volume. The bellows is mounted inside a housing which is movably mounted in the tank on a rolling diaphragm. Liquid is expelled from the tank when pressurizing gases from a gas generator move the housing and rolling diaphragm.
This invention relates to fuel tanks and more particularly to means for ullage control.
The space between the surface of a liquid contained in a tank and the walls of the tank is referred to as ullage. When the ullage is large, sloshing of the liquid can occur, which in some instances, such as in the flight of rockets, is undesirable. Further, when pressurized gas is utilized for expulsion of the liquid, increases the time required to attain a predetermined operational liquid flow rate. If a large pressurizing gas flow is used to reduce flow rate under high ullage conditions, the pressurizing gas flow will be too high for low ullage conditions. In the art, absence of ullage is referred to as zero ullage. The present invention provides zero ullage by the action of a bellows mounted on a diaphragm which rolls to expel the liquid.
Accordingly, it is an object of this invention to provide zero ullage in a tank containing liquid.
It is another object of this invention to provide a means by which liquid can be rapidly expelled from a tank over a wide range of operating temperatures.
The preferred embodiment of the invention will be described with reference to the accompanying drawing showing a central sectional view of the embodiment.
As illustrated in the drawing, a liquid (for example, a liquid fuel or oxidizer) is contained in tank 10. One end of a rolling diaphragm 12 is attached to the wall 14 of the tank, and the other end of the diaphragm is attached to a tubular housing 16, which is provided with a first end 18 and a second end 20 each having an aperture 22, 24 therein. A bellows 26 is disposed inside housing 16, and inside this bellows is a spring 28 which is under compression, thereby biasing the closed end 30 of bellows 26 toward first end 18 of housing 16. A gas generator 32 is centered at the bottom of tank 10. Although the burning charge 34 in the gas generator is illustrated as being a resin or plastic, other means for obtaining pressurizing gases could be employed.
During the storage of the liquid, its density and vapor pressure change with change in temperature, which tends to affect tank ullage. However, 'by selection of a spring 28 having a suitable spring constant, bellows 26 expands or contracts with changes of the liquid volume, whereby the volume defined by the interior surface of housing 16 and the exterior surface of bellows 26 is increased or de- 3,415,277 Patented Dec. 10, 1968 creased equally with the change in liquid volume, maintaining zero ullage in tank 10. When the liquid is to be expelled from the tank, gas generator 32 is fired by means not shown. Hot gases are generated by the burning of burning charge 34, rupturing a disc 36 and exerting pressure against housing 16. Diaphragm 12 rolls over itself as housing 16 moves along the tank. As liquid is expelled from tank 10, pressurizing gas from gas generator 32 enters bellows 26 through orifice 24 in second end 20 of housing 16. The pressurizing gas inside bellows 26 is at a higher pressure than the pressure of the liquid contained between the exterior of bellows 26 and the interior of housing 16, because a differential pressure is necessary to cause rolling of expulsion diaphragm 12. The differential pressure across bellows 26 therefore forces liquid through orifice 22 in first end 18 into tank 10.
Although a specific embodiment of the invention has been described and illustrated in detail, it is to be under- Stood that various changes and modifications may be made there without departing from the scope of the appended claims.
What is claimed is:
1. An ullage control apparatus comprising:
a tank for holding liquid;
a tubular housing disposed in said tank and formed with first and second ends each having an aperture therein;
a bellows disposed inside said housing with one end thereof fixed to said first end of said housing so that the aperture in said first end communicates with the interior of said bellows, the other end of said bellows being closed and free to move to vary the volume defined by the interior surface of said housing and the exterior surface of said bellows;
spring means connected to said housing and said bellows for biasing the closed end of said bellows toward said second end of said housing;
seal means sealingly engaging said housing and the interior surface of said tank and allowing said housing to move relative to said tank; and
pressurizing means for moving said housing to thereby expel liquid from said tank.
2. An ullage control as defined in claim 1 wherein said seal means comprises a tubular rolling diaphragm bonded at one end to the interior surface rolling diaphragm bonded at one end to the interior surface of said tank and at its other end to said housing circumjacent said first end thereof.
3. An ullage control as defined in claim 1 wherein said pressurizing means comprises a gas generator.
References Cited UNITED STATES PATENTS 2,902,988 9/1959 Rippingille 13830 X 3,273,577 9/1966 Moore 138-30 X 3,308,818 3/ 1967 Rutkowski 222386.5 X 3,321,112 5/1967 Cunningham et al. 222-3865 M. CARY NELSON, Primary Examiner. WILLIAM R. CLINE, Assistant Examiner.
US. Cl. X.R.
US62456767 1967-03-20 1967-03-20 Ullage control Expired - Lifetime US3415277A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US62456767 US3415277A (en) 1967-03-20 1967-03-20 Ullage control

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US62456767 US3415277A (en) 1967-03-20 1967-03-20 Ullage control

Publications (1)

Publication Number Publication Date
US3415277A true US3415277A (en) 1968-12-10

Family

ID=24502482

Family Applications (1)

Application Number Title Priority Date Filing Date
US62456767 Expired - Lifetime US3415277A (en) 1967-03-20 1967-03-20 Ullage control

Country Status (1)

Country Link
US (1) US3415277A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3648967A (en) * 1970-11-10 1972-03-14 Physics Int Co Temperature compensated hydraulic valve
US3952918A (en) * 1974-03-18 1976-04-27 Highland Laboratories Fluid dispenser apparatus
US4193513A (en) * 1977-04-19 1980-03-18 Bull Glen C Jr Non-aerosol type dispenser
US4215726A (en) * 1977-08-23 1980-08-05 Masahiro Tagami Protective unit for water pipes and a method for setting the unit
US4271989A (en) * 1979-03-27 1981-06-09 Physics International Company Micro-metering system
GB2176565A (en) * 1985-06-15 1986-12-31 Craig Hallam Horace Ernest Ric Ice expansion buffer arrangement
US5409134A (en) * 1990-01-12 1995-04-25 Hewlett-Packard Corporation Pressure-sensitive accumulator for ink-jet pens
US6012491A (en) * 1996-05-30 2000-01-11 Lucas Industries Public Limted Company Pressure accumulator
US6076558A (en) * 1996-05-30 2000-06-20 Lucas Industries Public Limited Company Electronically controllable vehicle braking system for a motor vehicle
RU2231669C2 (en) * 2002-04-25 2004-06-27 Конструкторское бюро "Полет" ГУДП ГП Производственное объединение "Полет" Dampening unit for fuel tank
US20170073208A1 (en) * 2014-05-07 2017-03-16 Khs Gmbh Filling apparatus
RU176706U1 (en) * 2017-03-07 2018-01-25 Акционерное общество "Государственный ракетный центр имени академика В.П. Макеева" DEVICE FOR CREATING PRESSURE IN THE FUEL TANK OF THE CATAPULATED APPARATUS

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2902988A (en) * 1954-10-08 1959-09-08 Clark Equipment Co Protective device for a carburetion system
US3273577A (en) * 1964-06-18 1966-09-20 Dow Chemical Co Method and apparatus for damping a pulsating flow of liquid
US3308818A (en) * 1964-07-24 1967-03-14 Eugene V Rutkowski Injection cartridge
US3321112A (en) * 1965-10-18 1967-05-23 Ara Inc Rolling cylindrical diaphragm means

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2902988A (en) * 1954-10-08 1959-09-08 Clark Equipment Co Protective device for a carburetion system
US3273577A (en) * 1964-06-18 1966-09-20 Dow Chemical Co Method and apparatus for damping a pulsating flow of liquid
US3308818A (en) * 1964-07-24 1967-03-14 Eugene V Rutkowski Injection cartridge
US3321112A (en) * 1965-10-18 1967-05-23 Ara Inc Rolling cylindrical diaphragm means

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3648967A (en) * 1970-11-10 1972-03-14 Physics Int Co Temperature compensated hydraulic valve
US3952918A (en) * 1974-03-18 1976-04-27 Highland Laboratories Fluid dispenser apparatus
US4193513A (en) * 1977-04-19 1980-03-18 Bull Glen C Jr Non-aerosol type dispenser
US4215726A (en) * 1977-08-23 1980-08-05 Masahiro Tagami Protective unit for water pipes and a method for setting the unit
US4271989A (en) * 1979-03-27 1981-06-09 Physics International Company Micro-metering system
GB2176565A (en) * 1985-06-15 1986-12-31 Craig Hallam Horace Ernest Ric Ice expansion buffer arrangement
US5409134A (en) * 1990-01-12 1995-04-25 Hewlett-Packard Corporation Pressure-sensitive accumulator for ink-jet pens
US5505339A (en) * 1990-01-12 1996-04-09 Hewlett-Packard Company Pressure-sensitive accumulator for ink-jet pens
US6012491A (en) * 1996-05-30 2000-01-11 Lucas Industries Public Limted Company Pressure accumulator
US6076558A (en) * 1996-05-30 2000-06-20 Lucas Industries Public Limited Company Electronically controllable vehicle braking system for a motor vehicle
US6209583B1 (en) 1996-05-30 2001-04-03 Lucas Industries Public Limited Company Pressure accumulator
RU2231669C2 (en) * 2002-04-25 2004-06-27 Конструкторское бюро "Полет" ГУДП ГП Производственное объединение "Полет" Dampening unit for fuel tank
US20170073208A1 (en) * 2014-05-07 2017-03-16 Khs Gmbh Filling apparatus
US10472217B2 (en) * 2014-05-07 2019-11-12 Khs Gmbh Filling apparatus
RU176706U1 (en) * 2017-03-07 2018-01-25 Акционерное общество "Государственный ракетный центр имени академика В.П. Макеева" DEVICE FOR CREATING PRESSURE IN THE FUEL TANK OF THE CATAPULATED APPARATUS

Similar Documents

Publication Publication Date Title
US3415277A (en) Ullage control
US2753801A (en) Combination liquid and solid propellent rocket
US2719583A (en) Fuel tank for aircraft
US5636513A (en) Two stage pressurization system for aerospace applications
US2979897A (en) Ullage compensators for pressurizing systems
US3091782A (en) Apparatus for flotation of articles on water
GB926780A (en) Improvements relating to heat storage devices
US2973694A (en) Buffer for automatic firearms
US3121993A (en) Rocket propellant support
US2989381A (en) Non-corrosive gas generator
US3222498A (en) Vapor generator
US2604230A (en) Liquid supply tank
US3151557A (en) Pressure actuated fuze
US2892452A (en) Load sensitive-gas operated thruster
US3194439A (en) Vortex cavity seal float
US5481869A (en) Two stage pressurization system for aerospace applications
US2955649A (en) Ullage compensators for pressurizing systems
US3286463A (en) Expulsion device
US3638905A (en) Propulsion system safety vent
US3259320A (en) Secondary injection thrust vector control system
US3149456A (en) Gas damped thruster
US4684080A (en) Pressure gas supply for a missile and the like
US3525217A (en) Self-pressurized gas generation system
US3510361A (en) Battery activator and venting system
US3508686A (en) Apparatus for positively displacing fluids