US2670596A - Device for delivering under relatively diminished pressure gaseous products of combustion at high pressures of self-combustible solid fuels - Google Patents

Device for delivering under relatively diminished pressure gaseous products of combustion at high pressures of self-combustible solid fuels Download PDF

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US2670596A
US2670596A US159988A US15998850A US2670596A US 2670596 A US2670596 A US 2670596A US 159988 A US159988 A US 159988A US 15998850 A US15998850 A US 15998850A US 2670596 A US2670596 A US 2670596A
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pressure
combustion
combustion chamber
self
chamber
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US159988A
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Whitworth Edward
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Imperial Chemical Industries Ltd
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Imperial Chemical Industries Ltd
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    • 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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • 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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/38Safety devices, e.g. to prevent accidental ignition

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  • the present invention is concerned with a'new and 'improved form' of device'for enabling'pressure gases generated in a combustion'chamber by the combustion of a self-combustible solid fuel, 'especially one based 'ona single or'double 'base 'gelatinised nitrocellulose composition, to pass' into another chamber under reduced'pressure; and comprisin'g a pressure 'reducin'g'throat member guarded by 'a'filter'member adapted to r'etain parti'cles'of the'sol'd'self-c'ombustible fuel, an'd thusprevent them from choking the or'ifice of'the throat'member.
  • an emergency pressure release means through the wall of 'the 'combustion 'chamber to the exterior, consisting Iof a disc ladapted to burst at a predetermined pressure in excess of the pressure normally used for the combustion of the fuel, the external wall of the combustion chamber being modified so that a normally gas-tight seating can be provided for this safety disc. While a safety disc so positioned is eifective in preventing the disruption of the combustion chamber should an excessive pressure develop within the latter owing to any interference with the discharge of the power gases therefrom, the bursting of the safety disc and the emergence of the thereby released power gases to the exterior might constitute a certain hazard of injury and fire.
  • the present invention also includes an'assembly 'compri'sing' a combustion chamber'havingf'a threaded end portion, an ⁇ exp'ansion ⁇ chamber having a threaded end portion,v a'm'e'tal'fiange, a pressure reducing throat member, and-a 'filter member, wheren'said ohambers areadapted to be screwed together to form a seating'for'the 'circumfere'ntial portion' of va ⁇ fian ⁇ ge, 4 whe'rei'n said flange is held in said seating, is adaptedv t'o'burst at a predetermined pressure and is inthe'yicinity of the 'low-pressure end of said throat 'member, wherein said filter memberissin positin'A to gu'ard the other end of said 'throat member, wherein 'said flang'e 'is adapted'tosupportfthe 'combination of said throat
  • the filter member and the flange of metal that iS adapted to yield under the said predetermined pressure may advantageously be formed as a unit from the same piece of metal, the pressure reducing throat member being threaded to the filter member in order to locate the latter in such a position that all the gases passing the filter must pass through the throat member.
  • the flange however can otherwise be formed integral with the pressure reducing throat member, the
  • aovdsoa filter in this case being threaded on to the throat A member.
  • the throat member and the filter member can each be fianged and the throat member threaded in the filter member to form a double layered fiange member.
  • the circumferential portion of the flange of the aforesaid device can be held in the seating formed by the threading together of the combustion chamber and the expansion chamber with the assistance of annular gaskets so as to improve the efificiency of the gas-tight joint.
  • l is the external wall of the combustion chamber externally threaded as shown at IO.
  • 2 is an internally threaded end portion of the wall of a lower pressure chamber, the shoulder loading into this threaded portion and the forward end of the Wall i being accurately cut so as to provide a seating for fiange li of the filter member 3 with the aid of gasket rings 8 and 9.
  • the filter member 3 is slotted on its cylindrioal and rearward end surfaces as shown at 5 for a portion of its length, the annular fange portion 4 being formed continuously with the latter of the same steel 5.
  • the forward unsiotted portion of the wall of the filter member is internally threaded as shown at 6 and therein is screwed an externally threaded pressure reduoing throat member 'I providing a throat through which the gases from the combustion chamber pass into the other chamber at a reduced pressure. It will be understood that the pressure at which the annular ange 4 bursts is considerably below the safety limit of pressure for the wall l of the combustion chamber.
  • a combustion chamber for generating combustion gases, said combustion chamber having a gas outlet end, an expansion chamber having an inlet end for receiving gases from the outlet end of said combustion chamber, means connecting the inlet end of said expansion chamber to the outlet end of said combustion chamber, said means forming a seat about the entire periphery of the connection, a pressure reducing throat member having a high pressure end Within said combustion chamber and a low pressure end opening into said expansion chamber permitting passage of gas from said combustion chamber into said expansion chamber at reduced pressure, a filter member positioned within said combustion chamber to guard the high pressure end of said throat member and a metallic fiange positioned about said throat member, adjacent the low pressure end thereof, and held in said seating to form a fluid-tight separating wall between said combustion chamber and said expansion chamber, said fiange being adapted to burst at a predetermined pressure to permit gases within said combustion chamber to exit into said expansion chamber When said pressure is exceeded.
  • a pressure reducing device adapted for use in a combustion chamber which is so constructed that the forward end of its wall can be threaded to the rearward end of the wall of an expansion chamber and can form with said rearward end a seating for the peripheral portion of a flange, said device comprising a pressure reducing throat member having a high pressure and a low pressure end, a filter member threaded onto said high pressure end of said throat member and having an exterior flange portion, said fiange portion having a predetermined bursting pressure lower than the bursting pressure of the external wall of the cornbustion chamber and being held in said seating adjacent the low pressure end of said throat member so that the filter member filters the gases generated in the combustion chamber and passing through the said throat member into the said expansion chamber.
  • a device wherein the filter member is in the form of a cylinder having its rearward end partially closed by a slotted portion, the slots in which are continued along a portion of the cylnder wall.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Handcart (AREA)
  • Measuring Fluid Pressure (AREA)

Description

Patented Mar. 2, 1954 VDEVICE Fon DELIVERING UNDER RELA- 'rfvELYgDIMINIsnED PREssURE GAsEoUs VPnonUc'rs toti` coMBU's'rioN A'r HIGH rnEssUREs oF sELr-coMBUsTfBLE 'SOLID FUELS Edward Whitworth, VWest Knbriae,seonandasvsignor tolmperial Chemical Industries Limited,
a corporation of Great Britain Application May 4, 1950,-Serial'No.159;988
Claims priority; application Great Britain July 25, 1949 =3 Claims. 1
The present invention is concerned with a'new and 'improved form' of device'for enabling'pressure gases generated in a combustion'chamber by the combustion of a self-combustible solid fuel, 'especially one based 'ona single or'double 'base 'gelatinised nitrocellulose composition, to pass' into another chamber under reduced'pressure; and comprisin'g a pressure 'reducin'g'throat member guarded by 'a'filter'member adapted to r'etain parti'cles'of the'sol'd'self-c'ombustible fuel, an'd thusprevent them from choking the or'ifice of'the throat'member.
In generating power gases for the operation of mechanical devices or for `rocket 'propulsion by the combustion of self-combustible 'solid' fuels such as for instance gelatinised nitrocellulose compositons, it is often found that the combustion of lthe solid fuel will only take place satisfactorily at a pressure substantially higher than that at which it is desired to utilise the power gases, and for'this purpose it is customary to provide a communication from the combustion chamber into an expansion chamber'through a pressure reducing throat member,-which must be guarded against choking by fragments of the* solid fuel by a filter usually of gridlike' construction adapted to retain particles of solidffuel of -any considerable magnitudev projected againstit. It is also customary to provide an emergency pressure release means through the wall of 'the 'combustion 'chamber to the exterior, consisting Iof a disc ladapted to burst at a predetermined pressure in excess of the pressure normally used for the combustion of the fuel, the external wall of the combustion chamber being modified so that a normally gas-tight seating can be provided for this safety disc. While a safety disc so positioned is eifective in preventing the disruption of the combustion chamber should an excessive pressure develop within the latter owing to any interference with the discharge of the power gases therefrom, the bursting of the safety disc and the emergence of the thereby released power gases to the exterior might constitute a certain hazard of injury and fire.
This hazard and the inconvenience of modifying the contour of the wall of the combustion chamber, are avoided by the provision of the improved form of device according to the present invention for enabling the pressure gases generated in the combustion chamber to pass into the lower pressure chamber.
According to the present invention a pressure reducing device adapted for use in a combustion chamber which is so constructed that the forward'end of 'its walll can be' threaded to the'rear- 'ward'end of the wall of an expansion'chair'iber and can form'with said rearward end Va'seating for the'circumferential portion of -a'fiange comprises a metal 'flange adapted toburst-at=a predetermined pressure 'and'to be held in said seating, a pressure 'reducing throatl member aifd a `filter' member, wherein said' fiange is inthefvicinity of the low pressure end of 'saidi'throat member, wherein saidy filter' member is in position to guard the other end of s'aidthroat'membr, and wherein said fiange is'adapted to suiznx'irt the combinationv of said throat member and'saidffllter member.
The present invention also includes an'assembly 'compri'sing' a combustion chamber'havingf'a threaded end portion, an `exp'ansion `chamber having a threaded end portion,v a'm'e'tal'fiange, a pressure reducing throat member, and-a 'filter member, wheren'said ohambers areadapted to be screwed together to form a seating'for'the 'circumfere'ntial portion' of va `fian`ge, 4 whe'rei'n said flange is held in said seating, is adaptedv t'o'burst at a predetermined pressure and is inthe'yicinity of the 'low-pressure end of said throat 'member, wherein said filter memberissin positin'A to gu'ard the other end of said 'throat member, wherein 'said flang'e 'is adapted'tosupportfthe 'combination of said throatmember andsaid'filter member, 'and where'in said combinatio'n is positioned within said combustion chamber.
The pressure at which the fian'g'e'isfadapted to burst'is lower than'the pressure' at whi'ch*`the 'external wall of the combustion chamber 'would rupture, so that if by any chance the fiow of gases from the interior of the combustion chamber through the pressure reducing throat should become interrupted and a pressure greater than is desirable be built up in the combustion chamber, the resulting bursting of the fiange member will cause the discharge of the power gases to take place into the lower pressure chamber instead of to the atmosphere outside and the need for a bursting disc or other pressure release member to the exteror is avoided.
The filter member and the flange of metal that iS adapted to yield under the said predetermined pressure may advantageously be formed as a unit from the same piece of metal, the pressure reducing throat member being threaded to the filter member in order to locate the latter in such a position that all the gases passing the filter must pass through the throat member. The flange however can otherwise be formed integral with the pressure reducing throat member, the
aovdsoa filter in this case being threaded on to the throat A member. Alternatively the throat member and the filter member can each be fianged and the throat member threaded in the filter member to form a double layered fiange member.
If desired the circumferential portion of the flange of the aforesaid device can be held in the seating formed by the threading together of the combustion chamber and the expansion chamber with the assistance of annular gaskets so as to improve the efificiency of the gas-tight joint.
The invention will be further understood by reference to the diagrammatic drawing accompanying the specification, which represents an isometric view of a longitudinal axial section illustrating an improved device in accordance with the invention in Operating position between the forward portion of a combustion chamber and the rearward portion of a lower pressure chamber.
In the drawing l is the external wall of the combustion chamber externally threaded as shown at IO. 2 is an internally threaded end portion of the wall of a lower pressure chamber, the shoulder loading into this threaded portion and the forward end of the Wall i being accurately cut so as to provide a seating for fiange li of the filter member 3 with the aid of gasket rings 8 and 9. The filter member 3 is slotted on its cylindrioal and rearward end surfaces as shown at 5 for a portion of its length, the annular fange portion 4 being formed continuously with the latter of the same steel 5. The forward unsiotted portion of the wall of the filter member is internally threaded as shown at 6 and therein is screwed an externally threaded pressure reduoing throat member 'I providing a throat through which the gases from the combustion chamber pass into the other chamber at a reduced pressure. It will be understood that the pressure at which the annular ange 4 bursts is considerably below the safety limit of pressure for the wall l of the combustion chamber.
I claim: i 1. In combnation, a combustion chamber for generating combustion gases, said combustion chamber having a gas outlet end, an expansion chamber having an inlet end for receiving gases from the outlet end of said combustion chamber, means connecting the inlet end of said expansion chamber to the outlet end of said combustion chamber, said means forming a seat about the entire periphery of the connection, a pressure reducing throat member having a high pressure end Within said combustion chamber and a low pressure end opening into said expansion chamber permitting passage of gas from said combustion chamber into said expansion chamber at reduced pressure, a filter member positioned within said combustion chamber to guard the high pressure end of said throat member and a metallic fiange positioned about said throat member, adjacent the low pressure end thereof, and held in said seating to form a fluid-tight separating wall between said combustion chamber and said expansion chamber, said fiange being adapted to burst at a predetermined pressure to permit gases within said combustion chamber to exit into said expansion chamber When said pressure is exceeded.
2. A pressure reducing device adapted for use in a combustion chamber which is so constructed that the forward end of its wall can be threaded to the rearward end of the wall of an expansion chamber and can form with said rearward end a seating for the peripheral portion of a flange, said device comprising a pressure reducing throat member having a high pressure and a low pressure end, a filter member threaded onto said high pressure end of said throat member and having an exterior flange portion, said fiange portion having a predetermined bursting pressure lower than the bursting pressure of the external wall of the cornbustion chamber and being held in said seating adjacent the low pressure end of said throat member so that the filter member filters the gases generated in the combustion chamber and passing through the said throat member into the said expansion chamber.
3. A device according to claim 2 wherein the filter member is in the form of a cylinder having its rearward end partially closed by a slotted portion, the slots in which are continued along a portion of the cylnder wall.
EDWARD WHITWORTH.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date V 1,983,330 Welch Dec. 4, 1934 2,062,381 Tryon et al. Dec. 1, 1936 2,169,359 Jones et al. Aug. 15, 1939 2,195,925 Hoesel Apr. 2, 1940 2,342,996 Barker et al Feb. 29, 1944 2,400242 Malina et al. May 14, 1946 2,457,578 Maliphant Dec. 28, 1948
US159988A 1949-07-25 1950-05-04 Device for delivering under relatively diminished pressure gaseous products of combustion at high pressures of self-combustible solid fuels Expired - Lifetime US2670596A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2939365A (en) * 1952-05-29 1960-06-07 Bendix Aviat Corp Solid propellant engine starter apparatus
US3066484A (en) * 1961-04-10 1962-12-04 Earl H Buchanan Gas flow control rocket motor device
US3079111A (en) * 1960-09-08 1963-02-26 Lambert Engineering Company Rockets and seat ejecting apparatus
US3115004A (en) * 1952-06-30 1963-12-24 Atlantic Res Corp Catapult launcher
US3171248A (en) * 1963-02-04 1965-03-02 United Aircraft Corp Thrust cut-off method
US4155850A (en) * 1977-01-27 1979-05-22 Lucas Industries Limited Fluidic filters

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1983330A (en) * 1928-07-06 1934-12-04 Celanese Corp Manufacture of artificial filaments, threads, films, or the like
US2062381A (en) * 1935-09-14 1936-12-01 Standard Oil Dev Co Frangible shear type safety valve
US2169359A (en) * 1938-12-05 1939-08-15 Barnes & Jones Inc Orifice device
US2195925A (en) * 1939-05-26 1940-04-02 Peerless Of America Flow restrictor for refrigerant feed valves
US2342996A (en) * 1939-10-10 1944-02-29 Hubert Scott Paine Torpedo tube
US2400242A (en) * 1943-07-15 1946-05-14 Aerojet Engineering Corp Motor
US2457578A (en) * 1944-05-31 1948-12-28 Westinghouse Air Brake Co Choke fitting

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1983330A (en) * 1928-07-06 1934-12-04 Celanese Corp Manufacture of artificial filaments, threads, films, or the like
US2062381A (en) * 1935-09-14 1936-12-01 Standard Oil Dev Co Frangible shear type safety valve
US2169359A (en) * 1938-12-05 1939-08-15 Barnes & Jones Inc Orifice device
US2195925A (en) * 1939-05-26 1940-04-02 Peerless Of America Flow restrictor for refrigerant feed valves
US2342996A (en) * 1939-10-10 1944-02-29 Hubert Scott Paine Torpedo tube
US2400242A (en) * 1943-07-15 1946-05-14 Aerojet Engineering Corp Motor
US2457578A (en) * 1944-05-31 1948-12-28 Westinghouse Air Brake Co Choke fitting

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2939365A (en) * 1952-05-29 1960-06-07 Bendix Aviat Corp Solid propellant engine starter apparatus
US3115004A (en) * 1952-06-30 1963-12-24 Atlantic Res Corp Catapult launcher
US3079111A (en) * 1960-09-08 1963-02-26 Lambert Engineering Company Rockets and seat ejecting apparatus
US3066484A (en) * 1961-04-10 1962-12-04 Earl H Buchanan Gas flow control rocket motor device
US3171248A (en) * 1963-02-04 1965-03-02 United Aircraft Corp Thrust cut-off method
US4155850A (en) * 1977-01-27 1979-05-22 Lucas Industries Limited Fluidic filters

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