US724675A - Fluid-conducting pipe. - Google Patents

Fluid-conducting pipe. Download PDF

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Publication number
US724675A
US724675A US12151402A US1902121514A US724675A US 724675 A US724675 A US 724675A US 12151402 A US12151402 A US 12151402A US 1902121514 A US1902121514 A US 1902121514A US 724675 A US724675 A US 724675A
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United States
Prior art keywords
sections
section
casing
pipe
conduit
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Expired - Lifetime
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US12151402A
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Rudolph J Decker
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WILLIAM M FERRY
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WILLIAM M FERRY
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Priority to US12151402A priority Critical patent/US724675A/en
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Publication of US724675A publication Critical patent/US724675A/en
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Expired - Lifetime legal-status Critical Current

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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
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L39/00Joints or fittings for double-walled or multi-channel pipes or pipe assemblies
    • F16L39/005Joints or fittings for double-walled or multi-channel pipes or pipe assemblies for concentric pipes

Definitions

  • the end walls are carried by the tube members 2 'of' ythe section, as are also the perforated lianges 8. It will also be observed that the bosses 10 are integral with the inner tube 2 and the openings into the annular chamber 7, extending out iiushwith the end faces ci' the s'Scn tion.
  • the openings 5 into and from the annular chamber 7 are circular in form' and are adapted to receive the double tapered connecting-nipples 11. Under some circumstances it is desirable to thus unite the chambers.
  • thc pipe or conduit 2 may be used as a Ventilating-pipe to convey foul. air from an apartment, and cooling-Water may be caused to circulate through the connected chambers 7 in order to reduce the i temperature of the air passing through the pipe and induce a strong ilow tlierein, or the pine 2 may be usedto convey steam from a generating,r plant to a heating system or engine located a long distance away from the generatipg plant, and the connected chambers in such cases may be arranged to receive steam. or a heating medium that operates to maintain the temperature of the steam being conveyed through the pipe 2.
  • Other instances of the use of. my invention might here be cited, but it is not thought necessary.
  • a conduit for tiuids formed of sections that are duplicates of each other, each section having au interior tube'member, a surrounding casing'member forminga chamber outside of the said tube member and end walls for the chamber, integral with one of the said section members, there being openings into the chamn ber for thepassage of a circulating medium,
  • Suitable packing 6 is arranged between whereby it may beconnected with correspond'- ing sections, substantially as set iorth.
  • each section having a main inj terior pipe, a surrounding casing inclosing an annular chamber about the Vpipe, and -end walls for the annular chamber through which are formed openings arranged to register with corresponding openings in adjacent sections whereby the chambers of the adjacent sec tions are connected, and th... sections being 1 also provided with perforated flanges Whereby they may be united by bolts, substantially as set forth.
  • a conduit for iiuids formed of independent sections that are duplicates of each other
  • each section having a main conduit or pipe
  • a conduit for uids formed of sections that are duplicates of each other, each section comprising an inner tube member 2, a 'jacket 3 surrounding the tube and inclosing a chamber about the same, end walls for the cham'- ber formed integral with one of the said section members and connected with the other by a screw-threaded joint, such end wall being provided with apertures 5, and perforated flanges or lugs Sarranged outside of thecas ing to receive the connecting-bolts 9, substantially as set forth.

Description

` PATBNTEB APR, 7, i902' Ja. J. maman.
Pum; ,GQNDUGTIG PIPE. APPLIUATION FILED UG. 29, 1902-.
N0 iMGIADIH..
f WJTNESSES.- 77 @Him The features thus far described are com mon to the different forms of my invention; but in other respects they diier one from the other. Thus in the form of invention illus- 'trated in Figs. l, 2, and 3 the casing is experforated lugs or danges S, through' which'v pass the bolts 9, by which the sections are connected together, such flanges orlugs being in this instance carried by the casing member the ends of the sections, the packing being so disposed as io leave free openings between adjacent ends'of the pipes 2 and the openings '5 into the annular chambers 7. i
In the form of my invention illustrated in,I
Figs'. 4, 5, and 6 the end walls 4' of the 'casing 8 are set back somewhat from the ends of the section, and the openings-5 into and from heannular chamber 7 are formed in bosses 1.0, disposednpon the out-eide of the tube 2 and between the end Walis 4 of the casi-ug andthe perforated fianges 8 of the section.
in this embodiment of my invention the end walls are carried by the tube members 2 'of' ythe section, as are also the perforated lianges 8. It will also be observed that the bosses 10 are integral with the inner tube 2 and the openings into the annular chamber 7, extending out iiushwith the end faces ci' the s'Scn tion.
The form of my invention -illustrated in Fig. 7 is quite similar to that shown in Figs.
l, 2,and 3. It differs, however, in that the openings 5 into and from the annular chamber 7 are circular in form' and are adapted to receive the double tapered connecting-nipples 11. Under some circumstances it is desirable to thus unite the chambers.
It will be obsered that in each form of my invention the apertures for the connecting- -bolts 9, by which the sections are united, are
situated outside of the casing 7, thus leaving the connecting-bolts entirely exposed and -easily accessible, so that a section of the conduit maybe easily removed and another put in its place should circumstances require it.
The uses to which my invention may be put are many. For/example, thc pipe or conduit 2 may be used as a Ventilating-pipe to convey foul. air from an apartment, and cooling-Water may be caused to circulate through the connected chambers 7 in order to reduce the i temperature of the air passing through the pipe and induce a strong ilow tlierein, or the pine 2 may be usedto convey steam from a generating,r plant to a heating system or engine located a long distance away from the generatipg plant, and the connected chambers in such cases may be arranged to receive steam. or a heating medium that operates to maintain the temperature of the steam being conveyed through the pipe 2. Other instances of the use of. my invention might here be cited, but it is not thought necessary.
Having -described. my invention, what l I claim, and desire to secure by Letters Patent,
ll. A conduit for tiuids formed of sections that are duplicates of each other, each section having au interior tube'member, a surrounding casing'member forminga chamber outside of the said tube member and end walls for the chamber, integral with one of the said section members, there being openings into the chamn ber for thepassage of a circulating medium,
= and each section being provided with means 3. Suitable packing 6 is arranged between whereby it may beconnected with correspond'- ing sections, substantially as set iorth.
2. A conduit for iuids formed of independ;
ent sections, each section having a main inj terior pipe, a surrounding casing inclosing an annular chamber about the Vpipe, and -end walls for the annular chamber through which are formed openings arranged to register with corresponding openings in adjacent sections whereby the chambers of the adjacent sec tions are connected, and th... sections being 1 also provided with perforated flanges Whereby they may be united by bolts, substantially as set forth.
3. A conduit for iiuids formed of independent sections that are duplicates of each other,
each section having a main conduit or pipe,
a casing inclosiug'a chamber about the pipe and end walls for the chamber, the chambers of the conduit being connected in series, and
y each section being provided with perforated ico anges by which they may be bolted together,
such auges beingfsituated outside the casing, substantially as set forth. v
4. AA conduit for fluids formed of sections each having an interior pipe or tube member,
IXO
and a surrounding jacket inclosing a chamber about the tube, the chambers of the sections being connected in series, and each casing being united with the tube member rigidly, whereby relative longitudinal movements of the casing and tube members are prevented, substantially as set forth.
5. A conduit for uids formed of sections that are duplicates of each other, each section comprising an inner tube member 2, a 'jacket 3 surrounding the tube and inclosing a chamber about the same, end walls for the cham'- ber formed integral with one of the said section members and connected with the other by a screw-threaded joint, such end wall being provided with apertures 5, and perforated flanges or lugs Sarranged outside of thecas ing to receive the connecting-bolts 9, substantially as set forth.
' RUDOLPH J, Decima.
YVitncsses:
J. S. BAKKER, GEo..B; Prr'rs.
US12151402A 1902-08-29 1902-08-29 Fluid-conducting pipe. Expired - Lifetime US724675A (en)

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US12151402A US724675A (en) 1902-08-29 1902-08-29 Fluid-conducting pipe.

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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2753893A (en) * 1952-02-08 1956-07-10 Glascote Products Inc Dip tube for tanks and the like
US3082795A (en) * 1960-05-10 1963-03-26 Chester M Heller Torsional pipe couplings
US3167204A (en) * 1961-05-26 1965-01-26 Jr Thomas P M Rouse Pressure vessels
US3943618A (en) * 1974-12-30 1976-03-16 Atlantic Richfield Company Method of assembly of a dual-walled pipe
US4095433A (en) * 1975-10-09 1978-06-20 Kubota, Ltd. Tunnel support structure using built-up pipe support set, and unit pipe support member therefor
US4111466A (en) * 1976-02-02 1978-09-05 Deregibus Alfio D A Collapsible tanker hose coupling
US5088774A (en) * 1990-05-07 1992-02-18 Tylan General, Inc. Coupling for interconnection of coaxial tubing
US5277455A (en) * 1992-09-25 1994-01-11 Performance Plastics Products, Inc. Plastic lined dual containment piping system
US6076519A (en) * 1993-12-14 2000-06-20 Ethex International, Inc. Passive inspiratory nebulizer system
US20040026922A1 (en) * 2002-08-09 2004-02-12 Carns James A. Shrouded fluid-conducting apparatus
US20060192053A1 (en) * 2005-02-25 2006-08-31 Crangle Gage B Systems and methods for controlling flexible communication links used for aircraft refueling
US20060278760A1 (en) * 2005-06-09 2006-12-14 The Boeing Company Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems
US20060278761A1 (en) * 2005-06-10 2006-12-14 Cutler Theron L Aerial refueling system
US20060278759A1 (en) * 2005-06-09 2006-12-14 The Boeing Company System and methods for distributing loads from fluid conduits, including aircraft fuel conduits
US20060278017A1 (en) * 2005-06-10 2006-12-14 The Boeing Company Shrouded body flow meter assembly
US20060284019A1 (en) * 2005-06-20 2006-12-21 Takacs John F Controllable refueling drogues and associated systems and methods
US20060284018A1 (en) * 2005-06-07 2006-12-21 Carns James A Valves for annular conduits including aircraft fuel conduits and associated systems and methods
US20070051406A1 (en) * 2002-08-09 2007-03-08 Carns James A Shrouded valve apparatus and related methods
US20070069071A1 (en) * 2005-06-08 2007-03-29 The Boeing Company Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft
US20070102583A1 (en) * 2005-10-26 2007-05-10 Cutler Theron L Systems and methods for reducing surge loads in hose assemblies, including aircraft refueling hose assemblies
US20070215753A1 (en) * 2005-09-01 2007-09-20 Schuster John H Systems and methods for controlling an aerial refueling device
US20080011368A1 (en) * 2006-04-25 2008-01-17 Singh Vinay K Inline swivel connection for multi-lumen tubing
US7469863B1 (en) 2005-03-24 2008-12-30 The Boeing Company Systems and methods for automatically and semiautomatically controlling aircraft refueling
US7581700B2 (en) 2005-06-09 2009-09-01 The Boeing Company Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods
EP3246609A1 (en) * 2016-05-20 2017-11-22 Airbus Operations GmbH Shrouded pipe
US10520116B2 (en) 2016-05-20 2019-12-31 Airbus Operations Gmbh Shrouded pipe
US10905836B2 (en) 2015-04-02 2021-02-02 Hill-Rom Services Pte. Ltd. Manifold for respiratory device

Cited By (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2753893A (en) * 1952-02-08 1956-07-10 Glascote Products Inc Dip tube for tanks and the like
US3082795A (en) * 1960-05-10 1963-03-26 Chester M Heller Torsional pipe couplings
US3167204A (en) * 1961-05-26 1965-01-26 Jr Thomas P M Rouse Pressure vessels
US3943618A (en) * 1974-12-30 1976-03-16 Atlantic Richfield Company Method of assembly of a dual-walled pipe
US4095433A (en) * 1975-10-09 1978-06-20 Kubota, Ltd. Tunnel support structure using built-up pipe support set, and unit pipe support member therefor
US4111466A (en) * 1976-02-02 1978-09-05 Deregibus Alfio D A Collapsible tanker hose coupling
US5088774A (en) * 1990-05-07 1992-02-18 Tylan General, Inc. Coupling for interconnection of coaxial tubing
US5277455A (en) * 1992-09-25 1994-01-11 Performance Plastics Products, Inc. Plastic lined dual containment piping system
US6076519A (en) * 1993-12-14 2000-06-20 Ethex International, Inc. Passive inspiratory nebulizer system
US6848720B2 (en) * 2002-08-09 2005-02-01 The Boeing Company Shrouded fluid-conducting apparatus
US20050120534A1 (en) * 2002-08-09 2005-06-09 Carns James A. Shrouded fluid-conducting apparatus
US20040026922A1 (en) * 2002-08-09 2004-02-12 Carns James A. Shrouded fluid-conducting apparatus
US7493911B2 (en) 2002-08-09 2009-02-24 The Boeing Company Shrouded valve apparatus and related methods
US20070051406A1 (en) * 2002-08-09 2007-03-08 Carns James A Shrouded valve apparatus and related methods
US20060192053A1 (en) * 2005-02-25 2006-08-31 Crangle Gage B Systems and methods for controlling flexible communication links used for aircraft refueling
US7309047B2 (en) 2005-02-25 2007-12-18 The Boeing Company Systems and methods for controlling flexible communication links used for aircraft refueling
US7469863B1 (en) 2005-03-24 2008-12-30 The Boeing Company Systems and methods for automatically and semiautomatically controlling aircraft refueling
US7213787B2 (en) 2005-06-07 2007-05-08 The Boeing Company Valves for annular conduits including aircraft fuel conduits and associated systems and methods
US20060284018A1 (en) * 2005-06-07 2006-12-21 Carns James A Valves for annular conduits including aircraft fuel conduits and associated systems and methods
US7637458B2 (en) 2005-06-08 2009-12-29 The Boeing Company Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft
US20070069071A1 (en) * 2005-06-08 2007-03-29 The Boeing Company Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft
US7581700B2 (en) 2005-06-09 2009-09-01 The Boeing Company Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods
US20060278759A1 (en) * 2005-06-09 2006-12-14 The Boeing Company System and methods for distributing loads from fluid conduits, including aircraft fuel conduits
US8356842B2 (en) 2005-06-09 2013-01-22 Carns James A Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems
US7946038B2 (en) 2005-06-09 2011-05-24 The Boeing Company Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods
US7922122B2 (en) * 2005-06-09 2011-04-12 The Boeing Company Systems and methods for distributing loads from fluid conduits, including aircraft fuel conduits
US20100024189A1 (en) * 2005-06-09 2010-02-04 The Boeing Company Systems and Methods for Distributing Loads from Fluid Conduits, Including Aircraft Fuel Conduits
US20060278760A1 (en) * 2005-06-09 2006-12-14 The Boeing Company Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems
US20090293256A1 (en) * 2005-06-09 2009-12-03 The Boeing Company Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods
US7533850B2 (en) 2005-06-09 2009-05-19 The Boeing Company Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems
US7458543B2 (en) 2005-06-10 2008-12-02 The Boeing Company Aerial refueling system
US7437952B2 (en) 2005-06-10 2008-10-21 The Boeing Company Shrouded body flow meter assembly
US20090032645A1 (en) * 2005-06-10 2009-02-05 The Boeing Company Aerial refueling system
US20060278017A1 (en) * 2005-06-10 2006-12-14 The Boeing Company Shrouded body flow meter assembly
US7665479B2 (en) 2005-06-10 2010-02-23 The Boeing Company Aerial refueling system
US20060278761A1 (en) * 2005-06-10 2006-12-14 Cutler Theron L Aerial refueling system
US20060284019A1 (en) * 2005-06-20 2006-12-21 Takacs John F Controllable refueling drogues and associated systems and methods
US20080054124A1 (en) * 2005-06-20 2008-03-06 The Boeing Company Controllable refueling drogues and associated systems and methods
US7219857B2 (en) 2005-06-20 2007-05-22 The Boeing Company Controllable refueling drogues and associated systems and methods
US7887010B2 (en) 2005-06-20 2011-02-15 The Boeing Company Controllable refueling drogues and associated systems and methods
US7472868B2 (en) 2005-09-01 2009-01-06 The Boeing Company Systems and methods for controlling an aerial refueling device
US20070215753A1 (en) * 2005-09-01 2007-09-20 Schuster John H Systems and methods for controlling an aerial refueling device
US20070102583A1 (en) * 2005-10-26 2007-05-10 Cutler Theron L Systems and methods for reducing surge loads in hose assemblies, including aircraft refueling hose assemblies
US8002313B2 (en) * 2006-04-25 2011-08-23 Kci Licensing, Inc. Inline swivel connection for multi-lumen tubing
US20080011368A1 (en) * 2006-04-25 2008-01-17 Singh Vinay K Inline swivel connection for multi-lumen tubing
US9216244B2 (en) 2006-04-25 2015-12-22 Kci Licensing, Inc. Inline swivel connection for multi-lumen tubing
US10905836B2 (en) 2015-04-02 2021-02-02 Hill-Rom Services Pte. Ltd. Manifold for respiratory device
US10905837B2 (en) 2015-04-02 2021-02-02 Hill-Rom Services Pte. Ltd. Respiratory therapy cycle control and feedback
EP3246609A1 (en) * 2016-05-20 2017-11-22 Airbus Operations GmbH Shrouded pipe
US10520116B2 (en) 2016-05-20 2019-12-31 Airbus Operations Gmbh Shrouded pipe
US11143349B2 (en) 2016-05-20 2021-10-12 Airbus Operations Gmbh Shrouded pipe

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