US724675A - Fluid-conducting pipe. - Google Patents
Fluid-conducting pipe. Download PDFInfo
- 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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- US
- United States
- Prior art keywords
- sections
- section
- casing
- pipe
- conduit
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L39/00—Joints or fittings for double-walled or multi-channel pipes or pipe assemblies
- F16L39/005—Joints 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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12151402A US724675A (en) | 1902-08-29 | 1902-08-29 | Fluid-conducting pipe. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12151402A US724675A (en) | 1902-08-29 | 1902-08-29 | Fluid-conducting pipe. |
Publications (1)
Publication Number | Publication Date |
---|---|
US724675A true US724675A (en) | 1903-04-07 |
Family
ID=2793186
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12151402A Expired - Lifetime US724675A (en) | 1902-08-29 | 1902-08-29 | Fluid-conducting pipe. |
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US (1) | US724675A (en) |
Cited By (27)
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 |
-
1902
- 1902-08-29 US US12151402A patent/US724675A/en not_active Expired - Lifetime
Cited By (51)
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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