US735912A - Rebound-preventing device for gas-engines. - Google Patents

Rebound-preventing device for gas-engines. Download PDF

Info

Publication number
US735912A
US735912A US1901046341A US735912A US 735912 A US735912 A US 735912A US 1901046341 A US1901046341 A US 1901046341A US 735912 A US735912 A US 735912A
Authority
US
United States
Prior art keywords
gas
engines
rebound
pipe
chamber
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
Carl Schrotz
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US1901046341 priority Critical patent/US735912A/en
Application granted granted Critical
Publication of US735912A publication Critical patent/US735912A/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
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D17/00Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling
    • F02D17/04Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling rendering engines inoperative or idling, e.g. caused by abnormal conditions
    • 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
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7837Direct response valves [i.e., check valve type]
    • Y10T137/7898Pivoted valves

Definitions

  • My invention relates to an improved apparatus that is to be inserted into the pipe admitting gas to a gas-engine and whereby the t pressure in the neighboring pipes is rendered more nearly equable and the flickering of flames fed by the same is prevented
  • the apparatus consists of a return-valve preferably arranged within a chamber con-" nected with the admission-pipe.
  • Figure 1 is a longitudinal section
  • Fig. 2 a cross-see tion on line 00 y in Fig. 1, of the preferred construction of the herein-described appa- 2 5 ratus.
  • M is a gas-pipe supposed to be connected with the gas-main
  • F is the gas-engine and admitting gas to the same.
  • the air-tight chamber preferably made in the shape of a cylinder.
  • the circular flange B Within this cylindrical'chamber and closely fitting one end of the same is placed the circular flange B, with a stud S in its center.
  • the st'ud S I prefer to cut off obliquely, as shown in the drawings.
  • I further provide a flat lid or cover V, suitably hinged at one end, which partly by its own weight and partly by the action of the spring N is normally pressed against the edge of the stud S.
  • An apparatus for preventing the rebound of gas in the feed-pipe of gas-engines consisting of a chamber arranged in the feedtion with exteriorly-operabie means for regupipe, said feed-pipe, where it discharges into lating the pressure of the spring upon the lid. 10 the chamber, being formed in the shape of In testimony whereof I have affixed my an obliquely-truncated stud having its dissignature in presence of two witnesses.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sampling And Sample Adjustment (AREA)

Description

PATBNTED AUG. '11, 1903.
0. SGHROTZ. I REBOUND PREVENTING DEVIGE-FOR/GAS ENGINES.
APPLIUATIOH FILED NIB. 7. 1901.
I0 MODEL.
WITNESSES UNITED STATES Patented August 11, 1903.
PATENT OFFICE.
CARL SOHROTZ, OF COLOGNE, GERMANY.
SPECIFICATION forming part of Letters Patent No. 735,912,dated August 11, 1903.
Application filed February "7, 1901. serial No. 46,341. (No model.)
tion, such as will enable others skilled in the art to which it appertains to make and use the same.
My invention relates to an improved apparatus that is to be inserted into the pipe admitting gas to a gas-engine and whereby the t pressure in the neighboring pipes is rendered more nearly equable and the flickering of flames fed by the same is prevented The apparatus consists of a return-valve preferably arranged within a chamber con-" nected with the admission-pipe.
Of the accompanying drawings, Figure 1 is a longitudinal section, and Fig. 2 a cross-see tion on line 00 y in Fig. 1, of the preferred construction of the herein-described appa- 2 5 ratus.
The same letters of reference indicate the same parts in both figures. I
In the drawings, M is a gas-pipe supposed to be connected with the gas-main, and F is the gas-engine and admitting gas to the same.
Between both pipes is placed the air-tight chamber 0, preferably made in the shape of a cylinder. Within this cylindrical'chamber and closely fitting one end of the same is placed the circular flange B, with a stud S in its center. The st'ud S, I prefer to cut off obliquely, as shown in the drawings. I further provide a flat lid or cover V, suitably hinged at one end, which partly by its own weight and partly by the action of the spring N is normally pressed against the edge of the stud S.
In order to secure tight closing of thelid a feed-pipe supposed to be connected with The pressure of the spring N can be adjusted by means of the screw 0, which passes through the wall of the chamber C, and there- :fore remains accessible at all times. t
1 The operation of the herein-describedapparatus is as follows: \Vhen the engine begins to suck, a certain reduction of pressure in thechamber C will precede the lifting of the cover V. The'spring N ought to be adjustedin such. a Way that. the difference of pressure on both sides of the lid V is merely 6o sufficient to lift it very slightly, and thus a wider opening of the valve is only effected when the inertia of the stream of gas has accumulated. When the period of suction has attained its end and the cut-on? valve of the engine has closed,-the flow of the gas will still continue for ashort time until the increasing pressure in the chamber 0 gradually stops it. At this period, however, the lid V, being subjected to the pressure of the spring N,besides the gas-pressure in chamber G,will close before the pressure in O has increased to the full amount of the pressure in Maud will thereby prevent a rebound of the gas, which otherwise usually is effected by the congestion ofthe gas in admission-pipes to gas-engines. It will readily be seen that the action of my apparatus is regulated not only by the pressure of the spring N, but also by the capacity of the chamber 0, and since the gas inclosed in the feed-pipe F will add its cushion action to that of the gas in the chamber O the size of the latter can be varied according to the length of the feed-pipe, and where the feed-pipe is sufficiently long the chamber 0 might be omitted altogether without altering the nature of my invention. Likewise if instead of having a sufficiently long feed-pipe an elastic reservoir were pro vided in the feed-pipesuch as, for instance, the rubber bag usually employed for the purpose-the same result would be obtained.
- Having now particularly described and as-' certained the nature of my said invention and in what manner thesame is to be performed,
-I declare that what I claim is.
An apparatus for preventing the rebound of gas in the feed-pipe of gas-engines, consisting of a chamber arranged in the feedtion with exteriorly-operabie means for regupipe, said feed-pipe, where it discharges into lating the pressure of the spring upon the lid. 10 the chamber, being formed in the shape of In testimony whereof I have affixed my an obliquely-truncated stud having its dissignature in presence of two witnesses.
charge substantially in line with the How of CARL SCHROTZ.
the gas through said feed-pipe, a hinged lid Witnesses:
closing the oblique mouth of said stud, and CHARLES LE SIMPLE,
a spring bearing upon said lid, in c-oinbina- KARL SCHMITT.
US1901046341 1901-02-07 1901-02-07 Rebound-preventing device for gas-engines. Expired - Lifetime US735912A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US1901046341 US735912A (en) 1901-02-07 1901-02-07 Rebound-preventing device for gas-engines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1901046341 US735912A (en) 1901-02-07 1901-02-07 Rebound-preventing device for gas-engines.

Publications (1)

Publication Number Publication Date
US735912A true US735912A (en) 1903-08-11

Family

ID=2804420

Family Applications (1)

Application Number Title Priority Date Filing Date
US1901046341 Expired - Lifetime US735912A (en) 1901-02-07 1901-02-07 Rebound-preventing device for gas-engines.

Country Status (1)

Country Link
US (1) US735912A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419318A (en) * 1944-11-08 1947-04-22 Aro Equipment Corp Check valve
US2461351A (en) * 1945-11-21 1949-02-08 Silverman Leslie Flowmeter
US5046408A (en) * 1990-07-13 1991-09-10 John Eugenio Hooded exhaust vent
US5099886A (en) * 1988-08-31 1992-03-31 Grovag Grossventiltechnik Ag Seals for gas isolators having multiple bias springs
US5772928A (en) * 1996-06-14 1998-06-30 Holtzman; Barry L. Needle and seat valve assembly
US6050294A (en) * 1999-03-17 2000-04-18 Val-Matic Valve And Manufacturing Corp. Spring return check valve
US6393628B1 (en) * 1998-06-02 2002-05-28 James Edward Kellogg Valve assembly for swimming pool cleaning systems
US20020157717A1 (en) * 2001-04-28 2002-10-31 Myung-Jung Hong Valve assembly of a reciprocal compressor
CH709981A1 (en) * 2014-08-15 2016-02-15 Ml Tech Gmbh Valve for a compressor.
EP2995802A1 (en) * 2014-09-11 2016-03-16 United Technologies Corporation Hinged seal using wire mesh
US9540995B2 (en) 2012-03-06 2017-01-10 KATCON USA, Inc. Exhaust valve assembly
US9964223B2 (en) * 2015-07-13 2018-05-08 Hamilton Sundstrand Corporation Bleed valves for gas turbine engines

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419318A (en) * 1944-11-08 1947-04-22 Aro Equipment Corp Check valve
US2461351A (en) * 1945-11-21 1949-02-08 Silverman Leslie Flowmeter
US5099886A (en) * 1988-08-31 1992-03-31 Grovag Grossventiltechnik Ag Seals for gas isolators having multiple bias springs
US5046408A (en) * 1990-07-13 1991-09-10 John Eugenio Hooded exhaust vent
US5772928A (en) * 1996-06-14 1998-06-30 Holtzman; Barry L. Needle and seat valve assembly
US6393628B1 (en) * 1998-06-02 2002-05-28 James Edward Kellogg Valve assembly for swimming pool cleaning systems
US6050294A (en) * 1999-03-17 2000-04-18 Val-Matic Valve And Manufacturing Corp. Spring return check valve
US6823896B2 (en) * 2001-04-28 2004-11-30 Samsung Gwangju Electronics Co., Ltd. Valve assembly of a reciprocal compressor
US20020157717A1 (en) * 2001-04-28 2002-10-31 Myung-Jung Hong Valve assembly of a reciprocal compressor
US9540995B2 (en) 2012-03-06 2017-01-10 KATCON USA, Inc. Exhaust valve assembly
CH709981A1 (en) * 2014-08-15 2016-02-15 Ml Tech Gmbh Valve for a compressor.
EP2988041A1 (en) * 2014-08-15 2016-02-24 ML Tech GmbH Valve for a compressor
EP2995802A1 (en) * 2014-09-11 2016-03-16 United Technologies Corporation Hinged seal using wire mesh
US9828868B2 (en) 2014-09-11 2017-11-28 United Technologies Corporation Hinged seal using wire mesh
EP3321492A1 (en) * 2014-09-11 2018-05-16 United Technologies Corporation Hinged seal using wire mesh
US10502079B2 (en) 2014-09-11 2019-12-10 United Technologies Corporation Hinged seal using wire mesh
US9964223B2 (en) * 2015-07-13 2018-05-08 Hamilton Sundstrand Corporation Bleed valves for gas turbine engines

Similar Documents

Publication Publication Date Title
US735912A (en) Rebound-preventing device for gas-engines.
US1170050A (en) Regulating-valve.
US1373906A (en) High-pressure governor-valve
US1449998A (en) Fluid regulator
US1031943A (en) Silencer.
US879450A (en) Cigar-holder.
US1322035A (en) A cobpobatioh
US929296A (en) Acetylene-gas lamp.
US988166A (en) Carbid-lamp.
US879837A (en) Explosion-engine.
US1281337A (en) Pressure-regulator.
US625833A (en) William a
US1083899A (en) Steam-pressure-regulator valve.
US1379331A (en) Lubricating apparatus
US1117993A (en) Automatic valve.
GB189820488A (en) Apparatus for Carburetting Air.
US994562A (en) Water-heating apparatus.
US627796A (en) Acetylene-gas generator.
US1214457A (en) Automatic adjustable feeder-valve.
GB191126615A (en) Improvements in Volumetric Gas Governors.
US1042078A (en) Pressure-reducer.
US958102A (en) Gas-burner.
US1278268A (en) Lubricating means for metering devices.
US1200541A (en) Compressed-fluid starting apparatus for internal-combustion engines.
US803617A (en) Acetylene-gas apparatus.