US778261A - Gas-engine starter. - Google Patents

Gas-engine starter. Download PDF

Info

Publication number
US778261A
US778261A US21117404A US1904211174A US778261A US 778261 A US778261 A US 778261A US 21117404 A US21117404 A US 21117404A US 1904211174 A US1904211174 A US 1904211174A US 778261 A US778261 A US 778261A
Authority
US
United States
Prior art keywords
gas
cylinder
engine
disk
threaded
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
US21117404A
Inventor
John Bruce Morrison
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 US21117404A priority Critical patent/US778261A/en
Application granted granted Critical
Publication of US778261A publication Critical patent/US778261A/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
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N13/00Starting of engines, or driving of starting apparatus by use of explosives, e.g. stored in cartridges

Definitions

  • This invention relates to new and useful improvements in starters for gasengines; and the object of the invention is to produce a simple and eiiicient means whereby the initial stroke of a piston of an engine may be started by the impact of an explosive material which is ignited in a receptacle havingcommunicationwith the combustion-chamber of the en, gine.
  • the invention consists in the provision of a starter for gas-engines comprising a shell adapted to contain an explosive material, such as powder, and which shell is, connected to and communicating with the cornbustion-chamber of an engine and having in one end of said shell a nipple adapted to receive a percussion-cap, against which a plug is adapted to be forced to explode the same, whereby the charge may be ignited and exploded for the purpose of starting the engine.
  • an explosive material such as powder
  • Figure l is a sectional view through a portion of the cylinder of au engine and of my attachment.
  • Fig. 2 is an enlarged detail sectionalzview of an explosive-tube which is attachedto the cylinder.
  • Fig. 3 is a perspective View of the parts disassembled; and
  • Fig. i is a longitudinal sectional View through a tube, showing a slight differentiation in the construction of the disk and plug.
  • A designates the'cylinder of an explosive gas-engine, which may be of any construction, and one end of the cylinder has an aperture,I vas at A', which is threaded to receive the threaded end ofthe tubular shell B, forming the cylinder of my Said shell B is adapted to contain an explosive material, such as powder, (indicated by the dotSv B',) mdfhas its outer end externally threaded to receive a unionU:
  • a disk D having a shoulder-D bf suihcient diameter to snugly t into' the Outer end of said shell B, isprovided, and said disk D has a central aperture adapted to receive a nipple E, and the outer face of the-'diskAD is countersunken, as shown clearly in Fig. ZAof-4 the drawings, and the nipple E has an annular .shoulder E about its ,circumference adapted.
  • The'nip'ple is centrally apertured, asat e., and
  • percussion cap e. having threaded circumference adapted to engage the threads on the inner face ofthe union C and a projecting portion F upon its ipner end adapted to contact with the cap and force the same against the end of the nipple with sufiicient force to cause the same to explode as the plug 'is screwed into the union.
  • a device for starting engines comprising a cylindrical' portion adapted to contain a starting charge of an explosive material and fastened to and communicating with the explosion-chamber of an engine, a union mounted upon the threaded end of said cylinder, an apertured disk seated against the end of said cylinder and-Within the union, a hollow nipple carried by saiddisk, and va threaded plug IOO 7o its outer end is of sufficient size to receive a.
  • a yplug F is pr0vided,- v
  • adisk having-a portion thereof fitted within said cylinder and centrally apertured, the outer face of said disk being countersunken, an apertured nipple fitted into the aperture of said disk, an-
  • a starter for gas-engines comprising a cylinder adapted to be connected to and comshoulder engaging the outer face 'of said disk, u w

Description

' lfumLNTED DB0. 27, T1964." 7
v J. B. MORRISON. v GAS ENGINE' STARTER.
. APPLIGLTION FILED JUNE 4, 1904.
a citizen of the United States, residing at Bays,
Nrrnn STATES Patented Deeember 27, 1904.
'PATENT OFFICE. i
JOHN BRUCE Moiu'nson',v or BYs, OHIO.
@As-ENGINE' STARTER.
SIPIECIIEIIGA'IITIIILTy forming' part of Letters Patent No. 778,261, dated December 27, 1904.v
Application filed June 4, i904. Serial No. 211,174. I
To all whom, Ait Hwy concern:
Be it known that I, JOHN BRUCEY MORRISON,
in the county of Wood and State of Ohio, have invented certain new and usefulImprovements in Gas-Engine Starters; andI do declare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to w-hich it appertains to make and use the same, reference being had tothe accompanying drawings, and to the letters of reference marked thereon, which form a part of this specification.
This invention relates to new and useful improvements in starters for gasengines; and the object of the invention is to produce a simple and eiiicient means whereby the initial stroke of a piston of an engine may be started by the impact of an explosive material which is ignited in a receptacle havingcommunicationwith the combustion-chamber of the en, gine.
More specifically, the invention consists in the provision of a starter for gas-engines comprising a shell adapted to contain an explosive material, such as powder, and which shell is, connected to and communicating with the cornbustion-chamber of an engine and having in one end of said shell a nipple adapted to receive a percussion-cap, against which a plug is adapted to be forced to explode the same, whereby the charge may be ignited and exploded for the purpose of starting the engine.
My invention consists, further, in various details of construction and arrangements of parts which will be hereinafter fully described and then'speciically dened in the appended claims. v
My invention is illustrated in the'accompanying drawings, in Which.-
Figure l is a sectional view through a portion of the cylinder of au engine and of my attachment. Fig. 2 is an enlarged detail sectionalzview of an explosive-tube which is attachedto the cylinder. Fig. 3 is a perspective View of the parts disassembled; and Fig. i is a longitudinal sectional View through a tube, showing a slight differentiation in the construction of the disk and plug. -f
Reference now being' had to the details of improved starter.
the drawings by letter," A designates the'cylinder of an explosive gas-engine, which may be of any construction, and one end of the cylinder has an aperture,I vas at A', which is threaded to receive the threaded end ofthe tubular shell B, forming the cylinder of my Said shell B is adapted to contain an explosive material, such as powder, (indicated by the dotSv B',) mdfhas its outer end externally threaded to receive a unionU: A disk D, having a shoulder-D bf suihcient diameter to snugly t into' the Outer end of said shell B, isprovided, and said disk D has a central aperture adapted to receive a nipple E, and the outer face of the-'diskAD is countersunken, as shown clearly in Fig. ZAof-4 the drawings, and the nipple E has an annular .shoulder E about its ,circumference adapted.
to bear against the outer face of said disk. The'nip'ple is centrally apertured, asat e., and
percussion cap e. having threaded circumference adapted to engage the threads on the inner face ofthe union C and a projecting portion F upon its ipner end adapted to contact with the cap and force the same against the end of the nipple with sufiicient force to cause the same to explode as the plug 'is screwed into the union.
In Fig.' 4 vof the drawings I have shown av slight moditicationof my invention, in which vthe disk D2 has its outer face'iiat instead of cap.
Having thus fully described my invention, what I claim as new, and desire to secure by Letters Patent, is-
l. A device for starting engines comprising a cylindrical' portion adapted to contain a starting charge of an explosive material and fastened to and communicating with the explosion-chamber of an engine, a union mounted upon the threaded end of said cylinder, an apertured disk seated against the end of said cylinder and-Within the union, a hollow nipple carried by saiddisk, and va threaded plug IOO 7o its outer end is of sufficient size to receive a.
A yplug F is pr0vided,- v
' chamber of a gas-engine, adisk having-a portion thereof fitted within said cylinder and centrally apertured, the outer face of said disk being countersunken, an apertured nipple fitted into the aperture of said disk, an-
' internally-threaded union tted to the circumference of the cylinder, and a threaded plug fitted to the threads of said union and adapted to bear with suiiicient force against a'cap designed to be held upon said nipple, to cause the sameto explode, whereby the charge within said cylinder may be ignited, as set forth.
3. A starter for gas-engines comprising a cylinder adapted to be connected to and comshoulder engaging the outer face 'of said disk, u w
a union fitted to the threaded circumference of the cylinder, a plug adapted to screw into said union and to -bear with suioient force against a percussion-cap uponsaid nipple to 'cause the same to explode, whereby the explosive material within said cylinder may be ignited, as set forth.
In testimony .whereof I hereuntonafiix my signature in presence of two witnesses.
JOHN BRUCE MORRISON.
Witnesses:
J. A. BEALS, J. W. CHAMBERS.
US21117404A 1904-06-04 1904-06-04 Gas-engine starter. Expired - Lifetime US778261A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US21117404A US778261A (en) 1904-06-04 1904-06-04 Gas-engine starter.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US21117404A US778261A (en) 1904-06-04 1904-06-04 Gas-engine starter.

Publications (1)

Publication Number Publication Date
US778261A true US778261A (en) 1904-12-27

Family

ID=2846747

Family Applications (1)

Application Number Title Priority Date Filing Date
US21117404A Expired - Lifetime US778261A (en) 1904-06-04 1904-06-04 Gas-engine starter.

Country Status (1)

Country Link
US (1) US778261A (en)

Similar Documents

Publication Publication Date Title
US4412420A (en) Explosive actuated pin puller
US1360602A (en) Projectile
US778261A (en) Gas-engine starter.
US1417475A (en) Shell
US320393A (en) Bomb-lance
US1311521A (en) Andrew johusou
US2833216A (en) Jet-propelled missile
US1167555A (en) Power-storage device.
US1223188A (en) Spark-plug.
US803078A (en) Gasolene-engine.
US1502400A (en) Inflammable shell
US1500464A (en) Internal-combustion engine
US3063374A (en) Electro-mechanical igniter
US1146906A (en) Engine-starting means.
US1279224A (en) Bomb.
US1172893A (en) Starting device for explosive-engines.
US417472A (en) Ignitor for gas-engines
US1080689A (en) Gas-engine starter.
US595489A (en) Gas-engine
US1076283A (en) Internal-combustion-engine tool.
US962653A (en) Starting apparatus for gasolene-engines.
US2299904A (en) Hand grenade
US753795A (en) Electric sparking igniter for explosive-engines.
US879837A (en) Explosion-engine.
US1311792A (en) driggs