US1743591A - Shock absorber - Google Patents

Shock absorber Download PDF

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Publication number
US1743591A
US1743591A US152003A US15200326A US1743591A US 1743591 A US1743591 A US 1743591A US 152003 A US152003 A US 152003A US 15200326 A US15200326 A US 15200326A US 1743591 A US1743591 A US 1743591A
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Prior art keywords
passage
head
casting
bore
piston
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Expired - Lifetime
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US152003A
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Adna F Blanchard
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GUY C SEATON
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GUY C SEATON
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Priority to US152003A priority Critical patent/US1743591A/en
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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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F9/00Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/10Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using liquid only; using a fluid of which the nature is immaterial
    • F16F9/14Devices with one or more members, e.g. pistons, vanes, moving to and fro in chambers and using throttling effect
    • F16F9/16Devices with one or more members, e.g. pistons, vanes, moving to and fro in chambers and using throttling effect involving only straight-line movement of the effective parts
    • F16F9/18Devices with one or more members, e.g. pistons, vanes, moving to and fro in chambers and using throttling effect involving only straight-line movement of the effective parts with a closed cylinder and a piston separating two or more working spaces therein
    • F16F9/185Bitubular units

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Actuator (AREA)

Description

Jan. 14, 1930. A. F. BLANCHARD SHOCK ABSORBER Filed Dec. 1926 INVENTOR.
ATTORNEY Patented Jan. 14, 1930 UNITED STATES PATENT OFFICE ADNA F. BLANCHARD, OF AL'IOONA, PENNSYLVANIA, ASSIGNOR TO GUY C. SEATON,
' i OF NEW YORK, N. Y.
sHocK ABSORBER Application filed December 1, 1926. Serial No. 152,003.
This invention has for an object to effect improvements in the construction of shock Serial No. 142,288. It is an important aim to improve the functioning of the device of my prior application, and also to provide a novel form of construction enabling its production with few parts and shop operations, as well as simplifying the assembly operations, and minimizing the need for special tools.
It is an important object to utilize the open end of the cylinder casting to mount a combined closure head, stuffing box and check valve mounting, enabling this assembly to be put into thecylinder as a unit, and obvlatmg the need for mounting the check valve or valves in the cylinder castingdirectly, where awkward positioning of parts would be involved. It is is also a purpose to so form the parts that in putting the head in place there will be no uncertainty or need for special care in securing registry between the ports of the by passage in the casting, and ducts in the re movable head carrying the check valves. A further important object is to enable at the same time the closure of the piston bore, and also the outer end of the large by-passage in the cylinder casting, while permitting closure of the small by-pass on the same end of the casting by an ustable screw by which the rebound check is regulated.
Additional objects, advantages and features of invention reside in the construction, arrangement and combination of parts involved in the embodiment of the invention, as may be understood from the following description, and accompanying drawings, wherein- Fig. l is a longitudinal sectional view of one form of the new construction.
Fig. 2 is a cross section thereof, on the line.
2-2 of Fig. 1.
Fig. (Sis an end View of the last mentioned modification.
There is illustrated a cylinder casting or casing 10, having a cylindrical bore 11 opening from the lower end, the other end being integrally closed and provided exteriorly with a coaxial ball 12 connected with the casting body by a reduced neck 12 Reciprocable in the bore 11 there is a piston 13 constructed as disclosed in my aforesaid application. A main by-pass passage 14- is formed in the wall of the cylinder at one side, while a two-way and smaller by-pass passage 15 is formed in the wall at the opposite side, as shown. These passagesopen into the bore 11 at the upper end in the same positions and relation as described in my prior application, and the by-pass 15 opens into the lower part of the bore 11 as 'did the similar bypass in the said prior ap- The passage 14: opens into the bore 11 near 7 the extremity of the casting, through a port 17 while the passage 15 opens into the bore a distance thereabove through the port 20. This passage 15 is continued rectilinearly in the wall of'th'e casting, downwardly past the port 20 and through the end of the casting, being interiorly threaded from the port to its outer end, and receiving a screw 18, by which the passage beyond the port is closed, and adjustable restriction of the port 20 efi'ected. The passage 14 is broadened, as well as the port 17 toprovide for movement of a substantial body of fluid therethrough under movement of the piston in one direction, while the passage 15 may be of much smaller capacity.
The lower part of the bore 11 from a distance above the port 17 to the lower end is castlng.
'33 held by screws.
finished with a planiform face.
be cut away at'all.
interiorly threaded, and screwed thereinto so as to cover the port 17, there is a head 21 having a circumscribing hexagonal flange 22 by radial pins 27 in the head. An interiorly threaded stuifing box recess 28 is formed in the outer side. of the head, a gland 29 being engaged therein, while the head is centrally bored to receive the piston rod 32 slidably.
The wall of the casting may be formed integrally with the bypass passages therein after any approved practice. For convenience I haveshown the casting as consisting of a body cylinder with a longitudinal medially recessed boss 33' at one side, and a corresponding boss 31 at the opposite side.
The recesses in the bosses are closed by plates The recess in the boss is wider than the recess in the boss 31 and .forms the passage 14, while the recess in the boss 31 may be much narrower, and forms the passage 15. The portion of the passage 15 receivingthe screw may at its lower part pass throughthe end of the boss spaced slightly from the plane of the closure plate 33.
'In Figures 5 and 6 I have shown a method of forming the by-passages adapted to die In this instance both of the pa ssages 14* and 15, corresponding to the passages 14.- and 15 have outer walls integral with the wall of the cylinder casting and they both extend rectilinearly past the ports 20 and 17 through the end of the casting, which is 21 is formed with a largerfiange than in the K first instance herein as at 351, while a hexagon 22 is formed outwardly thereof. This large flange is utilized to close the outer end of the 'passage 1-1, a gasket 35 being interposed.
After screwing of the head into place to safely seal the outer end of the passage 14:,
the opposite edge portion of the flange 34 opposite the passage 14: is cut away to expose the end of the passage 15 and permit insertion and, adjustment of the screw 18, as before described. By the use of a proper tool thisv cutting away may be done without removing the head again. The hexagon 22 is made of .a size to avoid interference with the operation of thescrew 18, and does not require to i In the operation of this device, the bore ll and all passages being filled with a proper liquid, the member 10 being connected to the frame of a motor vehicle centrally over the axle, and the rod 32 to the axlethereunder,
The head upon compression of the spring by which the frame is customarily supported on the axle, the piston 13 will move upwardly. This will cause the liquid tobe moved rapidly downward through the passage 14, and slowly downward through the passage 15. From the passage 14 the liquid passes into the groove 24 of the head 21 and thence upwardly past the valves 26 intothe borellbehind the piston. From the passage 15 the liquid escapes slowly and directly into the bore 11 behind the piston. On recoil of the vehicle spring the piston will move downwardly, but the valves 26 being seated there will be no rapid movement of liquid into the passage 14 and upwardly and only a slow escape of liquid from the lower-part of the bore 11v past the screw 18 through the assage 15 to the upper part of the bore 11. 1
a lay-passage in the wall thereof opening on. I respective end portions of the piston passage,
a head piece screwed into the open end of said ertain valves v in the piston function with novel effect at the V casing beyond the adjacent end of said passage having a circumscribing groove com-. municating with the passage, a multiplicity of ports opening. from the groove through the inner face of the head, and check valves mounted respectively in said ports to oppose movement of'fluid in one direction through the said'by-passage.
2. The structure of claim 1 in which the 5 by-passage is of considerable width, opening also on the end'of the casing adjacent said head, said head having a flange, and a closure plate for the open end of the by-passage confined against the end of the casing by said head.
In testimony whereof I affix my signature.
ADNA F. BLANCHARD.
US152003A 1926-12-01 1926-12-01 Shock absorber Expired - Lifetime US1743591A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045781A (en) * 1957-05-17 1962-07-24 Lees Sidney Viscous damper
DE102007032314A1 (en) * 2007-07-11 2009-01-15 Audi Ag Twin-Tube Shock
US20230256785A1 (en) * 2023-02-10 2023-08-17 Daniel J. Worley Electronically Adjustable Sway Bar Link

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045781A (en) * 1957-05-17 1962-07-24 Lees Sidney Viscous damper
DE102007032314A1 (en) * 2007-07-11 2009-01-15 Audi Ag Twin-Tube Shock
US9371880B2 (en) 2007-07-11 2016-06-21 Audi Ag Dual-tube shock absorber
US20230256785A1 (en) * 2023-02-10 2023-08-17 Daniel J. Worley Electronically Adjustable Sway Bar Link

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