US2558103A - Mechanical linkage with liquid sealing means - Google Patents

Mechanical linkage with liquid sealing means Download PDF

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Publication number
US2558103A
US2558103A US95916A US9591649A US2558103A US 2558103 A US2558103 A US 2558103A US 95916 A US95916 A US 95916A US 9591649 A US9591649 A US 9591649A US 2558103 A US2558103 A US 2558103A
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United States
Prior art keywords
receptacle
bearing
shaft
lever
liquid
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Expired - Lifetime
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US95916A
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Robert E Ruckstahl
Harold M Watson
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CBS Corp
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Westinghouse Electric Corp
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Priority to US95916A priority Critical patent/US2558103A/en
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Publication of US2558103A publication Critical patent/US2558103A/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
    • F16HGEARING
    • F16H51/00Levers of gearing mechanisms
    • 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
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/50Sealings between relatively-movable members, by means of a sealing without relatively-moving surfaces, e.g. fluid-tight sealings for transmitting motion through a wall
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00Seal for a joint or juncture
    • Y10S277/91O-ring seal
    • 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
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20576Elements
    • Y10T74/20582Levers
    • 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
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20576Elements
    • Y10T74/2093Slot closers and lever guards

Definitions

  • Our invention relates to apparatus for transmitting motion of one member to some other member, and more particularly our invention is directed to a new type linkage, and liquid seal therefor, by means of which a force may be transmitted from an enclosure filled with liquid to theexterior of the enclosure without leakage of any liquid from the enclosure.
  • One broad object of. our invention is the provision of means for transmitting a force acting on a member within an enclosure to. a member outside of the enclosure without leakage of any fluid in the enclosure to the outside.
  • Another but somewhat more specific object of our invention is the provision of linkage means for transmitting a force acting in a given direction within an enclosure to theoutside of the enclosure acting in the same plane without having any liquid in the enclosure leak from the enclosure at the bearings of the. linkage means.
  • Figure 1 is a broken out portion of an enclosure, or receptacle, showing the linkage and bearing structure therefor inlongitudinal section;
  • Fig, 2 is a view in section, along section line IIII of the subject matter shown in Fig. 1;
  • Fig. 3 shows a modification of our invention with the bearing structure shown in section.
  • Such devices usually include a bulky rubber diaphragm which is clamped around the neck of the link and the flange thereof is secured to the housing.
  • the diaphragm flexes with each movement of the link.
  • apparatus for guided missiles require the use of oils in anenclosure that must remain at substantially the same viscosity for temperature variations from 40 below zero to 225 above zero, it is apparent that a requirement is placed on the diaphragm which it is not capable of satisfying. At one temperature extreme the diaphragm solidifies and breaks and at the other extreme it becomes so pliable and soft that it tears readily.
  • a cap 5 is designed to fit. into, the recess 3 and is provided longitudinally thereof with a semi-cylindrical bearing .groove .6 of the same dimensions as hearing groovev 4 and having a common axis with the. bearing groove 4.
  • the side. wall atthe thickened portion and substantially rat the middle of the cylindrical bearing formed by the bearing groove 4 and 6 is provided with a dove-tailed slot 1.
  • the cap 5 is provided with two dove-tailed slots 8. and 9 disposed, respectively, near the ends of the bearing so that a cylindrical bearing surface of some axial length is provided between slots 8 and I and a similar cylindrical bearing surface of some axial length is provided between slots I and 9.
  • a movement transmitting link III having, the projection II, the stub shafts I2 and I3, and the projection I4 and I5, is so positioned that the projection I I extends through the slot 1 and the projections I 4 and I5 extend through slots 8 and 9, respectively.
  • the link I0 may be constructed of asingle forging, or casting, as shown, or of several parts.
  • the stub shafts are provided with bearing sleeves I6 and I] and then projection IIis passed through slot I and then the cap 5 is moved over the projections I4 and I5 is then bolted in position as shown to firmly hold the bearing sleeves and. to compress the O-rings I8 and I9 to efiectively sealthe slot I from the slots 8 and 9 and to thus effectively seal the tank against leakage.
  • actuatedmember may be secured to the member 23 at the bifurcations 24, or for that matter the member 23 may be considered either as the actuated member or the actuatin member.
  • link I may be actuated through a total angle of about 70", i. e., 35 to each side of the neutral position and that the force transmitted falls in the same plane as the force received.
  • the force transmitting link I00 with three grooves I20, I22 and I24 between the projections I I4 and I l I, and three similar grooves I2I, I23 and I25 between the projections III and H5. Into these grooves we fit the O-rings H8, I28 and I38, and H9, I29 and I39.
  • reference characters correspond to those used in Figs. 1 and 2, except that each is greater by one hundred.
  • reference characters Hi2, I05, I01, I08, I09, H2, H3, H6, In, etc. correspond in the elements to which they refer to reference characters 2, 5, I, 8, 9, I2, I3, I6, 11, etc.
  • a receptacle adapted to contain a liquid, said receptacle being provided with a table on one inner surface of the receptacle and the table being provided near its mid-region with a dove-tailed slot with the flared end of the slot being directed inwardly, the outer surface of the receptacle below the table being provided with a recess, a covering plate bolted into the base of the table and filling said recess, a semi-cylindrical bearing groove in the outer surface of said recess and a similar bearing groove in the plate both arranged in axial alignment, cylindrical bearings in the corresponding ends of the bearing grooves, a shaft disposed to snugly fit in said bearings, a lever rigidly secured to the mid-region of the shaft and disposed to project into the
  • a receptacle adapted to contain a liquid, said receptacle being provided with a table on one inner surface of the receptacle and the table being provided near its mid-region with a dove-tailed slot with the flared end of the slot being directed inwardly, the outer surface of the receptacle below the table being provided with a recess, a covering plate bolted into the base of the table and filling said recess, a semi-cylindrical bearing groove in the outer surface of said recess and a similar bearing groove in the plate both arranged in axial alignment, cylindrical bearings in the corresponding ends of the bearing grooves, a shaft disposed to snugly fit in said bearings, a lever rigidly secured to the mid-region of the shaft and disposed to project into the
  • a receptacle having a relatively thick side-wall, a bearing in the side-wall having four axially aligned axially spaced cylindrical bearing surfaces, a shaft disposed to snugly fit into the bearingsurfaces, liquid seals disposed in the bearing surfaces disposed between the two outer bearing surfaces, aprojection rigidly secured to the shaft and projecting inwardly through a dovetailed slot in the side-wall between the two middle bearing surfaces, a pair of projections rigidly secured to the shaft, one projecting outwardlly through a dove-tailed slot in the side-wall be tween one end bearing surface and the proximate bearing surface, and the other projecting outwardly through a dove-tailed slot in the sidewall between the other end bearing surface and the bearing surface proximate to this said other end bearing surface, and
  • a tank a plurality of axially aligned and axially spaced cylindrical bearing surfaces in side-wall of the tank, a shaft in the bearing surfaces, said shaft being provided with oppositely projecting levers, one projecting into the tank through a dove-tailed slot in the inner surface of the side-wall to the axis of the bearing surfaces,
  • the other lever projecting out of the tank through a dove-tailed slot in the outer surface of the sidewall to the axis of the bearing surfaces, said projections being axially spaced along the shaft so that one bearing surface is disposed about the shaft between the projections, a liquid seal disposed about the shaft and in the bearing surface between the projections, an actuated member at one end of one projection, and an actuating member at the end of the other projection.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sealing Devices (AREA)

Description

u 1951 R. E. RUCKSTAHL ET AL 2,553,103
MECHANICAL LINKAGE WITH LIQUID SEALING MEANS Filed May 28, 1949 7B 9 2 H O W mum. V .I T C "a m u M l Ni s \A V .M I L NEO. I. S k. nval mH d. L
WITNESSES W 2M4.
ATTORN EY Patented June 26, 1951 ME A I IN GE H LIQU SEALING MEANS Robert E. Ruckstahl, Turtle Creek, and Harold Watson, Pittsburgh, Pa., assignors to- West-- inghouse Electric Co rporation, East Pittsburgh,.
1%., a corporation of Pennsylvania.
Application May 28, 1949, Serial'No. 95,916
Our invention relates to apparatus for transmitting motion of one member to some other member, and more particularly our invention is directed to a new type linkage, and liquid seal therefor, by means of which a force may be transmitted from an enclosure filled with liquid to theexterior of the enclosure without leakage of any liquid from the enclosure.
One broad object of. our invention is the provision of means for transmitting a force acting on a member within an enclosure to. a member outside of the enclosure without leakage of any fluid in the enclosure to the outside.
Another but somewhat more specific object of our invention is the provision of linkage means for transmitting a force acting in a given direction within an enclosure to theoutside of the enclosure acting in the same plane without having any liquid in the enclosure leak from the enclosure at the bearings of the. linkage means.
The objects recited are merely illustrative. Other objects and advantages will become readily apparent from a study of the following specification and the accompanying drawing, in which:
Figure 1 is a broken out portion of an enclosure, or receptacle, showing the linkage and bearing structure therefor inlongitudinal section;
Fig, 2 is a view in section, along section line IIII of the subject matter shown in Fig. 1; and
Fig. 3 shows a modification of our invention with the bearing structure shown in section.
We are aware that devices forthe purpose to which our invention is directed are well known in the prior art. Such devices usually include a bulky rubber diaphragm which is clamped around the neck of the link and the flange thereof is secured to the housing. In thismost favored apparatus for the purpose the diaphragm flexes with each movement of the link. However, since apparatus for guided missiles require the use of oils in anenclosure that must remain at substantially the same viscosity for temperature variations from 40 below zero to 225 above zero, it is apparent that a requirement is placed on the diaphragm which it is not capable of satisfying. At one temperature extreme the diaphragm solidifies and breaks and at the other extreme it becomes so pliable and soft that it tears readily.
With our construction the sealing effect of the materials used is not noticeably affected. by the changes in temperatures to which theguided missile is subjected during use and proper functioning of the apparatus within the guided missile is always obtained.
4 Claims. (Cl; 74-519) In the figures of the drawing, I designates the tank, or enclosure. The enclosure, or receptacle, is provided with a table, or thickened, portion 2. This thickened portion of the side-Wall is provided with a generally rectangular recess 3 which is provided longitudinally thereof with a semi-cylindrical bearing groove .4. v
A cap 5 is designed to fit. into, the recess 3 and is provided longitudinally thereof with a semi-cylindrical bearing .groove .6 of the same dimensions as hearing groovev 4 and having a common axis with the. bearing groove 4.
The side. wall atthe thickened portion and substantially rat the middle of the cylindrical bearing formed by the bearing groove 4 and 6 is provided with a dove-tailed slot 1. The cap 5 is provided with two dove-tailed slots 8. and 9 disposed, respectively, near the ends of the bearing so that a cylindrical bearing surface of some axial length is provided between slots 8 and I and a similar cylindrical bearing surface of some axial length is provided between slots I and 9.
A movement transmitting link III, having, the projection II, the stub shafts I2 and I3, and the projection I4 and I5, is so positioned that the projection I I extends through the slot 1 and the projections I 4 and I5 extend through slots 8 and 9, respectively. The link I0 may be constructed of asingle forging, or casting, as shown, or of several parts.
In order to provide for an effective seal for the tank, provision must be made for a leakproof seal at the cylindrical bearing surfaces falling; respectively, between slots 8 and I and slots 'I and 9. To accomplish the sealing action we provide the link with grooves 28 and 2| and into these grooves we position O-rings of rubber, nylon, or preferably neoprene, having a sectional diametrical dimension greater than the depth of the grooves 20 and 2I.
In the assembly of the parts the stub shafts are provided with bearing sleeves I6 and I] and then projection IIis passed through slot I and then the cap 5 is moved over the projections I4 and I5 is then bolted in position as shown to firmly hold the bearing sleeves and. to compress the O-rings I8 and I9 to efiectively sealthe slot I from the slots 8 and 9 and to thus effectively seal the tank against leakage.
To the inner end of projection II. we adjustably secure the rod 22 and to the outwardly projecting. ends of the projections I4 and I5, we secure the member 23 bysuitable bolts or rivets as shown. An actuatedmember may be secured to the member 23 at the bifurcations 24, or for that matter the member 23 may be considered either as the actuated member or the actuatin member.
From the construction shown it will readily be apparent that the link I may be actuated through a total angle of about 70", i. e., 35 to each side of the neutral position and that the force transmitted falls in the same plane as the force received. I
In connection with some oils in the tank the prevention of oil leaks may be somewhat more diflicult than normal. To still more effectively seal the tank we provide, in the modification shown in Fig. 3, the force transmitting link I00 with three grooves I20, I22 and I24 between the projections I I4 and I l I, and three similar grooves I2I, I23 and I25 between the projections III and H5. Into these grooves we fit the O-rings H8, I28 and I38, and H9, I29 and I39.
These O-rings have a greater sectional diameter than the depth of the respective grooves into which they are positioned. The result is a very excellent seal for the tank.
In describing Fig. 3 it will be noted that the reference characters correspond to those used in Figs. 1 and 2, except that each is greater by one hundred. For example, reference characters Hi2, I05, I01, I08, I09, H2, H3, H6, In, etc., correspond in the elements to which they refer to reference characters 2, 5, I, 8, 9, I2, I3, I6, 11, etc.
While we have shown but a single embodiment of our invention, it will be understood that changes may be made in the arrangement and combination of the parts all within the scope of the appended claims without departing from the spirit of the invention.
We claim as our invention:
1. In apparatus for transmitting movement of a member in a receptacle adapted to contain a liquid to a member outside of the receptacle without leakage of any liquid from the receptacle, in combination, a receptacle adapted to contain a liquid, said receptacle being provided with a table on one inner surface of the receptacle and the table being provided near its mid-region with a dove-tailed slot with the flared end of the slot being directed inwardly, the outer surface of the receptacle below the table being provided with a recess, a covering plate bolted into the base of the table and filling said recess, a semi-cylindrical bearing groove in the outer surface of said recess and a similar bearing groove in the plate both arranged in axial alignment, cylindrical bearings in the corresponding ends of the bearing grooves, a shaft disposed to snugly fit in said bearings, a lever rigidly secured to the mid-region of the shaft and disposed to project into the receptacle through said dove-tailed slot in the table, a second lever rigidly secured to the shaft axially spaced from one side of the first lever, said cover plate being provided with an outwardly flaring dove-tailed groove for receiving the second lever so that the second lever projects beyond the outer surface of the cover plate, a liquid sealing ring disposed about the shaft and between the first and second levers and snugly fitting about the shaft and engaging the bearing grooves to thus effectively seal the liquid against leakage from the receptacle, an operating rod connected to the end of the first lever, and an operated rod connected to the end of the second lever.
2. In apparatus for transmitting movement of a member in a receptacle adapted to contain a liquid to a member outside of the receptacle without leakage of any liquid from the receptacle, in combination, a receptacle adapted to contain a liquid, said receptacle being provided with a table on one inner surface of the receptacle and the table being provided near its mid-region with a dove-tailed slot with the flared end of the slot being directed inwardly, the outer surface of the receptacle below the table being provided with a recess, a covering plate bolted into the base of the table and filling said recess, a semi-cylindrical bearing groove in the outer surface of said recess and a similar bearing groove in the plate both arranged in axial alignment, cylindrical bearings in the corresponding ends of the bearing grooves, a shaft disposed to snugly fit in said bearings, a lever rigidly secured to the mid-region of the shaft and disposed to project into the receptacle through said dove-tailed slot in the table, a second lever rigidly secured to the shaft axially spaced from one side of the first lever, a third lever rigidly secured to the shaft axially spaced from the other side of the first lever, said cover plate being provided with an outwardly flaring dove-tailed groove for receiving the-second lever so that the second lever projects beyond the outer surface of the cover plate, a liquid sealing ring disposed about the shaft and between the first and second levers and snugly fitting about the shaft and engaging the bearing grooves to thus effectively seal the liquid against leakage from the receptacle, said cover plate being provided with an outwardly flaring dove-tailed groove for receiving the third lever so that the third lever projects beyond the outer surface of the cover plate, a liquid sealing ring disposed about the shaft and between the first lever and third lever and snugly fitting about the shaft and engaging the bearing grooves to thus effectively seal the liquid against leakage from the receptacle, an operating rod connected to the end of the first lever, and an operated rod connected to the end of the second and third levers.
3. In apparatus for a guided missile having a sealed receptacle and including apparatus for transmitting movement from a member in the receptacle to a member outside of the receptacle, in combination, a receptacle having a relatively thick side-wall, a bearing in the side-wall having four axially aligned axially spaced cylindrical bearing surfaces,a shaft disposed to snugly fit into the bearingsurfaces, liquid seals disposed in the bearing surfaces disposed between the two outer bearing surfaces, aprojection rigidly secured to the shaft and projecting inwardly through a dovetailed slot in the side-wall between the two middle bearing surfaces, a pair of projections rigidly secured to the shaft, one projecting outwardlly through a dove-tailed slot in the side-wall be tween one end bearing surface and the proximate bearing surface, and the other projecting outwardly through a dove-tailed slot in the sidewall between the other end bearing surface and the bearing surface proximate to this said other end bearing surface, and means for operating said shaft through said projections.
4. In apparatus for transmitting motion from the inside of a tank in a guided missile adapted to contain a liquid to the outside of the tank, in combination, a tank, a plurality of axially aligned and axially spaced cylindrical bearing surfaces in side-wall of the tank, a shaft in the bearing surfaces, said shaft being provided with oppositely projecting levers, one projecting into the tank through a dove-tailed slot in the inner surface of the side-wall to the axis of the bearing surfaces,
the other lever projecting out of the tank through a dove-tailed slot in the outer surface of the sidewall to the axis of the bearing surfaces, said projections being axially spaced along the shaft so that one bearing surface is disposed about the shaft between the projections, a liquid seal disposed about the shaft and in the bearing surface between the projections, an actuated member at one end of one projection, and an actuating member at the end of the other projection.
ROBERT E. RUCKSTAHL.
HAROLD M. WATSON.
REFERENCES CITED The following references are of record in the file of this patent:
" UNITED STATES PATENTS Number Name Date 1,707,264 Gross Apr. 2, 1929 2,324,150 Groomes July 13, 1943 10 2,394,364 Christensen Feb. 5, 1946 Pevney June 7, 1949
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2737816A (en) * 1951-02-03 1956-03-13 Aebi & Co Maschinenfabrik Apparatus for driving the cutter bar of a mowing machine
US2833377A (en) * 1954-11-01 1958-05-06 Gen Motors Corp Railway vehicle brake rigging
US3267753A (en) * 1963-08-02 1966-08-23 Acme Machine Works Inc Landing gear control
US10394271B2 (en) * 2016-05-04 2019-08-27 Beihang University Force feedback handle device with a degree-of-freedom and working method thereof

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1707264A (en) * 1925-11-04 1929-04-02 Edward G Gross Fluid-pressure control for cylinder cocks
US2324150A (en) * 1940-10-21 1943-07-13 Harry M Groomes Liquid dispensing nozzle
US2394364A (en) * 1943-04-15 1946-02-05 Niels A Christensen Pressure seal
US2472724A (en) * 1944-06-26 1949-06-07 Republic Aviat Corp Seal

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1707264A (en) * 1925-11-04 1929-04-02 Edward G Gross Fluid-pressure control for cylinder cocks
US2324150A (en) * 1940-10-21 1943-07-13 Harry M Groomes Liquid dispensing nozzle
US2394364A (en) * 1943-04-15 1946-02-05 Niels A Christensen Pressure seal
US2472724A (en) * 1944-06-26 1949-06-07 Republic Aviat Corp Seal

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2737816A (en) * 1951-02-03 1956-03-13 Aebi & Co Maschinenfabrik Apparatus for driving the cutter bar of a mowing machine
US2833377A (en) * 1954-11-01 1958-05-06 Gen Motors Corp Railway vehicle brake rigging
US3267753A (en) * 1963-08-02 1966-08-23 Acme Machine Works Inc Landing gear control
US10394271B2 (en) * 2016-05-04 2019-08-27 Beihang University Force feedback handle device with a degree-of-freedom and working method thereof

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