US3074520A - Continuity device - Google Patents
Continuity device Download PDFInfo
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- US3074520A US3074520A US447A US44760A US3074520A US 3074520 A US3074520 A US 3074520A US 447 A US447 A US 447A US 44760 A US44760 A US 44760A US 3074520 A US3074520 A US 3074520A
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/16—Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal
- H01Q15/165—Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal composed of a plurality of rigid panels
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/30—Trim molding fastener
- Y10T24/309—Plastic type
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/44—Clasp, clip, support-clamp, or required component thereof
- Y10T24/44068—Clasp, clip, support-clamp, or required component thereof having gripping member actuated by fluid force
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/54—Flexible member is joint component
Definitions
- One particular application for which the present invention is intended is the bridging of sections of a high frequency radar antenna. It is desirable that the reflecting surface of such a radar antenna be a continuous surface without physical or electrical voids. Nevertheless, for the sake of portability and ease of repair and replacement, the antenna is usually formed in sections which are assembled together at the point of installation. To require that the sections when assembled form a continuous surface would place stringent limits on their manufacturing tolerances and thereby greatly increase their cost. A bet ter approach appears to be to deliberately space the sections one from the other and then provide some means for bridging the spaces. However, with the sections spaced, relative movement between sections will occur when the antenna is in motion.
- an object of this invention is to provide a device that bridges spaced relatively movable bodies, conducting current and/or covering the opening therebetween.
- Another object of this invention is to provide a device of this type that develops uniform contact pressure against the bodies being bridged but does not hamper their relative movement.
- a further object of this invention is to provide a device of this type that is inexpensive to manufacture and easy to use.
- the device comprises a bridging member secured to a closed hollow pneumatically deformable member, a pneumatically deformable member being herein defined as a component that is deformed by the pressure of air or any other fluid.
- the deformable member is resilient, and it is designed to assume one particular shape when it is deformed by inflation or evacuation and another particular shape when it is relaxed or undeformed by inflation or evacuation.
- the deformed shape allows the device to be easily positioned between the adjacent edges of two spaced relatively movable bodies, the deformable member being placed in grooves formed in the adjacent edges and the bridging member being placed adjacent to the surfaces on which the continuity is desired. Once the device is properly positioned, the pressure or vacuum in the deformable member is relieved, and its relaxed shape is such that it engages the grooves in the adjacent edges and biases the bridging member against the surfaces of the bodies.
- a feature of this invention resides in a continuity device having a pneumatically deformable member that in an inflated or evacuated condition is easily positioned between spaced relatively movable bodies and in a relaxed condition biases a bridging member against the surfaces of the bodies.
- FIG. 1 is a perspective view partly in section of a first embodiment of the device of this invention showing the pneumatically deformable member of the device in a relaxed condition whereby it biases the bridging member of the device into contact with the surfaces of two spaced relatively movable bodies;
- FIG. 2 is a cross sectional view of the device in FIG. 1;
- FIG. 3 is a view similar to FIG. 2 but showing the deformable member in an inflated condition
- FIG. 4 is a cross sectional view of a second embodiment of the continuity device showing the deformable member in a relaxed condition
- PEG. 5 is a view similar to FIG. 4 showing the deformable member in an evacuated condition
- FIGS. 6 and 7 are fragmentary cross sectional views showing how, when the deformable member is in a relaxed condition, the bridging member maintains continuity between the spaced bodies even though there is relative motion between the bodies.
- the continuity device comprises a pneumatically deformable member 10, hereinafter referred to as a tube, having a stem portion 12 affixed to a bridging member 14, hereinafter referred to as a cap.
- the tube is formed from a flexible material, such as rubber, and it is formed with a hermetically sealed cavity 16 extending therethrough.
- the cavity is in communication with a valve 18 that is advantageously integral with the tube and is located at a convenient point on the tube.
- the tube 10 is designed to assume one particular shape when it is in a relaxed condition, that is, when there is no pressure differential between the inside and the outside thereof, and as illustrated in FIGS. 3 and 5, it is designed to assume another particular shape when it is in a deformed condition, that is, when there is a pressure differential between the inside and the outside thereof caused either by the introduction of air or some other fluid into the cavity 16 by the evacuation of air from the cavity.
- Both shapes are determined by the configuration of the opening between the spaced relatively movable bodies to be joined, the bodies being indicated on the drawing by the reference numerals 20 and 22.
- the juxtaposed surfaces of the bodies are notched or grooved as shown in FIG. 2, or relieved as shown in FIG. 4.
- the opening defined by the juxtaposed surfaces of the bodies then takes on the configuration of a constricted entryway leading into a cavity, the surfaces at the juncture of the entryway and the cavity providing ledges or shoulders.
- a relaxed shape is selected that includes lateral extremities that are spaced a greater distance apart than the width of the entry way and bearing portions that tend to assume positions that are spaced closer to the cap 14 than the length of the entryway.
- a deformed version of the relaxed shape having a peripheral length (herein defined as the length of the line bounding the cavity of the tube when viewed in transverse cross section) that is substantially the same as the peripheral length of the relaxed shape but having this peripheral length rearranged to provide a second shape in which the lateral extremitie are moved toward one another and the bearing portions are spaced a greater distance from the cap than the length of the entryway.
- This deformed shape permits the tube to be easily placed through the entryway and into the cavity.
- the tube is designed with particular portions of the wall around the cavity thinner than the other portions, thefithinner portions being indicated on the drawing by the. reference numeral 24.
- the pressure exerted on the wall is everywhere equal, but the portions of the wall that are thinner are more flexible and therefore flex to a greater degree than the thicker portions, thereby giving the tube the selected deformed shape.
- the tube It is formed in the shape of a mouth with the midportions of the lower and upper lips thinner than the extremities.
- the corners of 'the mouth which are both the lateral extremities and the bearing portions of the tube, tend to move downward, thereby biasing the cap 14 against the spaced bodies.
- both lips flex, thereby moving the corners of the mouth in toward each other and away from the cap.
- the tube 10 is formed in the shape of a cylinder with the walls at the side thinner than the walls at the top and the bottom.
- the bottom wall of the cylinder which is the bearing portion of the tube, tends to assume a position that is closer to the cap than the length of the entryway, and thus the cylinder biases the cap 14 against the spaced bodies.
- the side walls which are the lateral extremities of the tube, move in toward each other, thereby moving the bottom wall of the cylinder away from the cap.
- the design of the cap 14 is determined by the function that the continuity device is to perform. If it is to provide only surface continuity between the spaced relatively movable bodies, it is designed to engage the surfaces along the entire length of the adjacent edges, and advantageously it can be formed from a highly flexible material, such as rubber, which. will provide a good closure over the space between the bodies. If it is designed to provide only electrical continuity, it need only engage the electrically conductive portions of the surfaces of the bodies.
- It is designed to make a good electrical contact with these surfaces, and it is formed from an electrically conductive material, such as aluminum. If it is to provide both surface and electrical continuity between the bodies, it is designed to engage the surfaces along the entire length of the adjacent edges, making a good electrical contact with the conductive portions of the surface and a good closure against the entire length of the surfaces. In this case, it may be formed entirely from an electrically conductive material, or it may be a composite of conductive matethrough the valve, and the tube assumes its relaxed shape, whereby the cap is biased against the surfaces of the bodies.
- Vari- 1 In a structure including two spaced elements, each element having a first surface facing the first surface of the other element, a second surface extending from the first surface and diverging from the second surface of the other element, and a third surface extending from the first surface a spaced distance from the second surface and diverging from the third surface of the other element, the combination therewith of a device for providing continuity between the spaced elements, the continuity device comprising a bridging portion joined to a hollow pneumatically deformable portion, the bridging portion being positioned in juxtaposition with the second surfaces of the spaced elements at the same time that the deformable portion is positioned in juxtaposition with the third surfaces of the spaced elements, the deformable portion when in a relaxed condition having a first shape that includes portions that bear against the third surfaces and bias the bridging portion against the second surfaces, and the deformable portion when deformed by a pressure differential between the inside
- a-structure including two spaced elements, each element having a first surface facing the first surface of the other element, a second surface extending from the first surface and diverging from the second surface of ,the other element, and a third surface extending from the first surface a spaced distance from the second surface and diverging from the third surface of the other element, the combination therewith of a device for providing continuity between the spaced elements, the continuity device comprising a bridging portion joined to a hollow pneumatically deformable portion, the bridging portion being positioned in juxtaposition with the second surfaces of the spaced elements at the same time that the deformable portion is positioned in juxtaposition with the third surfaces of the spaced elements, the deformable portion whenin a relaxed condition having a first shape that includes lateral extremities that are spaced a greater distance apart than the distance between the first surfaces and thereby prevent the removal of the deformable portion through the space between the first surfaces, the deformable portion when deformed by a pressure differential between the inside and outside thereof having a second shape in which
- each *element having a first surface facing the first surface of the other element, a second surface extending from the first surface and diverging from the second surface of the other element, and a thirdsurface extending from the first surface a spaced distance from the second sur- 7 face and diverging from the third surface of the other ous changes can be made in the design and arrangement of the parts without departing from the spirit and the scope of the accompanying claims.
- the continuity device comprising a bridging portion joined to a pneumatically deformable portion, the bridging portion being positioned in juxtaposition with the second surfaces of the spaced elements at the same time that the deformable portion is positioned in juxtaposition with the third surfaces of the spaced elements, the deformable portion being hollow and the wall of the deformable portion selectively varying in flexibility, the deformable portions when in a relaxed condition having a first shape that has a particular peripheral length and includes portions that bear against the third surfaces and bias the bridging portion against the second surfaces, and the deformable portion when deformed by a pressure differential between the inside and outside thereof having a second shape in which the peripheral length thereof is substantially the same as the peripheral length of the first shape but the bearing portions are spaced a greater distance from the bridging portion than the distance between the second and third surfaces and thereby permits the continuity device to be removed from or positioned between the spaced members.
- a continuity device comprising a pneumatically deformable portion joined to a bridging portion, the pneumatically deformable portion being hollow and the wall thereof selectively varying in flexibility, the deformable portion when relaxed having a first shape that has a particular peripheral length and includes bearing portions that are spaced a first distance from the bridging portion and lateral extremities that are spaced at second distance apart, and the deformable portion when deformed by a pressure difierential between the inside and outside thereof having a second shape in which the pe- 6 ripheral length thereof is substantially the same as the peripheral length of the first shape but the bearing portions are spaced a third distance from the bridging portion, which distance is greater than the first distance, and the lateral extremities are spaced a fourth distance apart, which distance is less than the second distance.
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Description
Jan. 22, 1963 INVENF R Cu EQM ATTORNEY United States Patent 3,074,520 CONTINUITY DEVICE Matthew J. Grubelich, North Plainiield, N.J., assignor to Bell Telephone Laboratories, Incorporated, New York, N .Y., a corporation of New York Filed Jan. 4, 1960, Ser. No. 447 4 Claims. (Cl. 189-36) This invention relates to continuity devices and particularly to means for providing electrical and/ or surface continuity between spaced relatively movable bodies.
One particular application for which the present invention is intended is the bridging of sections of a high frequency radar antenna. It is desirable that the reflecting surface of such a radar antenna be a continuous surface without physical or electrical voids. Nevertheless, for the sake of portability and ease of repair and replacement, the antenna is usually formed in sections which are assembled together at the point of installation. To require that the sections when assembled form a continuous surface would place stringent limits on their manufacturing tolerances and thereby greatly increase their cost. A bet ter approach appears to be to deliberately space the sections one from the other and then provide some means for bridging the spaces. However, with the sections spaced, relative movement between sections will occur when the antenna is in motion.
Accordingly, an object of this invention is to provide a device that bridges spaced relatively movable bodies, conducting current and/or covering the opening therebetween.
Another object of this invention is to provide a device of this type that develops uniform contact pressure against the bodies being bridged but does not hamper their relative movement.
A further object of this invention is to provide a device of this type that is inexpensive to manufacture and easy to use.
These and other objects of the invention are achieved in an illustrative embodiment thereof wherein the device comprises a bridging member secured to a closed hollow pneumatically deformable member, a pneumatically deformable member being herein defined as a component that is deformed by the pressure of air or any other fluid. The deformable member is resilient, and it is designed to assume one particular shape when it is deformed by inflation or evacuation and another particular shape when it is relaxed or undeformed by inflation or evacuation. The deformed shape allows the device to be easily positioned between the adjacent edges of two spaced relatively movable bodies, the deformable member being placed in grooves formed in the adjacent edges and the bridging member being placed adjacent to the surfaces on which the continuity is desired. Once the device is properly positioned, the pressure or vacuum in the deformable member is relieved, and its relaxed shape is such that it engages the grooves in the adjacent edges and biases the bridging member against the surfaces of the bodies.
Thus, a feature of this invention resides in a continuity device having a pneumatically deformable member that in an inflated or evacuated condition is easily positioned between spaced relatively movable bodies and in a relaxed condition biases a bridging member against the surfaces of the bodies.
A complete understanding of the invention and of this and other features and advantages thereof may be gained from consideration of the following detailed description taken in conjunction with the accompanying drawing wherein two embodiments of the invention are illustrated. It is to be expressly understood, however, that the drawing is for the purposes of illustration and description and is not to be construed as defining the limits of the invention.
In the drawing:
FIG. 1 is a perspective view partly in section of a first embodiment of the device of this invention showing the pneumatically deformable member of the device in a relaxed condition whereby it biases the bridging member of the device into contact with the surfaces of two spaced relatively movable bodies;
FIG. 2 is a cross sectional view of the device in FIG. 1;
FIG. 3 is a view similar to FIG. 2 but showing the deformable member in an inflated condition;
FIG. 4 is a cross sectional view of a second embodiment of the continuity device showing the deformable member in a relaxed condition;
PEG. 5 is a view similar to FIG. 4 showing the deformable member in an evacuated condition; and
FIGS. 6 and 7 are fragmentary cross sectional views showing how, when the deformable member is in a relaxed condition, the bridging member maintains continuity between the spaced bodies even though there is relative motion between the bodies.
Referring to the drawing, the continuity device comprises a pneumatically deformable member 10, hereinafter referred to as a tube, having a stem portion 12 affixed to a bridging member 14, hereinafter referred to as a cap. The tube is formed from a flexible material, such as rubber, and it is formed with a hermetically sealed cavity 16 extending therethrough. The cavity is in communication with a valve 18 that is advantageously integral with the tube and is located at a convenient point on the tube.
As illustrated in FIGS. 2 and 4, the tube 10 is designed to assume one particular shape when it is in a relaxed condition, that is, when there is no pressure differential between the inside and the outside thereof, and as illustrated in FIGS. 3 and 5, it is designed to assume another particular shape when it is in a deformed condition, that is, when there is a pressure differential between the inside and the outside thereof caused either by the introduction of air or some other fluid into the cavity 16 by the evacuation of air from the cavity.
Both shapes are determined by the configuration of the opening between the spaced relatively movable bodies to be joined, the bodies being indicated on the drawing by the reference numerals 20 and 22. Advantageously the juxtaposed surfaces of the bodies are notched or grooved as shown in FIG. 2, or relieved as shown in FIG. 4. The opening defined by the juxtaposed surfaces of the bodies then takes on the configuration of a constricted entryway leading into a cavity, the surfaces at the juncture of the entryway and the cavity providing ledges or shoulders. A relaxed shape is selected that includes lateral extremities that are spaced a greater distance apart than the width of the entry way and bearing portions that tend to assume positions that are spaced closer to the cap 14 than the length of the entryway. The lateral extremities prevent movement of the tube through the entryway and the bearing portions bear against the ledges or shoulders provided and bias the cap 14 against the external surfaces of the bodies. Then a deformed version of the relaxed shape is selected having a peripheral length (herein defined as the length of the line bounding the cavity of the tube when viewed in transverse cross section) that is substantially the same as the peripheral length of the relaxed shape but having this peripheral length rearranged to provide a second shape in which the lateral extremitie are moved toward one another and the bearing portions are spaced a greater distance from the cap than the length of the entryway. This deformed shape permits the tube to be easily placed through the entryway and into the cavity.
To achieve the desired transition from the selected relaxed shape to the selected deformed shape, the tube is designed with particular portions of the wall around the cavity thinner than the other portions, thefithinner portions being indicated on the drawing by the. reference numeral 24. When a pressure differential is created between the inside and the outside of the cavity, the pressure exerted on the wall is everywhere equal, but the portions of the wall that are thinner are more flexible and therefore flex to a greater degree than the thicker portions, thereby giving the tube the selected deformed shape.
In the embodiment in FIGS. 1, 2, and 3, the tube It) is formed in the shape of a mouth with the midportions of the lower and upper lips thinner than the extremities. When the tube is in a relaxed position, the corners of 'the mouth, which are both the lateral extremities and the bearing portions of the tube, tend to move downward, thereby biasing the cap 14 against the spaced bodies. When the tube is in an inflated condition, both lips flex, thereby moving the corners of the mouth in toward each other and away from the cap.
In the embodiment in FIGS. 4 and 5, the tube 10 is formed in the shape of a cylinder with the walls at the side thinner than the walls at the top and the bottom. When the tube is in a relaxed condition, the bottom wall of the cylinder, which is the bearing portion of the tube, tends to assume a position that is closer to the cap than the length of the entryway, and thus the cylinder biases the cap 14 against the spaced bodies. When the tube is in an evacuated condition, the side walls, which are the lateral extremities of the tube, move in toward each other, thereby moving the bottom wall of the cylinder away from the cap.
The design of the cap 14 is determined by the function that the continuity device is to perform. If it is to provide only surface continuity between the spaced relatively movable bodies, it is designed to engage the surfaces along the entire length of the adjacent edges, and advantageously it can be formed from a highly flexible material, such as rubber, which. will provide a good closure over the space between the bodies. If it is designed to provide only electrical continuity, it need only engage the electrically conductive portions of the surfaces of the bodies.
It is designed to make a good electrical contact with these surfaces, and it is formed from an electrically conductive material, such as aluminum. If it is to provide both surface and electrical continuity between the bodies, it is designed to engage the surfaces along the entire length of the adjacent edges, making a good electrical contact with the conductive portions of the surface and a good closure against the entire length of the surfaces. In this case, it may be formed entirely from an electrically conductive material, or it may be a composite of conductive matethrough the valve, and the tube assumes its relaxed shape, whereby the cap is biased against the surfaces of the bodies.
As shown in FIGS. 6 and 7, the contact between the cap and the'surfaces of the bodies is maintained even though relative motion occurs between the bodies. To remove the continuity device from between the spaced bodies, it is again deformed by inflation or evacuation.
Although two embodiments of the invention have been illustrated and described in detail, it is to be expressly understood that the invention is not limited thereto. Vari- 1. In a structure including two spaced elements, each element having a first surface facing the first surface of the other element, a second surface extending from the first surface and diverging from the second surface of the other element, and a third surface extending from the first surface a spaced distance from the second surface and diverging from the third surface of the other element, the combination therewith of a device for providing continuity between the spaced elements, the continuity device comprising a bridging portion joined to a hollow pneumatically deformable portion, the bridging portion being positioned in juxtaposition with the second surfaces of the spaced elements at the same time that the deformable portion is positioned in juxtaposition with the third surfaces of the spaced elements, the deformable portion when in a relaxed condition having a first shape that includes portions that bear against the third surfaces and bias the bridging portion against the second surfaces, and the deformable portion when deformed by a pressure differential between the inside and outside thereof having a second shape in which the bearing portions are spaced a greater distance from the bridging portion than the distance between the second and third surfaces and thereby allow the continuity device to be removed from or positioned between the spaced ele ments. 7
2. In a-structure including two spaced elements, each element having a first surface facing the first surface of the other element, a second surface extending from the first surface and diverging from the second surface of ,the other element, and a third surface extending from the first surface a spaced distance from the second surface and diverging from the third surface of the other element, the combination therewith of a device for providing continuity between the spaced elements, the continuity device comprising a bridging portion joined to a hollow pneumatically deformable portion, the bridging portion being positioned in juxtaposition with the second surfaces of the spaced elements at the same time that the deformable portion is positioned in juxtaposition with the third surfaces of the spaced elements, the deformable portion whenin a relaxed condition having a first shape that includes lateral extremities that are spaced a greater distance apart than the distance between the first surfaces and thereby prevent the removal of the deformable portion through the space between the first surfaces, the deformable portion when deformed by a pressure differential between the inside and outside thereof having a second shape in which the lateral extremities are moved toward one another and thereby facilitate the removal or insertion of the deformable portion through the space between the first surfaces.
3. In a structure including two spaced elements, each *elementhaving a first surface facing the first surface of the other element, a second surface extending from the first surface and diverging from the second surface of the other element, and a thirdsurface extending from the first surface a spaced distance from the second sur- 7 face and diverging from the third surface of the other ous changes can be made in the design and arrangement of the parts without departing from the spirit and the scope of the accompanying claims.
What is claimed is:
element, the combination therewith of a device for providing continuity between the spaced elements, the continuity device comprising a bridging portion joined to a pneumatically deformable portion, the bridging portion being positioned in juxtaposition with the second surfaces of the spaced elements at the same time that the deformable portion is positioned in juxtaposition with the third surfaces of the spaced elements, the deformable portion being hollow and the wall of the deformable portion selectively varying in flexibility, the deformable portions when in a relaxed condition having a first shape that has a particular peripheral length and includes portions that bear against the third surfaces and bias the bridging portion against the second surfaces, and the deformable portion when deformed by a pressure differential between the inside and outside thereof having a second shape in which the peripheral length thereof is substantially the same as the peripheral length of the first shape but the bearing portions are spaced a greater distance from the bridging portion than the distance between the second and third surfaces and thereby permits the continuity device to be removed from or positioned between the spaced members.
4. A continuity device comprising a pneumatically deformable portion joined to a bridging portion, the pneumatically deformable portion being hollow and the wall thereof selectively varying in flexibility, the deformable portion when relaxed having a first shape that has a particular peripheral length and includes bearing portions that are spaced a first distance from the bridging portion and lateral extremities that are spaced at second distance apart, and the deformable portion when deformed by a pressure difierential between the inside and outside thereof having a second shape in which the pe- 6 ripheral length thereof is substantially the same as the peripheral length of the first shape but the bearing portions are spaced a third distance from the bridging portion, which distance is greater than the first distance, and the lateral extremities are spaced a fourth distance apart, which distance is less than the second distance.
References Cited in the file of this patent UNITED STATES PATENTS 329,773 Perry Nov. 3, 1885 2,324,520 Lamson July 20, 1943 2,523,716 Parr Sept. 26, 1950 2,685,071 McCreary July 27, 1954 2,883,638 Mark Apr. 21, 1959 2,930,637 Heller Mar. 29, 1960 2,943,874 Valdi et al July 5, 1960
Claims (1)
- 4. A CONTINUITY DEVICE COMPRISING A PNEUMATICALLY DEFORMABLE PORTION JOINED TO A BRIDGING PORTION, THE PNEUMATICALLY DEFORMABLE PORTION BEING HOLLOW AND THE WALL THEREOF SELECTIVELY VARYING IN FLEXIBILITY, THE DEFORMABLE PORTION WHEN RELAXED HAVING A FIRST SHAPE THAT HAS A PARTICULAR PERIPHERAL LENGTH AND INCLUDES BEARING PORTIONS THAT ARE SPACED A FIRST DISTANCE FROM THE BRIDGING PORTION AND LATERAL EXTREMITIES THAT ARE SPACED A SECOND DISTANCE APART, AND THE DEFORMABLE PORTION WHEN DEFORMED BY A PRESSURE DIFFERENTIAL BETWEEN THE INSIDE AND OUTSIDE THEREOF HAVING A SECOND SHAPE IN WHICH THE PERIPHERAL LENGTH THEREOF IS SUBSTANTIALLY THE SAME AS THE PERIPHERAL LENGTH OF THE FIRST SHAPE BUT THE BEARING PORTIONS ARE SPACED A THIRD DISTANCE FROM THE BRIDGING PORTION, WHICH DISTANCE IS GREATER THAN THE FIRST DISTANCE, AND THE LATERAL EXTREMITIES ARE SPACED A FOURTH DISTANCE APART, WHICH DISTANCE IS LESS THAN THE SECOND DISTANCE.
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US447A US3074520A (en) | 1960-01-04 | 1960-01-04 | Continuity device |
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US447A US3074520A (en) | 1960-01-04 | 1960-01-04 | Continuity device |
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Cited By (24)
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US3324775A (en) * | 1963-04-22 | 1967-06-13 | Acme Highway Prod | Method and means for sealing pavement grooves |
US3379469A (en) * | 1966-02-21 | 1968-04-23 | Elia Louis | Detachable headliner |
US3850214A (en) * | 1972-10-20 | 1974-11-26 | Airflex Containers Ltd | Containers |
US4071990A (en) * | 1975-01-29 | 1978-02-07 | Fritz Traber | Demountable frame and panel |
US4074496A (en) * | 1976-08-12 | 1978-02-21 | Artur Fischer | Composite plate |
US4177353A (en) * | 1977-03-18 | 1979-12-04 | The United States Of America As Represented By The Secretary Of The Army | RFI shielded doors with inflatable gaskets |
US4626615A (en) * | 1985-04-08 | 1986-12-02 | Keene Corporation | RF expansion joint for an electrically sealed enclosure |
FR2582895A1 (en) * | 1985-05-30 | 1986-12-05 | Elf Aquitaine | METHOD OF MOUNTING AN ANTENNA AND ANTENNA THUS OBTAINED |
US4670136A (en) * | 1983-03-05 | 1987-06-02 | Isenmann, Drahterzeugnisse Gmbh | Screen surfacing with exchangeable screen elements |
US4672723A (en) * | 1985-11-04 | 1987-06-16 | Minigrip, Inc. | Stabilized reclosable extruded plastic fasteners |
US4709121A (en) * | 1985-12-23 | 1987-11-24 | General Dynamics, Pomona Division | Hinge seal |
US4762020A (en) * | 1980-05-30 | 1988-08-09 | Peter Schmidberger | Link-type apron arrangement |
US4884381A (en) * | 1976-06-10 | 1989-12-05 | Jorge Gabrielli Zacharias Calixto | Structural joint system |
US5531455A (en) * | 1993-09-16 | 1996-07-02 | Calixto; Jorge Gabrielli Z. | Expansion joint sealing element |
US5979828A (en) * | 1997-04-30 | 1999-11-09 | Mcdonnell Douglas | Apparatus for eliminating gaps in an aircraft |
US6186691B1 (en) * | 1998-10-15 | 2001-02-13 | Klaus Rudolf-Bauer | Linear joining and sealing device |
US6185807B1 (en) * | 1997-01-28 | 2001-02-13 | Seagate Technology Llc | Component sealing system |
US20040099767A1 (en) * | 2002-11-22 | 2004-05-27 | Colich Joseph M. | Flexible hydraulic latch |
US20050140098A1 (en) * | 2003-12-31 | 2005-06-30 | The Boeing Company | Apparatus and method for sealing surfaces |
US20070251147A1 (en) * | 2006-04-28 | 2007-11-01 | Box Neil K | Door sealing system |
US20070256390A1 (en) * | 2005-09-29 | 2007-11-08 | Carrier Corporation | Trim joint for sealing gaps between panes of flat glass |
US20100170160A1 (en) * | 2006-06-21 | 2010-07-08 | Albanese James V | Weatherstrip adapted to be captured in t-slots |
US20100301166A1 (en) * | 2009-06-01 | 2010-12-02 | Lockheed Martin Corporation | Expandable precured joint filler |
US9415853B2 (en) | 2013-01-30 | 2016-08-16 | The Boeing Company | Surface sealing system |
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Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3324775A (en) * | 1963-04-22 | 1967-06-13 | Acme Highway Prod | Method and means for sealing pavement grooves |
US3379469A (en) * | 1966-02-21 | 1968-04-23 | Elia Louis | Detachable headliner |
US3850214A (en) * | 1972-10-20 | 1974-11-26 | Airflex Containers Ltd | Containers |
US4071990A (en) * | 1975-01-29 | 1978-02-07 | Fritz Traber | Demountable frame and panel |
US4884381A (en) * | 1976-06-10 | 1989-12-05 | Jorge Gabrielli Zacharias Calixto | Structural joint system |
US4074496A (en) * | 1976-08-12 | 1978-02-21 | Artur Fischer | Composite plate |
US4177353A (en) * | 1977-03-18 | 1979-12-04 | The United States Of America As Represented By The Secretary Of The Army | RFI shielded doors with inflatable gaskets |
US4762020A (en) * | 1980-05-30 | 1988-08-09 | Peter Schmidberger | Link-type apron arrangement |
US4670136A (en) * | 1983-03-05 | 1987-06-02 | Isenmann, Drahterzeugnisse Gmbh | Screen surfacing with exchangeable screen elements |
US4626615A (en) * | 1985-04-08 | 1986-12-02 | Keene Corporation | RF expansion joint for an electrically sealed enclosure |
EP0205366A1 (en) * | 1985-05-30 | 1986-12-17 | Elene S.A. | Method of assembling an antenna |
FR2582895A1 (en) * | 1985-05-30 | 1986-12-05 | Elf Aquitaine | METHOD OF MOUNTING AN ANTENNA AND ANTENNA THUS OBTAINED |
US4672723A (en) * | 1985-11-04 | 1987-06-16 | Minigrip, Inc. | Stabilized reclosable extruded plastic fasteners |
US4709121A (en) * | 1985-12-23 | 1987-11-24 | General Dynamics, Pomona Division | Hinge seal |
US5531455A (en) * | 1993-09-16 | 1996-07-02 | Calixto; Jorge Gabrielli Z. | Expansion joint sealing element |
US6185807B1 (en) * | 1997-01-28 | 2001-02-13 | Seagate Technology Llc | Component sealing system |
US6347021B2 (en) | 1997-01-28 | 2002-02-12 | Seagate Technology Llc | Component sealing system |
US5979828A (en) * | 1997-04-30 | 1999-11-09 | Mcdonnell Douglas | Apparatus for eliminating gaps in an aircraft |
US6186691B1 (en) * | 1998-10-15 | 2001-02-13 | Klaus Rudolf-Bauer | Linear joining and sealing device |
US20040099767A1 (en) * | 2002-11-22 | 2004-05-27 | Colich Joseph M. | Flexible hydraulic latch |
US6951319B2 (en) * | 2002-11-22 | 2005-10-04 | Theboeing Company | Flexible hydraulic latch |
US20050140098A1 (en) * | 2003-12-31 | 2005-06-30 | The Boeing Company | Apparatus and method for sealing surfaces |
US7784799B2 (en) * | 2003-12-31 | 2010-08-31 | The Boeing Company | Apparatus and method for sealing surfaces |
US20070256390A1 (en) * | 2005-09-29 | 2007-11-08 | Carrier Corporation | Trim joint for sealing gaps between panes of flat glass |
US7743560B2 (en) * | 2006-04-28 | 2010-06-29 | Box Neil K | Door sealing system |
US20070251147A1 (en) * | 2006-04-28 | 2007-11-01 | Box Neil K | Door sealing system |
US20100170160A1 (en) * | 2006-06-21 | 2010-07-08 | Albanese James V | Weatherstrip adapted to be captured in t-slots |
US8769876B2 (en) * | 2006-06-21 | 2014-07-08 | Ultrafab, Inc. | Weatherstrip adapted to be captured in t-slots |
US20100301166A1 (en) * | 2009-06-01 | 2010-12-02 | Lockheed Martin Corporation | Expandable precured joint filler |
US8316544B2 (en) | 2009-06-01 | 2012-11-27 | Lockheed Martin Corporation | Expandable precured joint filler |
US9415853B2 (en) | 2013-01-30 | 2016-08-16 | The Boeing Company | Surface sealing system |
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