US2537822A - Spiral scanning mechanism - Google Patents

Spiral scanning mechanism Download PDF

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Publication number
US2537822A
US2537822A US637125A US63712545A US2537822A US 2537822 A US2537822 A US 2537822A US 637125 A US637125 A US 637125A US 63712545 A US63712545 A US 63712545A US 2537822 A US2537822 A US 2537822A
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United States
Prior art keywords
shaft
hollow shaft
scanning mechanism
worm
spiral scanning
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Expired - Lifetime
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US637125A
Inventor
Fritts Morris
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AT&T Corp
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Bell Telephone Laboratories Inc
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Publication date
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Priority to US637125A priority Critical patent/US2537822A/en
Application granted granted Critical
Publication of US2537822A publication Critical patent/US2537822A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/12Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems
    • H01Q3/16Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device
    • H01Q3/18Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device wherein the primary active element is movable and the reflecting device is fixed
    • 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
    • Y10T74/18Mechanical movements
    • Y10T74/18056Rotary to or from reciprocating or oscillating
    • Y10T74/18184Crank, pitman, and lever
    • 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
    • Y10T74/18Mechanical movements
    • Y10T74/18544Rotary to gyratory

Definitions

  • This invention relates to radio signaling apparatus and more specifically to a scanning mechanism for use in such apparatus.
  • the object of this invention is the provision of a scanning mechanism of the type above referred to whichwill be simple and in which a directive element is operated in a manner to generate a scanning field determined by the operation of two shafts relative to each other.
  • Fig. 1 is an elevational view shown with a number of operating parts in vertical section
  • Fig. 2 is a front elevational view
  • Fig. 3 is a top view
  • Fig. 4 is a partial top view shown with the directive element or reflector in an operated position
  • Fig. 5 is a detail view looking in the direction indicated by the arrows on line 5-5 of Fig. 1;
  • Fig. 6 is a diagrammatic view of the scanning field obtained by the movement of the reflector.
  • the scanning mechanism of this invention consists of a base ll! formed with two upright Supports I l and I2, upright support ll having an inverted U-shaped portion I3 at its free end serving in cooperation with upright support I2 for rotatably mounting as on ball bearings BI and B2, a hollow shaft l4 best seen in Figs. 1 and 3.
  • hollow shaft I4 On one end of hollow shaft I4 is keyed a gear l5 meshing with a pinion I6 keyed on the armature shaft of a motor I! secured to the base [0 as by a number of bolts l8, while on the opposite end of hollow shaft 14 is keyed a forkshaped member 19, the shaft I4 and member 19 being rotated through the operation of motor l'l, pinion l6 and gear l5 keyed as above mentioned on hollow shaft l4.
  • the fork-shaped member I9 is formed with a pair of arms 20 and 2
  • a worm gear 23 On one end of shaft 22 is keyed a worm gear 23 best seen in Fig. 2, meshing with a worm 24 carried or formed at one end of a hollow shaft 25 mounted in position concentric to hollow shaft l4 and supported at one end by support ll, shaft 25 being-held from rotation by a plate 26 secured to upright supports II, as by a number of screws 21, best seen in Figs.
  • a disc member 28 provided with a crank pin 29 serving for pivotally mounting a bell crank 30, the opposite end of which is pivoted to an arm 3
  • Head-piece H in cooperation with a head-piece HI, pivoted on a spindle 34, secured to the other prong of forkshaped member l9, serves for mounting a parabolic reflector 35 having a rim portion 36 clamped between similarly shaped projections S and SI formed with the head-pieces H and HI while the reflector 35 is formed with an oblong-shaped opening 31 through which projects the so-called emitter or antenna 38 connecting with a coaxial line (not shown) in the hollow shaft 25.
  • the operation of motor I! is effective to rotate the hollow shaft I4 and the fork-shaped member l9 carried thereby through the engagement of pinion IS with gear [5 keyed to the hollow shaft [4.
  • the rotation of forkshaped member I9 is effective to rotate the parabolic reflector. 35, while causing the rotation of shaft 22 through the engagement of worm 23 carried by the shaft 22 with the worm 24 carried by the hollow shaft 25, which is held against rotary movement by the forked plate 26.
  • Rotation of shaft 22, and that of the crank formed by disc 28 and the pin 29 which connects with the bell crank 30, is effective to impart reciprocating movements to the head-piece H and thereby to the reflector from the position shown in full line, to the position shown in dotted line in Fig.
  • a mechanical driving apparatus comprising a support, a first hollow shaft rotatably supported in said support, a yoke secured to said hollow shaft, a fixed hollow shaft extending from within said first hollow shaft and into the space between the arms of said yoke, a worm gear on said fixed shaft, a counter-shaft rotatably supported in said yoke, a worm wheel secured to said counter-shaft and in mesh with said worm gear, spaced levers pivotally supported on arms of said yoke and cov operating to support a paraboloid movable member having a transverse slot therein, a rigid member extending through said fixed hollow shaft and through said slot, and a crank and lever system forming a mechanical driving connection between said counter-shaft and at least one of said spaced levers.

Description

Jan. 9, 1951 M. FRITTS 2,537,822
SPIRAL SCANNING MECHANISM Filed Dec. 24, 1945 2 Sheets-Sheet 1 3 .j If .i'. 2
29 I p 28 I l5 1 22 5 27 BI 82 as I 25 4 as BVJ ZMES MM ATTORNEY Jan. 9, 1951 M. FRlTTS 2,537,822
SPIRAL SCANNING MECHANISM Filed Dec. 24, 1945 2 Sheets-Sheet 2 //v l E/VTOR M. FR/ 7' TS Q? 7% xm A T TOANE Y Patented Jan. 9 1951 UNITED STATES PATENT OFFICE Telephone Laboratories,
Incorporated, New
York, N. Y., a corporation of New York Application December 24, 1945, Serial N 0. 637,125
1 Claim.
This invention relates to radio signaling apparatus and more specifically to a scanning mechanism for use in such apparatus.
The object of this invention is the provision of a scanning mechanism of the type above referred to whichwill be simple and in which a directive element is operated in a manner to generate a scanning field determined by the operation of two shafts relative to each other.
In the drawing:
Fig. 1 is an elevational view shown with a number of operating parts in vertical section;
Fig. 2 is a front elevational view;
Fig. 3 is a top view;
Fig. 4 is a partial top view shown with the directive element or reflector in an operated position;
Fig. 5 is a detail view looking in the direction indicated by the arrows on line 5-5 of Fig. 1; and
Fig. 6 is a diagrammatic view of the scanning field obtained by the movement of the reflector.
As shown in the drawing, the scanning mechanism of this invention consists of a base ll! formed with two upright Supports I l and I2, upright support ll having an inverted U-shaped portion I3 at its free end serving in cooperation with upright support I2 for rotatably mounting as on ball bearings BI and B2, a hollow shaft l4 best seen in Figs. 1 and 3.
On one end of hollow shaft I4 is keyed a gear l5 meshing with a pinion I6 keyed on the armature shaft of a motor I! secured to the base [0 as by a number of bolts l8, while on the opposite end of hollow shaft 14 is keyed a forkshaped member 19, the shaft I4 and member 19 being rotated through the operation of motor l'l, pinion l6 and gear l5 keyed as above mentioned on hollow shaft l4.
The fork-shaped member I9 is formed with a pair of arms 20 and 2| extending laterally therefrom and havingbearing portions in which is journaled a shaft 22. On one end of shaft 22 is keyed a worm gear 23 best seen in Fig. 2, meshing with a worm 24 carried or formed at one end of a hollow shaft 25 mounted in position concentric to hollow shaft l4 and supported at one end by support ll, shaft 25 being-held from rotation by a plate 26 secured to upright supports II, as by a number of screws 21, best seen in Figs. 1, 3 and 5, and having a fork-shaped portion fitted over two opposite sides of a square-shaped portion formed at the end of shaft 25 for preventing its rotation as would be imparted by friction between this shaft and the shaft l4 and the friction between the worm 24 and the worm gear 23 while in operation.
To the end of shaft 22, opposite the worm gear 23, there is securely mounted a disc member 28 provided with a crank pin 29 serving for pivotally mounting a bell crank 30, the opposite end of which is pivoted to an arm 3|, best seen in Figs. 2, 3 and 4, formed with a head-piece H in turn pivoted on a spindle 32 secured to the prong P of the fork-shaped member l9. Head-piece H in cooperation with a head-piece HI, pivoted on a spindle 34, secured to the other prong of forkshaped member l9, serves for mounting a parabolic reflector 35 having a rim portion 36 clamped between similarly shaped projections S and SI formed with the head-pieces H and HI while the reflector 35 is formed with an oblong-shaped opening 31 through which projects the so-called emitter or antenna 38 connecting with a coaxial line (not shown) in the hollow shaft 25.
In the operation of the scanning mechanism of this invention, the operation of motor I! is effective to rotate the hollow shaft I4 and the fork-shaped member l9 carried thereby through the engagement of pinion IS with gear [5 keyed to the hollow shaft [4. The rotation of forkshaped member I9 is effective to rotate the parabolic reflector. 35, while causing the rotation of shaft 22 through the engagement of worm 23 carried by the shaft 22 with the worm 24 carried by the hollow shaft 25, which is held against rotary movement by the forked plate 26. Rotation of shaft 22, and that of the crank formed by disc 28 and the pin 29 which connects with the bell crank 30, is effective to impart reciprocating movements to the head-piece H and thereby to the reflector from the position shown in full line, to the position shown in dotted line in Fig. 4 for each complete turn of the shaft 22 to cause the reflector 35 to generate a scanning field representing a spiral, as shown in Fig. 6, the pitch of which is dependent upon the speed ratio between the worm 24 and worm gear 23 for any given speed at which the parabolic reflector may be rotated.
What is claimed is:
A mechanical driving apparatus comprising a support, a first hollow shaft rotatably supported in said support, a yoke secured to said hollow shaft, a fixed hollow shaft extending from within said first hollow shaft and into the space between the arms of said yoke, a worm gear on said fixed shaft, a counter-shaft rotatably supported in said yoke, a worm wheel secured to said counter-shaft and in mesh with said worm gear, spaced levers pivotally supported on arms of said yoke and cov operating to support a paraboloid movable member having a transverse slot therein, a rigid member extending through said fixed hollow shaft and through said slot, and a crank and lever system forming a mechanical driving connection between said counter-shaft and at least one of said spaced levers.
MORRIS FRITTS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,083,242 Runge June 8, 1937 2,231,929 Lyman Feb. 18, 1941 2,407,305 Langstroth et al. Sept. 10, 1946 2,410,831 Maybarduk et a1. Nov. 12, 1946
US637125A 1945-12-24 1945-12-24 Spiral scanning mechanism Expired - Lifetime US2537822A (en)

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2677121A (en) * 1950-10-19 1954-04-27 Pyle National Co Combination warning light and stationary headlight
US2762041A (en) * 1950-09-09 1956-09-04 Motorola Inc Signalling equipment
DE1010122B (en) * 1955-03-10 1957-06-13 Gen Electric Arrangement for the mechanical pivoting of a member to achieve a straight or circular scanning movement
US2811719A (en) * 1953-04-28 1957-10-29 Henry W Wallace Double-universal nod mechanism
US2916739A (en) * 1955-07-28 1959-12-08 Underwood Corp Scanner for antenna system
US2925594A (en) * 1946-03-18 1960-02-16 George A Garrett Radar search scan system
US3166750A (en) * 1961-02-14 1965-01-19 Raytheon Co Antenna intersecting-orthogonal-axes gimbal mount utilizing rotary bearings for two axes and push-pull linkage for third axis
US5422623A (en) * 1990-10-04 1995-06-06 Federal Signal Corporation Programmable emergency signalling device and system
EP2549585A1 (en) * 2011-07-21 2013-01-23 Harris Corporation Systems for positioning reflectors, such as passive reflectors
US9368867B2 (en) 2013-10-07 2016-06-14 Harris Corporation Near-linear drive systems for positioning reflectors
US20170216998A1 (en) * 2014-08-06 2017-08-03 C.M.S. S.P.A. System for supporting a workpiece
DE102020102576A1 (en) 2020-02-03 2021-08-05 Neura Robotics GmbH Device for detecting the position and / or speed of objects in space

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2083242A (en) * 1934-01-27 1937-06-08 Telefunken Gmbh Method of direction finding
US2231929A (en) * 1937-04-29 1941-02-18 Sperry Gyroscope Co Inc Tridimensional radio direction indicator
US2407305A (en) * 1942-04-10 1946-09-10 Sperry Gyroscope Co Inc Scanning device
US2410831A (en) * 1942-04-10 1946-11-12 Sperry Gyroscope Co Inc Scanning device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2083242A (en) * 1934-01-27 1937-06-08 Telefunken Gmbh Method of direction finding
US2231929A (en) * 1937-04-29 1941-02-18 Sperry Gyroscope Co Inc Tridimensional radio direction indicator
US2407305A (en) * 1942-04-10 1946-09-10 Sperry Gyroscope Co Inc Scanning device
US2410831A (en) * 1942-04-10 1946-11-12 Sperry Gyroscope Co Inc Scanning device

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2925594A (en) * 1946-03-18 1960-02-16 George A Garrett Radar search scan system
US2762041A (en) * 1950-09-09 1956-09-04 Motorola Inc Signalling equipment
US2677121A (en) * 1950-10-19 1954-04-27 Pyle National Co Combination warning light and stationary headlight
US2811719A (en) * 1953-04-28 1957-10-29 Henry W Wallace Double-universal nod mechanism
DE1010122B (en) * 1955-03-10 1957-06-13 Gen Electric Arrangement for the mechanical pivoting of a member to achieve a straight or circular scanning movement
US2916739A (en) * 1955-07-28 1959-12-08 Underwood Corp Scanner for antenna system
US3166750A (en) * 1961-02-14 1965-01-19 Raytheon Co Antenna intersecting-orthogonal-axes gimbal mount utilizing rotary bearings for two axes and push-pull linkage for third axis
US6100791A (en) * 1990-10-04 2000-08-08 Federal Signal Corporation Programmable emergency signalling device and system
US5422623A (en) * 1990-10-04 1995-06-06 Federal Signal Corporation Programmable emergency signalling device and system
EP2549585A1 (en) * 2011-07-21 2013-01-23 Harris Corporation Systems for positioning reflectors, such as passive reflectors
US9054409B2 (en) 2011-07-21 2015-06-09 Harris Corporation Systems for positioning reflectors, such as passive reflectors
US9281560B2 (en) 2011-07-21 2016-03-08 Harris Corporation Systems for positioning reflectors, such as passive reflectors
US9368867B2 (en) 2013-10-07 2016-06-14 Harris Corporation Near-linear drive systems for positioning reflectors
US9912052B2 (en) 2013-10-07 2018-03-06 Harris Corporation Near-linear drive systems for positioning reflectors
US20170216998A1 (en) * 2014-08-06 2017-08-03 C.M.S. S.P.A. System for supporting a workpiece
US10562157B2 (en) * 2014-08-06 2020-02-18 C.M.S. S.P.A. System for supporting a workpiece
DE102020102576A1 (en) 2020-02-03 2021-08-05 Neura Robotics GmbH Device for detecting the position and / or speed of objects in space

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