US2480181A - Directive high-frequency antenna - Google Patents

Directive high-frequency antenna Download PDF

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Publication number
US2480181A
US2480181A US574368A US57436845A US2480181A US 2480181 A US2480181 A US 2480181A US 574368 A US574368 A US 574368A US 57436845 A US57436845 A US 57436845A US 2480181 A US2480181 A US 2480181A
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Prior art keywords
slots
apertures
sleeve
guide
reflector
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Expired - Lifetime
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US574368A
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Stanley L Breen
Chu Lan Jen
Pao Chia-Shan
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United States, WAR, Secretary of
US SEC WAR
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US SEC WAR
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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
    • H01Q3/24Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching

Definitions

  • the present invention relates to an antenna for use in a high frequency communication system and is particularly directed to an antenna adapted to discontinuously scan portions of space.
  • the principal object of this invention is to provide an antenna which is ⁇ adapted to radiate electromagnetic waves of high frequency energy in a distribution pattern which shifts in discrete steps through a plurality of regions in space rather than scanning continuously.
  • Fig. 1 is a side elevation view, partly broken away, of one embodiment of an antenna according to the invention; with a circular wave guide,
  • diagram- Fig. 3 is a sectional view, partly broken away
  • a parabolic reflector is diagrammatically indicated at I ll in Fig. 1.
  • a circular hollow wave guide II mounted in front of reflector I is a circular hollow wave guide II, adapted to be excited by energy from a source (not shown), preferably in the TEM mode and polarized as indicated in Fig. 3. the arrows E representing the direction of the electric lines of force.
  • Wave guide II is generally disposed so thata plane tangential to its surface and perpendicular to the axis of reilector I0 passes through the focal point F of reflector Ill.
  • a plurality of slots are disposed inthe wave guide II and are symmetrically spaced about and near the focal point F. As shown more clearly in the exciting energy so that the slots are properly matched to space.
  • Energy from guide Il is adapted to be radiated from the respective slotstoward the reflector Ill from which it is reected into space in a directional manner.
  • a cylindrical sleeve or collar member I6 mounted coaxially relative to guide II.
  • Sleeve I6 surrounds the guide Il in closely tting relation thereto over a substantialportion of the length of the guide II.
  • Sleeve member I6 is rotatably mounted relative to guide Il in any suitable manner such as by a ball bearing raceway generally indicated at I1 in the broken away portion of Fig. 1. Any suitable means may be used for rotating sleeve IB about guide I I for example, a ring gear I8 may be mounted on the lower peripheral surface of sleeve I6 mating with gear Fig. 2.
  • guide II is provided preferably with four slots, l2, I3, I4 and I5, having their longitudinal axes parallel with the longitudinal axis of guide il. The length of each of the slots is generally a I9 and driven through shaft 20 by motor 2l.
  • vSleeve I6 is provided with a group of apertures or slots so disposed that only one of the apertures at a time will match or register with one of the slots in guide I I and the remaining slots in guide I I will be covered by the solid wall of cylindrical sleeve I6.
  • sleeve I6 is preferably provided with four apertures 22, 23, 24 and 25.
  • These apertures may be of any suitable dimensions, but preferably of substantially the same vertical dimensions as the length of the slots in guide Il.
  • apertures 22, 23, 24 and 25 are spaced symmetrically in sleeve I6 with the width of the apertures, 1n the illustrated example, being equal to about a 40 arc of the peripheral surface of cylindrical sleeve I6.
  • Apertures 12,2 and 24 are preferalznlyl disposed diametrically opposite to apertures 23 and 25 respectively, with adjacent apertures being disposed radially substantially 90 apart.
  • slots I2 and I3 and apertures 22 and 23 are located on one side of the axis of reiiector IIJ, and slots I4 and I 5 and apertures 24 and 25 are located on the opposite side of the reflector axis.
  • Aperture 23 is shown corresponding with, or in registry with, slot I3; thus permitting radiation of energy from slot I3 toward reilector I0,
  • the illustrated antenna having four radiating slots as shown, there are thus four separate paths of radiation adapted to be independently illuminated according to a predetermined sequence.
  • the radiation pattern of each individiual beam overlaps the radiation pattern of one or more of the other beams.
  • any desired sequence of radiation from the slots may be provided.
  • any desired scanning pattern may be obtained by the present invention merely by suitably arranging the slots in the wave guide Il and the apertures in the sleeve I6.
  • An antenna for use in a high frequency communication system comprising, in combination, a parabolic reflector, a hollow circular wave guide adapted to transmit high frequency electromagnetic energy mounted in front of said reflector so that a plane tangential to its surface and perpendicular to the axis of said reflector passes substantlally through the focal point thereof, a cy lindrical sleeve rotatably mounted in closely tting coaxial relation around said wave guide, said wave guide having a plurality of slots spaced symmetrically with reference to said focal point, the longitudinal axes 0f said slots being parallel with the longitudinal axis of said wave guide,
  • each said slot being substantially half the operating wavelength of the electromagnetic oscillations
  • said sleeve having a plurality of spaced apertures, and means for rotating said sleeve whereby said apertures are adapted to register successively with said slots in a predetermined sequence for permitting energy to be radiated from said slots one at a time, the remaining slots being closed and effectively shortcircuited by said sleeve, for thereby enabling said antenna to discontinuously scan in a distribution pattern which shifts in discrete steps through a plurality of regions in space.
  • An antenna as claimed in claim ,1 in which the wave guide is provided with four slots, said slots being spaced symmetrically with reference to the focal point of the reflector, two of said slots being parallel to each other on one side of the axis of said reflector, the other two of said slots being parallel to each other on the opposite side of the axis of said reflector, and in which the sleeve is provided with four apertures, the length of each aperture being substantially equal to the length of said slots and the width of each aperture-being substantially wider than the width of said slots, two of said apertures being located diametrically opposite each other and adapted to be rotated into registration with said rst-mentioned two slots, the other two of said apertures being located diametrically opposite each other and adapted to be rotated into registration with said second two slots.

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  • Aerials With Secondary Devices (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Description

Patented Aug. 30, 1949 DIRECTIVE HIGH-FREQUENCY ANTENNA Stanley L. Breen, Cambridge, Lan Jen Chu, Brookline, and, Chia-Shan Pao, Cambridge, Mass., asslgnors, by mesne assignments, to the United States of America as represented by the Secretary of War Application January 24, 1945, Serial No. 574,368
2 Claims. 1
The present invention relates to an antenna for use in a high frequency communication system and is particularly directed to an antenna adapted to discontinuously scan portions of space. Y
Accordingly,the principal object of this invention is to provide an antenna which is` adapted to radiate electromagnetic waves of high frequency energy in a distribution pattern which shifts in discrete steps through a plurality of regions in space rather than scanning continuously.
It is also an object -of the invention to obtain a discontinuous scan by providing a group of spaced radiating elements and means for radiating energy from one or more of the elements in a predetermined arrangement or sequencel to provide a variety of scanning patterns.
It is another object ofthe invention to provide an antenna adapted to discontinuously search a portion of space and which is economical to construct and easy to operate.
Dther objects and advantages of this invention will become apparent as the description proceeds, reference being made to the accompanying drawings in which:
Fig. 1 is a side elevation view, partly broken away, of one embodiment of an antenna according to the invention; with a circular wave guide,
and with a parabolic reflector shown diagram- Fig. 3 is a sectional view, partly broken away,
of said reflector taken on the line 3-3 of Fig. 2.
Referring to the drawings, a parabolic reflector is diagrammatically indicated at I ll in Fig. 1. Mounted in front of reflector I is a circular hollow wave guide II, adapted to be excited by energy from a source (not shown), preferably in the TEM mode and polarized as indicated in Fig. 3. the arrows E representing the direction of the electric lines of force. Wave guide II is generally disposed so thata plane tangential to its surface and perpendicular to the axis of reilector I0 passes through the focal point F of reflector Ill.
A plurality of slots are disposed inthe wave guide II and are symmetrically spaced about and near the focal point F. As shown more clearly in the exciting energy so that the slots are properly matched to space. Energy from guide Il is adapted to be radiated from the respective slotstoward the reflector Ill from which it is reected into space in a directional manner.
Mounted coaxially relative to guide II is a cylindrical sleeve or collar member I6. Sleeve I6 surrounds the guide Il in closely tting relation thereto over a substantialportion of the length of the guide II. Sleeve member I6 is rotatably mounted relative to guide Il in any suitable manner such as by a ball bearing raceway generally indicated at I1 in the broken away portion of Fig. 1. Any suitable means may be used for rotating sleeve IB about guide I I for example, a ring gear I8 may be mounted on the lower peripheral surface of sleeve I6 mating with gear Fig. 2. guide II is provided preferably with four slots, l2, I3, I4 and I5, having their longitudinal axes parallel with the longitudinal axis of guide il. The length of each of the slots is generally a I9 and driven through shaft 20 by motor 2l.
vSleeve I6 is provided with a group of apertures or slots so disposed that only one of the apertures at a time will match or register with one of the slots in guide I I and the remaining slots in guide I I will be covered by the solid wall of cylindrical sleeve I6. For example, when guide II is provided with four slots, l2, I3, I4 and I5, as referred to above, sleeve I6 is preferably provided with four apertures 22, 23, 24 and 25. These apertures may be of any suitable dimensions, but preferably of substantially the same vertical dimensions as the length of the slots in guide Il.
As shown more clearly in Figs. 2 and 3, apertures 22, 23, 24 and 25 are spaced symmetrically in sleeve I6 with the width of the apertures, 1n the illustrated example, being equal to about a 40 arc of the peripheral surface of cylindrical sleeve I6. Apertures 12,2 and 24 are preferalznlyl disposed diametrically opposite to apertures 23 and 25 respectively, with adjacent apertures being disposed radially substantially 90 apart.
As shown, slots I2 and I3 and apertures 22 and 23 are located on one side of the axis of reiiector IIJ, and slots I4 and I 5 and apertures 24 and 25 are located on the opposite side of the reflector axis. Aperture 23 is shown corresponding with, or in registry with, slot I3; thus permitting radiation of energy from slot I3 toward reilector I0,
the remaining slots being closed and effectively short-circuited by the solid wall of sleeve I6.
As sleeve I6 is rotated, for example in a clockwise direction (Fig. 3), aperture 23 moves out of registry with slot I3 and into registry with slot I2, slot I3 thereby being closed by the wall of sleeve I6. Continued rotation brings aperture 25 into registry with slot I5 and then slot I4, and
half wavelength of the operating wavelength of aperture 22 into registry with slots I3 and I2 a path of radiation which makes an angle with the axis of the reiiector. The size of the angle, of course, is proportional to the amount the radiating slot is displaced from the focal point F. 1n the illustrated antenna having four radiating slots as shown, there are thus four separate paths of radiation adapted to be independently illuminated according to a predetermined sequence. Preferably the radiation pattern of each individiual beam overlaps the radiation pattern of one or more of the other beams. Such a system provides a scanning action of the portion of space included within the composite pattern of radia-A tion.
. By suitable arrangement of the mentioned apertures and slots any desired sequence of radiation from the slots may be provided. Thus any desired scanning pattern may be obtained by the present invention merely by suitably arranging the slots in the wave guide Il and the apertures in the sleeve I6.
Thus it will be apparent that as radiation occurs rst from one slot and then from another according to a predetermined arrangement, energy is radiated in a distribution pattern which shifts from section to section in space in a discontinu- While an embodimentof the invention is illustrateclV herein, it will be .understood that many different arrangements of any number of radiating elements, i. e. slots, wave guides, horns, etc., are possible with. the present invention. The elements may be fed in series or parallel, as desired. Similarly'any predetermined sequences of illumination of the elements may be used.
We claim:
1. An antenna for use in a high frequency communication system comprising, in combination, a parabolic reflector, a hollow circular wave guide adapted to transmit high frequency electromagnetic energy mounted in front of said reflector so that a plane tangential to its surface and perpendicular to the axis of said reflector passes substantlally through the focal point thereof, a cy lindrical sleeve rotatably mounted in closely tting coaxial relation around said wave guide, said wave guide having a plurality of slots spaced symmetrically with reference to said focal point, the longitudinal axes 0f said slots being parallel with the longitudinal axis of said wave guide,
the length of each said slot being substantially half the operating wavelength of the electromagnetic oscillations, said sleeve having a plurality of spaced apertures, and means for rotating said sleeve whereby said apertures are adapted to register successively with said slots in a predetermined sequence for permitting energy to be radiated from said slots one at a time, the remaining slots being closed and effectively shortcircuited by said sleeve, for thereby enabling said antenna to discontinuously scan in a distribution pattern which shifts in discrete steps through a plurality of regions in space.
2. An antenna as claimed in claim ,1 in which the wave guide is provided with four slots, said slots being spaced symmetrically with reference to the focal point of the reflector, two of said slots being parallel to each other on one side of the axis of said reflector, the other two of said slots being parallel to each other on the opposite side of the axis of said reflector, and in which the sleeve is provided with four apertures, the length of each aperture being substantially equal to the length of said slots and the width of each aperture-being substantially wider than the width of said slots, two of said apertures being located diametrically opposite each other and adapted to be rotated into registration with said rst-mentioned two slots, the other two of said apertures being located diametrically opposite each other and adapted to be rotated into registration with said second two slots. 'f
STANLEY L BREEN.- LAN JEN CHU. CHIA-SHAN PAO.
REFERENCES CITED UNITED STATES PATENTS Number Name Date 2,002,181 Ilberg May 21, 1935 2,075,808 Fliess Apr. 6, 1937 2,082,347 Leib et al June 1, 1937 2,083,242 Runge s June 8, 1937 2,189,549 Hershberger Feb. 6, 1940 2,206,923 Southworth July 9, 1940 2,241,119 Dallenbach May 6, 1941 2,283,054 Gosse] May 12, 1942 2,396,044 Fox Mar. 5, 1946 2 415 242 Hershberger Feb. 4, 1947 2,415,807 Barrow et al. Feb. 18, 1947 2,436,380 Cutler Feb. 24, 1948 2,438,735 Alexanderson Mar. 30, 1948
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2571612A (en) * 1948-02-24 1951-10-16 Robert H Rines Stereoscopic image reception by millimetric radiation
US2601610A (en) * 1948-03-18 1952-06-24 Marconi Wireless Telegraph Co Radio aerial installation
US2648003A (en) * 1946-01-07 1953-08-04 Us Navy Vernier scanner
US2664560A (en) * 1949-12-01 1953-12-29 Sperry Corp Radio aid to navigation
US2670436A (en) * 1950-05-03 1954-02-23 Allen S Dunbar Helical slot scanner
US3040319A (en) * 1958-12-09 1962-06-19 Itt Beacon antenna system
US3377596A (en) * 1962-01-31 1968-04-09 Csf Slot antenna with programmed radiation pattern
US3916415A (en) * 1950-09-28 1975-10-28 Rca Corp Antenna scanning
DE3820920A1 (en) * 1988-03-31 1989-11-16 Franz Eisenhofer Antenna arrangement
EP2221921A1 (en) * 2009-02-20 2010-08-25 Vivant Medical, Inc. Leaky-wave antennas for medical applications
US20100217252A1 (en) * 2009-02-20 2010-08-26 Vivant Medical, Inc. Leaky-Wave Antennas for Medical Applications
JP2014531173A (en) * 2011-10-26 2014-11-20 アルカテル−ルーセント Distributed antenna system and method for manufacturing distributed antenna system
GB2553634A (en) * 2016-06-24 2018-03-14 Ford Global Tech Llc A multiple orientation antenna for vehicle communication
EP2258300B1 (en) * 2009-06-02 2018-10-17 Covidien LP Electrosurgical devices with directional radiation pattern

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2002181A (en) * 1930-10-29 1935-05-21 Telefunken Gmbh Transmitter
US2075808A (en) * 1930-11-21 1937-04-06 Robert A Fliess Method and apparatus for observing bodies through opaque substances
US2082347A (en) * 1932-11-29 1937-06-01 Telefunken Gmbh Radio direction system
US2083242A (en) * 1934-01-27 1937-06-08 Telefunken Gmbh Method of direction finding
US2189549A (en) * 1938-03-18 1940-02-06 Rca Corp Antenna switching system
US2206923A (en) * 1934-09-12 1940-07-09 American Telephone & Telegraph Short wave radio system
US2241119A (en) * 1936-09-15 1941-05-06 Pintsch Julius Kg Ultra-short-wave apparatus
US2283054A (en) * 1939-01-07 1942-05-12 Lorenz C Ag Directional transmitter
US2396044A (en) * 1941-12-10 1946-03-05 Bell Telephone Labor Inc Switching device
US2415242A (en) * 1943-02-25 1947-02-04 Rca Corp Switching in wave guide transmission system
US2415807A (en) * 1942-01-29 1947-02-18 Sperry Gyroscope Co Inc Directive electromagnetic radiator
US2436380A (en) * 1944-09-23 1948-02-24 Bell Telephone Labor Inc Rapid sweep radiating system
US2438735A (en) * 1944-10-02 1948-03-30 Gen Electric High-frequency wave transmitting apparatus

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2002181A (en) * 1930-10-29 1935-05-21 Telefunken Gmbh Transmitter
US2075808A (en) * 1930-11-21 1937-04-06 Robert A Fliess Method and apparatus for observing bodies through opaque substances
US2082347A (en) * 1932-11-29 1937-06-01 Telefunken Gmbh Radio direction system
US2083242A (en) * 1934-01-27 1937-06-08 Telefunken Gmbh Method of direction finding
US2206923A (en) * 1934-09-12 1940-07-09 American Telephone & Telegraph Short wave radio system
US2241119A (en) * 1936-09-15 1941-05-06 Pintsch Julius Kg Ultra-short-wave apparatus
US2189549A (en) * 1938-03-18 1940-02-06 Rca Corp Antenna switching system
US2283054A (en) * 1939-01-07 1942-05-12 Lorenz C Ag Directional transmitter
US2396044A (en) * 1941-12-10 1946-03-05 Bell Telephone Labor Inc Switching device
US2415807A (en) * 1942-01-29 1947-02-18 Sperry Gyroscope Co Inc Directive electromagnetic radiator
US2415242A (en) * 1943-02-25 1947-02-04 Rca Corp Switching in wave guide transmission system
US2436380A (en) * 1944-09-23 1948-02-24 Bell Telephone Labor Inc Rapid sweep radiating system
US2438735A (en) * 1944-10-02 1948-03-30 Gen Electric High-frequency wave transmitting apparatus

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2648003A (en) * 1946-01-07 1953-08-04 Us Navy Vernier scanner
US2571612A (en) * 1948-02-24 1951-10-16 Robert H Rines Stereoscopic image reception by millimetric radiation
US2601610A (en) * 1948-03-18 1952-06-24 Marconi Wireless Telegraph Co Radio aerial installation
US2664560A (en) * 1949-12-01 1953-12-29 Sperry Corp Radio aid to navigation
US2670436A (en) * 1950-05-03 1954-02-23 Allen S Dunbar Helical slot scanner
US3916415A (en) * 1950-09-28 1975-10-28 Rca Corp Antenna scanning
US3040319A (en) * 1958-12-09 1962-06-19 Itt Beacon antenna system
US3377596A (en) * 1962-01-31 1968-04-09 Csf Slot antenna with programmed radiation pattern
DE3820920A1 (en) * 1988-03-31 1989-11-16 Franz Eisenhofer Antenna arrangement
US8197473B2 (en) 2009-02-20 2012-06-12 Vivant Medical, Inc. Leaky-wave antennas for medical applications
US10080610B2 (en) * 2009-02-20 2018-09-25 Covidien Lp Leaky-wave antennas for medical applications
US20100217251A1 (en) * 2009-02-20 2010-08-26 Vivant Medical, Inc. Leaky-Wave Antennas for Medical Applications
EP2221921A1 (en) * 2009-02-20 2010-08-25 Vivant Medical, Inc. Leaky-wave antennas for medical applications
US8202270B2 (en) 2009-02-20 2012-06-19 Vivant Medical, Inc. Leaky-wave antennas for medical applications
US8608731B2 (en) 2009-02-20 2013-12-17 Covidien Lp Leaky-wave antennas for medical applications
US8679108B2 (en) 2009-02-20 2014-03-25 Covidien Lp Leaky-wave antennas for medical applications
US20100217252A1 (en) * 2009-02-20 2010-08-26 Vivant Medical, Inc. Leaky-Wave Antennas for Medical Applications
US8968292B2 (en) 2009-02-20 2015-03-03 Covidien Lp Leaky-wave antennas for medical applications
US20150164588A1 (en) * 2009-02-20 2015-06-18 Covidien Lp Leaky-wave antennas for medical applications
EP2258300B1 (en) * 2009-06-02 2018-10-17 Covidien LP Electrosurgical devices with directional radiation pattern
JP2014531173A (en) * 2011-10-26 2014-11-20 アルカテル−ルーセント Distributed antenna system and method for manufacturing distributed antenna system
US10249960B2 (en) 2011-10-26 2019-04-02 Alcatel Lucent Distributed antenna system and method of manufacturing a distributed antenna system
GB2553634A (en) * 2016-06-24 2018-03-14 Ford Global Tech Llc A multiple orientation antenna for vehicle communication
US10439275B2 (en) 2016-06-24 2019-10-08 Ford Global Technologies, Llc Multiple orientation antenna for vehicle communication

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