US3176303A - Collapsible antenna with plurality of flexible reflector petals releasably retained - Google Patents

Collapsible antenna with plurality of flexible reflector petals releasably retained Download PDF

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Publication number
US3176303A
US3176303A US174776A US17477662A US3176303A US 3176303 A US3176303 A US 3176303A US 174776 A US174776 A US 174776A US 17477662 A US17477662 A US 17477662A US 3176303 A US3176303 A US 3176303A
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Prior art keywords
petals
reflector
antenna
releasably retained
collapsible antenna
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Expired - Lifetime
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US174776A
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Holland Herman
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Whittaker Corp
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Whittaker Corp
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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
    • H01Q15/161—Collapsible reflectors

Definitions

  • An antenna generally has a radiator or collector and a reflector.
  • the reflector is an element which ordinarily takes up more space than any other component of the antenna. It would be desirable to provide an antenna which has a reflector capable of being packaged in a Heretofore, no practical means has been provided to achieve this result.
  • This invention provides an antenna which employs a reflector consisting of a plurality of petals, each petal being made of a flexible material. Because of the resilient characteristic of the petals, the petals can be compacted to a relatively small area and maintained in this position by a retaining means. Release of the retaining means permits the petals to assume their respective original positions, thereby forming an operative reflector surface.
  • An object of the invention is to provide an antenna which is compact.
  • Another object of the invention is to provide an antenna having a reflector which can be collapsed into a compact position when not in use.
  • a further object of the invention is to provide an antenna which has a reflector capable of being collapsed when not in use, and, upon remote activation, can be expanded into an operative position.
  • a still further object of the invention is to provide a collapsible antenna which is simple in construction and 1 operation and at the same time, is reliable in operation.
  • FIGURE 1 is a showing of the reflector in a collapsed, compact condition.
  • FIGURE 2 is a side view of the antenna in an expanded condition.
  • FIGURE 3 is a front view of the antenna in the full open position.
  • FIGURE 4 is a sectional view of the antenna substantially on the line of AA of FIGURE 3, illustrating a form of locking means employed for maintaining the petals of the reflector in place.
  • FIGURE 1 A general showing of the antenna in the collapsed position is shown in FIGURE 1.
  • a mounting base 1 is provided to support the antenna structure generally shown at 2.
  • a radiator 3 with its associated support 4 is attached to the mounting base by suitable means and exthe total space taken up by the antenna.
  • Patented MarQ30, 196 5 tends in a longitudinal direction from the mounting base 1.
  • a plurality of petals 5 are attached to the mounting base by suitable means such as screws 6.
  • the respective petals 5 are made from a flexible material capable of being distorted and returning to an original position after the distorting means is removed. Any fiberglass or other reinforced plastic materials could be used.
  • a metal can also be used therein if it has a high modulus of elasticity. Fiberglass is especially good since it has an inherently low flexural modulus. Large deflections are possible with fiberglass materials without consequent permanent deformations occurring since the yield stress of fiberglass is close to its ultimate stress.
  • the respective petals 5 are bent over from their original poistion to form a cup-like structure around the collector means as shown in FIGURE 1, thereby decreasing The petals are restrained in this position by suitable retaining means.
  • a strap 7 is employed to retain the petals 5 in their flexed position.
  • the strap 7 is held in place relative to the petals 5 by a plurality of clips 8 attached to the petals 5.
  • the strap 7 itself is held in a locked position by a destructive link 9. Unless the link 9 is destroyed, the strap 7 serves to hold the petals 5 in their folded position.
  • the destructible link 9 can take any of a plurality of forms.
  • a squib could be provided wherein, by utilizing a remotely controlled actuating apparatus (not shown), the link 9 can be destroyed, whereby the flexed petals 5 spring out to their normal position and form an operative reflector surface.
  • a remotely actuated solenoid could also serve as the actuating means to release the latching means (not shown) linking the respective ends of the strap 7 together.
  • any type of well-known triggering mechanisms could be used to release the strap '7.
  • the surface area of the collapsed reflector necessarily is less than the surface area of the reflector in its open position.
  • the decrease in size of the reflector surface upon collapse is made possible by having the petals 5 overlap each other as is clearly shown in FIGURE 1.
  • the degree of overlap is necessarily proportionate to the decrease in the reflector surface area.
  • the open operative reflector surface can be parabolic, spherical, flat, or any other design, the operative form depending solely on how the respective petals 5 had been originally molded or preformed.
  • Locking means 10 are provided near the edge of each petal to maintain the individual petals 5 in a desired relationship.
  • One type of locking means 10 which could be employed is a complementary pair of permanent magnets, as is clearly shown in FIGURE 4.
  • a brace 11 is attached to a first edge of each petal 5 on its backside and includes an extension 12 which protrudes over the edge of the petal 5.
  • the extension 12 is formed in such a manner so as to provide a recessed area 13 to support a magnet.
  • a first magnet 14 having a recess 15 therein is inserted in the recessed area 13 of the extension 12 and attached thereto with a suitable adhesive.
  • the opposite edge of each petal has a second magnet 16 attached thereto by suitable adhesive means.
  • the second magnet 16 has a convex form which is capable of fitting snugly into the recess- '15 of the' adjoining first magnet 14.
  • The-magnets'14a1'1'd 16 are'aligned so as to match upwith each atnerwnenthereflectbfis in its fully opened position.
  • the attractive force between the respective pairs of magnets 14. and .16 serves toprevent separationf of-theindividual petals ".5 and helpsfto n'i'aintain he-prewarmined surface contour "of'flthe" reflectofriand provide .rim
  • the petal folding operation automatically stores energy in the form of material'flexural stress.
  • ltis'thisflexural j stress energy which 'isjutilized” to ac'c'o'mplish'the im- "flding action.
  • v f' the necessity'bf including withflthe antennava'ric'm's mechaanisms; control" devices; or ether extraneousf liar'dv'vare to effectthe expansion'of'the reflector.
  • the onl 'power necessary to expand the reflectoris'thatffenergynecesfsary to trigger the release, ofthe' link 9'holdingf'the ends of the"strap"7 together.
  • the reflector assembly-set forth in claim 12 including clockingm'eans'for rnaintaining thexpetals-in an aligned position .whilein anunflexed' state. i I 3.
  • the reflector 'assembly'set fo'rth1in claim 2 wherein J said locking means are: permanent magnets.

Description

March 30, 1965 H. HOLLAND 3,176,303
COLLAPSIBLE ANTENNA WITH PLURALITY 0F FLEXIBLE REFLECTOR PETALS RELEASABLY RETAINED Filed Feb. 21, 1962 -2 Sheets-Sheet l Fl G. 2.
INVENTOR HERMAN HOLLAND M r 1965 H. HOLLAND 3,176,303
COLLAPSIBLE ANTENNA WITH PLURALITY OF FLEXIBLE REFLECTOR PETALS RELEASABLY RETAINED INVENTOR. H ERM AN HOLLAND United States Patent M ,COLLAPSELE ANTENNA WITH PLURALITY 0F This invention relates to a collapsible antenna and more particularly to an antenna which is maintained in a collapsed position, taking up a relatively small space, and, when needed, is rapidly expanded into operative position. I In present day space applications, a need exists to make everything which is to be carried aloft by a missile, such as the'components of a satellite, as lightweight and compact as possible. Any decrease in the weight of a device carried aloft will necessarily result in a corresponding increase in the payload capacity of the missile. The space within a satellite is also limited, and, accordingly, it is desirable to have all devices contained in the satellite in as compact a shape as possible.
Most satellites now include at least one antenna. An antenna generally has a radiator or collector and a reflector. The reflector is an element which ordinarily takes up more space than any other component of the antenna. It would be desirable to provide an antenna which has a reflector capable of being packaged in a Heretofore, no practical means has been provided to achieve this result.
This invention provides an antenna which employs a reflector consisting of a plurality of petals, each petal being made of a flexible material. Because of the resilient characteristic of the petals, the petals can be compacted to a relatively small area and maintained in this position by a retaining means. Release of the retaining means permits the petals to assume their respective original positions, thereby forming an operative reflector surface.
An object of the invention is to provide an antenna which is compact.
Another object of the invention is to provide an antenna having a reflector which can be collapsed into a compact position when not in use.
A further object of the invention is to provide an antenna which has a reflector capable of being collapsed when not in use, and, upon remote activation, can be expanded into an operative position.
A still further object of the invention is to provide a collapsible antenna which is simple in construction and 1 operation and at the same time, is reliable in operation.
Other objects and advantages will be apparent from the detailed description of the invention and from the appended drawings and claims.
In the drawings:
FIGURE 1 is a showing of the reflector in a collapsed, compact condition.
FIGURE 2 is a side view of the antenna in an expanded condition.
FIGURE 3 is a front view of the antenna in the full open position.
FIGURE 4 is a sectional view of the antenna substantially on the line of AA of FIGURE 3, illustrating a form of locking means employed for maintaining the petals of the reflector in place.
A general showing of the antenna in the collapsed position is shown in FIGURE 1. A mounting base 1 is provided to support the antenna structure generally shown at 2. A radiator 3 with its associated support 4 is attached to the mounting base by suitable means and exthe total space taken up by the antenna.
3,375,33 Patented MarQ30, 196 5 tends in a longitudinal direction from the mounting base 1. A plurality of petals 5 are attached to the mounting base by suitable means such as screws 6. The respective petals 5 are made from a flexible material capable of being distorted and returning to an original position after the distorting means is removed. Any fiberglass or other reinforced plastic materials could be used. A metal can also be used therein if it has a high modulus of elasticity. Fiberglass is especially good since it has an inherently low flexural modulus. Large deflections are possible with fiberglass materials without consequent permanent deformations occurring since the yield stress of fiberglass is close to its ultimate stress.
The respective petals 5 are bent over from their original poistion to form a cup-like structure around the collector means as shown in FIGURE 1, thereby decreasing The petals are restrained in this position by suitable retaining means. In this embodiment, a strap 7 is employed to retain the petals 5 in their flexed position. The strap 7 is held in place relative to the petals 5 by a plurality of clips 8 attached to the petals 5. The strap 7 itself is held in a locked position by a destructive link 9. Unless the link 9 is destroyed, the strap 7 serves to hold the petals 5 in their folded position.
The destructible link 9 can take any of a plurality of forms. A squib could be provided wherein, by utilizing a remotely controlled actuating apparatus (not shown), the link 9 can be destroyed, whereby the flexed petals 5 spring out to their normal position and form an operative reflector surface.
A remotely actuated solenoid could also serve as the actuating means to release the latching means (not shown) linking the respective ends of the strap 7 together. In fact, any type of well-known triggering mechanisms could be used to release the strap '7.
The surface area of the collapsed reflector, shown in FIGURE 1, necessarily is less than the surface area of the reflector in its open position. The decrease in size of the reflector surface upon collapse is made possible by having the petals 5 overlap each other as is clearly shown in FIGURE 1. The degree of overlap is necessarily proportionate to the decrease in the reflector surface area.
Release of the strap retainer 7 upon activation of the destructible link 9 results in the petals 5 snapping out into their operative position. An important feature of the invention resides in the fact that the energy for expanding the collapsed reflector structure is inherently contained in the reflector structure itself. The energy is stored up in the flexed petals 5 and this energy alone is used to expand the reflector structure. The open operative reflector surface can be parabolic, spherical, flat, or any other design, the operative form depending solely on how the respective petals 5 had been originally molded or preformed.
Locking means 10 are provided near the edge of each petal to maintain the individual petals 5 in a desired relationship. One type of locking means 10 which could be employed is a complementary pair of permanent magnets, as is clearly shown in FIGURE 4. A brace 11 is attached to a first edge of each petal 5 on its backside and includes an extension 12 which protrudes over the edge of the petal 5. The extension 12 is formed in such a manner so as to provide a recessed area 13 to support a magnet. A first magnet 14 having a recess 15 therein is inserted in the recessed area 13 of the extension 12 and attached thereto with a suitable adhesive. The opposite edge of each petal has a second magnet 16 attached thereto by suitable adhesive means. The second magnet 16 has a convex form which is capable of fitting snugly into the recess- '15 of the' adjoining first magnet 14. The-magnets'14a1'1'd 16 are'aligned so as to match upwith each atnerwnenthereflectbfis in its fully opened position. The attractive force between the respective pairs of magnets 14. and .16 serves toprevent separationf of-theindividual petals ".5 and helpsfto n'i'aintain he-prewarmined surface contour "of'flthe" reflectofriand provide .rim
' stiffness ties.
Other and ditferenflocking'rheans,-?stich as'conipleme'ntary latching means could be used .vvithout departing from the scope'of the invention.
The petal folding operation automatically stores energy in the form of material'flexural stress. ltis'thisflexural j stress energy which 'isjutilized" to ac'c'o'mplish'the im- "flding action. v f' the necessity'bf including withflthe antennava'ric'm's mechaanisms; control" devices; or ether extraneousf liar'dv'vare to effectthe expansion'of'the reflector. The onl 'power necessary to expand the reflectoris'thatffenergynecesfsary to trigger the release, ofthe' link 9'holdingf'the ends of the"strap"7 together. Since'no extraneous structure "is necessary to jprovide' the-.mo tive'po wer for expanding the reflector, a: significant decrease in the overallflweight offthe 'antenna structu're results. The absence" of "com- 'plica'ted mechanisms r'esults'in'an increase in reliability" of thecantennag I Because fiberglass plastic el ectro -magnetic radiations, a metallic surfacefmust'be *pro'vidediif"thepetals"5. are made of fiberglass." This can be achieved by vapor'depositing, metal spraying, or. metalbonding gold; silver, copper orlalumi'nu'mdo the fiberglass petals '5, Of course, this would not be neces- Ifsary ifthe. petals'5 themselvesare constructed ,from'a flexible metal.
I Alth'ongh this inventionfhas been disclosed and 'illus- This energy"s"torage' capability [obviates materials' do f'not {reflect I trated with reference to particular,applications, the principlesjnvolved are susceptible ;of numerous, other applications which will be 'apparent'to persons skilled in the art. The invention is, therefore, to be limited only asindicated by the scope of the appended claims.
lIA collapsible "reflector assembly essentially compris- '-ing a basearnernber; a plurality-ofindependent petals at- 4 tached to said base member and extending radially-there- "10 from, each of said petals bein'g'com'posed of a flexible solid material, sa'idi petals in "anunflex'ed 'state being capable of p'resenting aunitary'feflector surface, releas-v able retainer means for holding said petals in a flexed, overlapping position, meansfor deactivating said retainer Jrnea'ns, 'whereby the energy" utilized to expand said reflector assembly issupplied-solely by the petals.
.2. The reflector assembly-set forth in claim 12 including clockingm'eans'for rnaintaining thexpetals-in an aligned position .whilein anunflexed' state. i I 3. The reflector 'assembly'set fo'rth1in claim 2= wherein J said locking means are: permanent magnets.
4. The'reflector'assem'bly set forth in" claim 1 wherein I. said relea's'abler'etainer 'meansare remotely activated.
. i iliefer'encesQGited by the Examiner '35 HERMANKARLSAALBACH, Primary Examiner.

Claims (1)

1. A COLLAPSIBLE REFLECTOR ASSEMBLY ESSENTIALLY COMPRISING A BASE MEMBER, A PLURALITY OF INDEPENDENT PETALS ATTACHED TO SAID BASE MEMBER AND EXTENDING RADIALLY THEREFROM EACH OF SAID PETALS BEING COMPOSED OF A FLEXIBLE SOLID MATERIAL, SAID PETALS IN AN UNFLEXED STATE BEING CAPABLE OF PRESENTING A UNITARY REFLECTOR SURFACE, A RELEASABLE RETAINER MEANS FOR HOLDING SAID PETALS IN A FLEXED, OVERLAPPING POSITION, MEANS FOR DEACTIVATING SAID RETAINER MEANS, WHEREBY THE ENERGY UTILIZED TO EXPAND SAID RELFECTOR ASSEMBLY IS SUPPLIED SOLELY BY THE PETALS.
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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3286259A (en) * 1964-04-30 1966-11-15 Goodyear Aerospace Corp Unfurlable reflector
US3456999A (en) * 1965-10-29 1969-07-22 Gerhard Hopp Periscope
US3496941A (en) * 1966-11-14 1970-02-24 David Clough Ketner Sun-bathers reflector device
FR2016447A1 (en) * 1968-08-27 1970-05-08 Telefunken Gmbh
US3540048A (en) * 1966-10-19 1970-11-10 Nasa Deep space-monitor communication satellite system
US4350412A (en) * 1980-04-07 1982-09-21 Georgia Tech Research Institute Fresnel spiral reflector and method for making same
EP0091343A1 (en) * 1982-04-02 1983-10-12 Thomson-Csf Inverse Cassegrain antenna for a multifunction radar
EP0286716A2 (en) * 1987-04-16 1988-10-19 CONTRAVES ITALIANA S.p.A. An antenna system for exoatmospheric missiles
US4862190A (en) * 1987-05-15 1989-08-29 Trw Inc. Deployable offset dish structure
US5198832A (en) * 1991-12-13 1993-03-30 Comtech Antenna Systems, Inc. Foldable reflector
EP0534110A1 (en) * 1991-09-27 1993-03-31 Hughes Aircraft Company Simplified spacecraft antenna reflector for stowage in confined envelopes
FR2777118A1 (en) * 1998-04-03 1999-10-08 Aerospatiale Satellite launched folded reflector antenna
US6625288B1 (en) * 2000-03-31 2003-09-23 Intel Corporation Collapsing paraboloid dish and method
EP1386838A1 (en) * 2002-07-31 2004-02-04 Astrium GmbH Deployable antenna reflector
US7557995B1 (en) 2006-07-11 2009-07-07 Itt Manufacturing Enterprises, Inc. Deployable telescope shade
US20100315306A1 (en) * 2009-06-12 2010-12-16 Strydesky Gregory L Segmented antenna reflector
WO2016011338A1 (en) * 2014-07-17 2016-01-21 Gatr Technologies, Inc. Foldable radio wave antenna
US9899743B2 (en) 2014-07-17 2018-02-20 Cubic Corporation Foldable radio wave antenna deployment apparatus for a satellite
US10153559B1 (en) * 2016-06-23 2018-12-11 Harris Corporation Modular center fed reflector antenna system
US10236590B1 (en) 2016-12-21 2019-03-19 The United States Of America, As Represented By The Secretary Of The Air Force Foldable segmented structure and deployable reflector antenna comprised thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1683270A (en) * 1923-08-25 1928-09-04 Taylor Marcia Estabrook Radiation receiving conductor
US2572430A (en) * 1946-05-17 1951-10-23 Breeze Corp Antenna structure
US2763002A (en) * 1951-06-30 1956-09-11 Bendix Aviat Corp Collapsible antenna
US2806134A (en) * 1949-08-27 1957-09-10 Tarcici Adnan Collapsible reflectors
US3064534A (en) * 1960-04-13 1962-11-20 United Aircraft Corp Reflector for space vehicle
US3109608A (en) * 1960-12-21 1963-11-05 Boehm Josef Vision skirt

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1683270A (en) * 1923-08-25 1928-09-04 Taylor Marcia Estabrook Radiation receiving conductor
US2572430A (en) * 1946-05-17 1951-10-23 Breeze Corp Antenna structure
US2806134A (en) * 1949-08-27 1957-09-10 Tarcici Adnan Collapsible reflectors
US2763002A (en) * 1951-06-30 1956-09-11 Bendix Aviat Corp Collapsible antenna
US3064534A (en) * 1960-04-13 1962-11-20 United Aircraft Corp Reflector for space vehicle
US3109608A (en) * 1960-12-21 1963-11-05 Boehm Josef Vision skirt

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3286259A (en) * 1964-04-30 1966-11-15 Goodyear Aerospace Corp Unfurlable reflector
US3456999A (en) * 1965-10-29 1969-07-22 Gerhard Hopp Periscope
US3540048A (en) * 1966-10-19 1970-11-10 Nasa Deep space-monitor communication satellite system
US3496941A (en) * 1966-11-14 1970-02-24 David Clough Ketner Sun-bathers reflector device
FR2016447A1 (en) * 1968-08-27 1970-05-08 Telefunken Gmbh
US4350412A (en) * 1980-04-07 1982-09-21 Georgia Tech Research Institute Fresnel spiral reflector and method for making same
EP0091343A1 (en) * 1982-04-02 1983-10-12 Thomson-Csf Inverse Cassegrain antenna for a multifunction radar
EP0286716A2 (en) * 1987-04-16 1988-10-19 CONTRAVES ITALIANA S.p.A. An antenna system for exoatmospheric missiles
EP0286716A3 (en) * 1987-04-16 1988-11-30 CONTRAVES ITALIANA S.p.A. An antenna system for exoatmospheric missiles
US4862190A (en) * 1987-05-15 1989-08-29 Trw Inc. Deployable offset dish structure
EP0534110A1 (en) * 1991-09-27 1993-03-31 Hughes Aircraft Company Simplified spacecraft antenna reflector for stowage in confined envelopes
US5198832A (en) * 1991-12-13 1993-03-30 Comtech Antenna Systems, Inc. Foldable reflector
FR2777118A1 (en) * 1998-04-03 1999-10-08 Aerospatiale Satellite launched folded reflector antenna
US6175341B1 (en) 1998-04-03 2001-01-16 Aerospatiale Societe Nationale Industrielle Elastically deformable antenna reflector for a spacecraft
US6625288B1 (en) * 2000-03-31 2003-09-23 Intel Corporation Collapsing paraboloid dish and method
EP1386838A1 (en) * 2002-07-31 2004-02-04 Astrium GmbH Deployable antenna reflector
US20040104861A1 (en) * 2002-07-31 2004-06-03 Manfred Schmid Deployable antenna reflector
US6930654B2 (en) 2002-07-31 2005-08-16 Astrium Gmbh Deployable antenna reflector
US7557995B1 (en) 2006-07-11 2009-07-07 Itt Manufacturing Enterprises, Inc. Deployable telescope shade
US20100315306A1 (en) * 2009-06-12 2010-12-16 Strydesky Gregory L Segmented antenna reflector
US8723752B2 (en) * 2009-06-12 2014-05-13 Gregory L. Strydesky Segmented antenna reflector
US20140225799A1 (en) * 2009-06-12 2014-08-14 Gregory L. Strydesky Segmented antenna reflector
WO2016011338A1 (en) * 2014-07-17 2016-01-21 Gatr Technologies, Inc. Foldable radio wave antenna
US9899743B2 (en) 2014-07-17 2018-02-20 Cubic Corporation Foldable radio wave antenna deployment apparatus for a satellite
US9960498B2 (en) 2014-07-17 2018-05-01 Cubic Corporation Foldable radio wave antenna
US10153559B1 (en) * 2016-06-23 2018-12-11 Harris Corporation Modular center fed reflector antenna system
US10236590B1 (en) 2016-12-21 2019-03-19 The United States Of America, As Represented By The Secretary Of The Air Force Foldable segmented structure and deployable reflector antenna comprised thereof

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