WO1991009434A1 - A corner reflector for use in a radar balloon - Google Patents

A corner reflector for use in a radar balloon Download PDF

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Publication number
WO1991009434A1
WO1991009434A1 PCT/NO1989/000129 NO8900129W WO9109434A1 WO 1991009434 A1 WO1991009434 A1 WO 1991009434A1 NO 8900129 W NO8900129 W NO 8900129W WO 9109434 A1 WO9109434 A1 WO 9109434A1
Authority
WO
WIPO (PCT)
Prior art keywords
balloon
reflector
stated
corners
frame system
Prior art date
Application number
PCT/NO1989/000129
Other languages
English (en)
French (fr)
Inventor
Oddvar Bjordal
Haakon Fykse
Original Assignee
Baco Industrier A/S
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Baco Industrier A/S filed Critical Baco Industrier A/S
Priority to AU46659/89A priority Critical patent/AU645743B2/en
Priority to JP90501160A priority patent/JPH05503610A/ja
Priority to FI922692A priority patent/FI922692A0/fi
Publication of WO1991009434A1 publication Critical patent/WO1991009434A1/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • H01Q15/18Reflecting surfaces; Equivalent structures comprising plurality of mutually inclined plane surfaces, e.g. corner reflector
    • H01Q15/20Collapsible reflectors

Definitions

  • the present Invention relates to a corner reflector for us in a radar balloon, especially for use In measuring meteoro logical parameters, furthermore, for use as a radar marker e.g. in life-saving service and for other objects.
  • a radar balloon should provide the best possible reflection at the same time as it should use a small volume of gas. Th principle of placing a corner reflector in a balloon i previously known, as mentioned, but it was difficult to hav the reflector fully expanded. Especially, in case o deviation from the orthogonality of various planes, efficien reflection is reduced. Expansion of the balloon when it i filled, or in connection with its ascent in the atmospher according to known technology, may deform the reflector, an cause high mechanical loads on the structure, especially i case of meteorological balloons, which are also subjected t great variations of temperature. A freely rotating balloo may remain in a position with one plane almost in paralle with the radar beam and may, thus, provide bad or even zer reflection. A corner reflector with eight internal corner will always have half of the internal corners positioned i radar shadow.
  • Th invention is based on a reflector in which the reflectin plane is suspended from a cord frame system of substantiall non-elastic cords which at the same time defines the angl between planes and distends the radar reflector in the shap of a reflecting net, a cloth, a sheet, or the like, hereafte called a sheet.
  • the present invention relates to a corne reflector to be suspended in a radar balloon, and th invention is characterized by the fact that the reflector i formed by a distended, substantially non-elastic cord fram system with a reflecting sheet attached to the same, so tha all three orthogonal planes are only in physical contact, vi the cord frame system, and the the external nodes at the sam time serve as suspension points.
  • the invention also relates to a balloon of a flexibl material for internal suspension of the above disclose corner reflector, which is characterized by the fact that i has at least the same number of corners as the reflector and that they may be directly secured to the reflector t distend the reflector corners in case of gas filling an expansion.
  • the cord frame system is expande by the balloon.
  • Each sheet member is in principle separate from the other sheet members and from the balloon cloth to b freely suspended, so that no friction will occur due t lateral forces, which might destroy the angle between variou planes.
  • the shape of the reflector is only to a very smal degree influenced by variations in the tensional load fro the balloon if the tensional load exceeds a certain minimum
  • An additional sheet area may be extended beyond the oute edges of the cord frame system by the aid of lightweigh stays or profiles resting or balancing on the distended cor frame system and on the sheet.
  • a reflector used as a radar marker in- life-saving service o as a dummy target for civil or military purposes, should hav 8 internal corners to be able to reflect incident radiatio from all arbitrary directions.
  • a reflector to be used for meteorological purposes need no have more than four internal corners, since the reflector ca be orientated by suitable means to make the same side alway face downwards.
  • a balloon of the present kind is, preferably, made fro single, if desired, combined webs of a resilient gastigh cloth, sheet or the like, here called sheet.
  • the shape of the web is selected to permit the reflector t fill a finished inflated ballon as much as possible, and t permit the reflector to be suspended at the corners.
  • One of the attachment points may in this connection preferably, be combined with a valve/filler neck.
  • Attachment at the corners provides for rapid distension o the reflector and utilizes the resiliency of part of th balloon cloth which is not otherwise subjected to grea elastic loads.
  • Balloons which are intended for great heights may be provide with cords or the like which will adjust the expansion volum to begin with. It will, thus, be possible to achiev sufficient pressure in the balloon to distend the reflecto from the start.
  • meteorolo gical balloons it may be desirable in case of meteorolo gical balloons to ensure permanent orientation in a certai direction. This may, e.g. be achieved by the aid of a weight if desired in the shape of a probe wich is suspended belo the balloon, e.g. for registration of temperature an moisture.
  • Figures 1-3 show sheet members for the reflector with cords in a dashed line;
  • Figure 4 shows a completed reflector;
  • Figure 5 shows a distension of the reflector area;
  • Figure 6 shows a continuous and unfolded blank for a balloon;
  • Figure 7 shows the same blank in a partly folded and welded design;
  • Figure 8 shows a finished balloon with reflector and probe;
  • Figures 8 and 10 show variants of the balloon cloth in
  • Figure 7 shows a variant of the square marked ghij in
  • Figure 6; and Figures 12 and 13 show a balloon blank for a reflector having eight internal corners.
  • the reflector is suspended in a substantiall non-elastic cord frame system which clearly defines th positions of three orthogonally intersecting planes, and i in principle provided with the reflecting sheet, so that eac plane adjusts quite freely in relation to the other plane and in a direction which is predetermined by the cord fram system.
  • the cords may at the same time be used to tensio each of the planes.
  • the reflecting sheet of a corner reflector according to th invention must show sufficient conductivity to provide thre separate reflections. Characteristically, a 0.003 m aluminium sheet at 9 GHz will provide approximately 0.9 time what is achievable by the aid of a thicker sheet, wherea 0.0005 mm provides 0.08 times what is theoretically achiev able.
  • Cords 2 may be secured in place on sheet members while th latter lie flat. Further mounting comprises connecting th cords from various members at the corners.
  • both vertical planes are to form diagonals AC, and BD, respectively in 1.
  • At least one of said planes must be split along the line of intersection 6 between said two vertical planes for them to be freely tensioned in a right-angled manner.
  • the other vertical plane must be split at least sufficiently to permit cords 2 to be freely tensioned. Also, the cords should go in differently at points of intersection F/F' of both vertical planes, so that the cords may arrange them ⁇ selves freely.
  • a complete reflector, cf. Figure 4 is achieved when B i secured to B', D to D', C to C, A to .A*, and E to E'. Attachment of cords is essential to the invention, since th angle betwen planes i determined by the nodes. Outside th nodes the cords may be used to suspend the reflector.
  • Figure 4 shows a finished reflector in a distended state Before it is arranged in the balloon, the vertical planes m be folded by simple folds on triangles 3-5, so that point will sit towards the center of 1 and the remaining reflecto will be in parallel with 1.
  • Another variant of the reflector according to the inventio may be achieved by substituting triangle 3 in Figure 2 b corresponding members 4 and 5 in Figure 3. By placing a additional set of triangles in Figures 2 and 3 symmetricall to sheet 1, a reflector with eight internal corners i achieved.
  • the shape of members is not limited to the shape indicated i Figures 1-4, as long as orthogonality is maintained.
  • Figur 5 shows a possibility of increasing the active are when the distance between points of suspension is given. I stead of cutting the sheet along straight line HI, a stay is attached to the sheet, which will, in turn, balance o cord 2, so that an additional area GHI is achieved which i in the same plane with the remaining sheet 7.
  • the reflecto enlargement may be used along all external edges of th reflector, and one or a number of stays may also be use along each edge.
  • Another embodiment for enlarging the reflector area i achieved by stretching cords 2 by the aid of small frame close to the point of suspension.
  • Said frames will absor tension of the cords to ensure the same tension as If th cords had extended to their tie-up points.
  • the frames may b plates or frames with three or four corners.
  • An essential feature of the balloon according to the presen invention is that it consists of single and, if desired connected plane members of a resilient material, and that th edges to be secured to close the balloon have equal length in pairs, and that corners are shaped which may serve a points of attachment for the reflector.
  • Balloon corners may be attached directly to reflector corner so that the balloon corners are retracted when the balloo expands. In this manner the resiliency of the balloon clot may be utilized in an area which is not otherwise subjecte to great tensional loads due to expansion.
  • the shape of faces may be selected from manufacturin considerations, and based on the concept that the balloo should sit as tightly as possible around the reflector t reduce the utilized volume of gas.
  • a balloon of the same original shape as the reflector o Figure 4 may be manufactured from a running web of cloth, a shown in Figure 6.
  • Figure 7 shows the same cloth in a folded state along f'k' and, furthermore, welded along k'(l'/j').
  • the cloth may be folded in such a manner that pieces are cu for the balloon directly in the shape as shown in Figure 7.
  • Another possibility in case of difficulties in procurement o wide cloth, may be to let one or both squares g'h'i'j', and e'f'k'l' be manufactured separately to be welded to squar f'g'j'k' to form the shape as shown in Figure 7.
  • the reflector may be mounted in the balloon by providing plane folded reflector in the centre of square g'h'j'k' with reflector corners and securing cords facing the corners o the cloth.
  • E" will sit centrally on the square and is attached to k' by lifting e' and pulling k' to E" an oining.
  • Securing in k' may suitably be combined with securing valve/fillerm neck.
  • the balloon is finished tightly by e' being pulled to i' an f to h', followed by welding along g'(h'/f' )(i'/e' )-( '/I' )
  • Cords from the corner reflector may be attached to th balloon corners by binding, clamping, glueing, welding o attaching in another manner.
  • the cords there may, suitabl be provided with small sferes, knots or the like to facilit ate securing operations.
  • a distinctive feature is that the manufacturing operation maynly occurs in one plane.
  • FIG. 8 An inflated radar balloon with a probe, or a stabilizin weight 12, respectively, is shown in Figure 8. Afte inflation the balloon will look approximately like a spher with inwards curved points of attachment.
  • Variants of a cloth blank, as shown in Figure 7, is shown i Figures 9 and 10. Inter alia, they are advantageous in tha they are simple and may be manufactured from a narro straight running web.
  • square g'h'i'j' is reduce to a parallelogram g"h"i"j
  • parallelogram e'f'k'l' and g'f'k'j' are reduced to a square e'"f'"k''' 1'", and g" - f ' 'k” '1" '.
  • Manufacture of the balloon may b quite analogous with that of the cloth blanks in Figure 7 and for the rest similar variants are, obviously, true.
  • a balloon with eight internal reflector corners has si points of attachment.
  • the balloon may also be made symmetrical about a correspond ing plane of mirror symmetry, closer to what would otherwis be the corresponding square ghij .
  • the square may be replaced by a piec making the balloon blank symmetrical about a plane normal t the paper along line gj , as shown in Figure 12.

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aerials With Secondary Devices (AREA)
  • Optical Elements Other Than Lenses (AREA)
PCT/NO1989/000129 1988-07-13 1989-12-11 A corner reflector for use in a radar balloon WO1991009434A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
AU46659/89A AU645743B2 (en) 1989-12-11 1989-12-11 A corner reflector for use in a radar balloon
JP90501160A JPH05503610A (ja) 1989-12-11 1989-12-11 レーダ気球に使用するコーナレフレクタ
FI922692A FI922692A0 (fi) 1989-12-11 1989-12-11 Hoernreflektor foer anvaendning i en radarballong.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NO883124A NO165368C (no) 1988-07-13 1988-07-13 Hjoernereflektor til bruk i en radarballong.

Publications (1)

Publication Number Publication Date
WO1991009434A1 true WO1991009434A1 (en) 1991-06-27

Family

ID=19891068

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/NO1989/000129 WO1991009434A1 (en) 1988-07-13 1989-12-11 A corner reflector for use in a radar balloon

Country Status (3)

Country Link
EP (1) EP0504135A1 (enrdf_load_html_response)
NO (1) NO165368C (enrdf_load_html_response)
WO (1) WO1991009434A1 (enrdf_load_html_response)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0977308A1 (en) * 1997-06-30 2000-02-02 Harris Corporation Tensioned cord attachement of antenna reflector to inflated support structure

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO177620C (no) * 1993-06-25 1995-10-18 Forsvarets Forsknings Kraftkontrollerende oppheng for objekt i ballong

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463517A (en) * 1945-06-30 1949-03-08 Chromak Leon Air-borne corner reflector
US3276017A (en) * 1961-10-18 1966-09-27 Gen Mills Inc Inflatable support structure
EP0182274A2 (de) * 1984-11-13 1986-05-28 Laval, Marlene Aufblasbarer Radarreflektor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463517A (en) * 1945-06-30 1949-03-08 Chromak Leon Air-borne corner reflector
US3276017A (en) * 1961-10-18 1966-09-27 Gen Mills Inc Inflatable support structure
EP0182274A2 (de) * 1984-11-13 1986-05-28 Laval, Marlene Aufblasbarer Radarreflektor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0977308A1 (en) * 1997-06-30 2000-02-02 Harris Corporation Tensioned cord attachement of antenna reflector to inflated support structure

Also Published As

Publication number Publication date
EP0504135A1 (en) 1992-09-23
NO165368B (no) 1990-10-22
NO883124D0 (no) 1988-07-13
NO165368C (no) 1991-01-30
NO883124L (enrdf_load_html_response) 1990-02-05

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