GB1015368A - Collapsible rod like bodies - Google Patents

Collapsible rod like bodies

Info

Publication number
GB1015368A
GB1015368A GB3063963A GB3063963A GB1015368A GB 1015368 A GB1015368 A GB 1015368A GB 3063963 A GB3063963 A GB 3063963A GB 3063963 A GB3063963 A GB 3063963A GB 1015368 A GB1015368 A GB 1015368A
Authority
GB
United Kingdom
Prior art keywords
parts
bodies
rod
folded
helix
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB3063963A
Inventor
Kenneth Bullough
Arnold Bradley
George Alan Francis Jenkins
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
National Research Development Corp UK
Original Assignee
National Research Development Corp UK
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 National Research Development Corp UK filed Critical National Research Development Corp UK
Priority to GB3063963A priority Critical patent/GB1015368A/en
Publication of GB1015368A publication Critical patent/GB1015368A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/08Means for collapsing antennas or parts thereof

Landscapes

  • Aerials With Secondary Devices (AREA)

Abstract

1,015,368. Aerials. NATIONAL RESEARCH DEVELOPMENT CORPORATION. July 31, 1964 [Aug. 1, 1963], No. 30639/63. Heading H4A. A foldable rod-like body comprises a helix 15, Fig. 1, of closely wound square section spring steel wire fitting closely within and secured to the adjacent ends of two tubular parts 11, 12 (which may be of stainless steel and aluminium respectively and copper plated for improved electrical conductivity) whose spacing apart is such that the length 10 of helix between them is sufficient to permit the parts to be folded together and also to spring substantially into line when released, As described, anchors 13, 14 are held within parts 11, 12 by crimping and serve as abutments for the ends of helix 15. They have lugs 17, 18 extending within the helix carrying pins 19, 21 between which a tension spring 22 is stretched, so holding the parts together and increasing the restoring force when they are folded. A bell-mouthed sleeve 23 lapped over the joint in the unfolded position holds the parts 11, 12 positively in line. It may be pushed back, for folding the parts, against a compression spring 24 which abuts at its other end against a collar 25 fixed to part 12 by a rivet 26. The forward movement of sleeve 21 is restricted either by outwardly tapering part 11 or by providing a positive stop. As applied to an aerial system which may be accommodated in the nose cone of a high altitude rocket, a Langmuir probe 31 may be fitted at the extremity of the body and be connected by a coaxial cable 32 secured by a grub screw 38 with hard rubber button 39, and passing inside the body. Towards the other end of the body the cable is secured to a slidable member 35 by a grub screw 36 and button 37 and is tensioned by a compression spring 34 abutting against another anchor 33, that anchor and anchors 13, 14, being provided with clearance holes for the cable. An external mounting flange 41 is welded to the outside of part 11. A complete system, Fig. 3 (not shown) may comprise three dipoles mounted at rightangles, i.e., one extending axially comprising the rod-like body 42 having one joint 43 and, in association with it, the shell of the rocket, and two dipoles each with two rod-like bodies 44 having two joints 45, 46. The extremities of the rod-like bodies in their folded positions are held by nylon cords 47, Fig. 4 (not shown), each of which is wound on a section of a drum, Fig. 5 (not shown) provided with flanges and a surrounding slotted cylinder. The shaft of the drum is extended on one side and squared for a winding key, and extended on the other side to carry a copper ratchet wheel positioned in the gap of a permanent magnet, for providing eddy-current braking, and held by a pawl which may be released at the proper time. Neoprene protective sleeves 58, Fig. 4, fitting over the metal sleeves associated with joints 46 may actuate microswitch indicators when rod-like bodies 44 are fully extended and other microswitches may be provided to indicate the folded and unfolded positions of all aerial members. The centre joint sleeves may be protected with rubber grommets. The various parts may be mounted on a base 55 made from paper or fabric laminations impregnated with synthetic resin and slots 59, 61 therein may receive the extremities of bodies 42, 44 when folded.
GB3063963A 1963-08-01 1963-08-01 Collapsible rod like bodies Expired GB1015368A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3063963A GB1015368A (en) 1963-08-01 1963-08-01 Collapsible rod like bodies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3063963A GB1015368A (en) 1963-08-01 1963-08-01 Collapsible rod like bodies

Publications (1)

Publication Number Publication Date
GB1015368A true GB1015368A (en) 1965-12-31

Family

ID=10310774

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3063963A Expired GB1015368A (en) 1963-08-01 1963-08-01 Collapsible rod like bodies

Country Status (1)

Country Link
GB (1) GB1015368A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0666613A1 (en) * 1994-02-04 1995-08-09 Orbital Sciences Corporation Axially arrayed helical antenna
CN106121350A (en) * 2016-06-29 2016-11-16 德清天盛轻工工艺制品有限公司 Fold flagpole

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0666613A1 (en) * 1994-02-04 1995-08-09 Orbital Sciences Corporation Axially arrayed helical antenna
US5587719A (en) * 1994-02-04 1996-12-24 Orbital Sciences Corporation Axially arrayed helical antenna
CN106121350A (en) * 2016-06-29 2016-11-16 德清天盛轻工工艺制品有限公司 Fold flagpole

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