US1517602A - Antenna safety link - Google Patents
Antenna safety link Download PDFInfo
- Publication number
- US1517602A US1517602A US400255A US40025520A US1517602A US 1517602 A US1517602 A US 1517602A US 400255 A US400255 A US 400255A US 40025520 A US40025520 A US 40025520A US 1517602 A US1517602 A US 1517602A
- Authority
- US
- United States
- Prior art keywords
- antenna
- link
- safety link
- halliard
- safety
- 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 - Lifetime
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/14—Supports; Mounting means for wire or other non-rigid radiating elements
- H01Q1/16—Strainers, spreaders, or spacers
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/39—Cord and rope holders
Landscapes
- Support Of Aerials (AREA)
- Details Of Aerials (AREA)
Description
Dec. 2, 192 1,517,602
A. M. TROGNER ANTENNA SAFETY LINK Filed July 50. 1920 @flrthvr 01%. {Fro ner Patented flee. 2, 1.924.
ARTHUR M. TROGNER, OF TAKOMA MARYLAND.
ANTENNA SAFETY LINK.
Al i lication filed m 2.0, 1920.
To all whom it may concern:
Be it known. that I, ARTHUR M. Tnoennn, a citizen of the United States, residing at Takoma Park, in the county of Montgomery and State of Maryland, have invented certain new and useful Improvements in .z-iir tenna Safety Links. of which the following is a specification.
My invention relates to antenna. safety links and has for an object to prevent the carrying away of the antenna as the result of an abnormal whipping of the masts, such as happens in cases of collision, torpedoing, grounding, etc.
A further object of my invention is to provide means whereby the antenna will be automatically slacked off upon receiving an excessive stress.
A still further object of my invention is to provide means by which the antenna, after having been automatically slacked oil, may be easily and quickly returned to its normal position.
A further object of the invention is to provide suitable means by which the antenna may be originally hoisted into position without subjecting the safety link to stress.
In cases where a vessel is torpedoed, is in collision, or is otherwise subjected to a severe shock, there often results a whipping of the masts to such a degree that the an tenna is carried away, thereby putting the radio apparatus out of operation at a time when it is most needed. My invention, generally stated, consists in inserting a safety link between the antenna and the mast at one or both ends; the link being so constructed that upon receiving a severe stress it will give away and automatically slack off the antenna thereby relieving the stress and preventing the carrying away of the antenna.
I will now proceed to describe in detail the construction by which the above and other objects are attained, reference being had to the accompanying drawings in which:
Fig. 1 is a perspective view of the complete apparatus assembed, showing a safety link at each end of the antenna.
Fig. 2 is a side elevation, on an enlarged. scale, of the safety link shown in Fig. 1, and
Fig. 3 is a side elevation of a modified. form of safety link.
flerial N. 400,255.
Between the masts 1, the usual antenna 2 extends, which antenna is attached to the masts in any suitable manner through a safety link referred to generally by the numeral 8.
The link 8 has weakened portion t therein, which is of sutficient strength to support the antenna under normal conditions but which will give away when subjected to abnormal stresses. The weakened portion is here shown as a single antenna wire but it will be obvious, of course,- that any other equivalent means may be substituted tor that which I have shown, it being merely necessary to provide some means by which the antenna is normally supported and which will automatically release the antenna when subjected to any undue stress.
As shown in Figures 1 and 2, halliards 5 pass over blocks 6 and are secured to the antenna by means of thimbles 7 or any other desired means. The antenna is hoisted into position by these halliards and it is then shackled to the masts by means of shackes 8. After shackling the antenna bight 9 of suitable length is taken in the halliard, which bight, if desired, may be lightly seized to the safety link as indicated at 10, 10. The halliards are now made fast on deck. It will be obvious that in this construction the safety link will not receive any stress when the antenna is originally hoisted into position.
The operat on of the apparatus disclosed in Figures and 2 is as follows:
The antenna is normally carried shown. Now, if the vessel receives any sudden shock which causes a whipping of the masts, the antenna will not be brought down but. one or both of the weakened portions 4- may be ruptured as a result of the stress on the antenna. When this happens the weight of the antenna will be received by the halliard 5, the seizing will carry away and the an.- tenna will be slacked ofi" to the extent of one or both bights depending upon whether one or both safety links are ruptured. By means of the halliard or halliards the antenna may be immediately hoisted back to its normal position so that there will be no decrease in the signalling range.
In the modified form of the invention shown in Figure 3, the halliard. 5 after pass ing over the block 6 is secured to the safety link instead of being secured to the antenna as in Figures 1 and 2.
A. rope or cable ll of? the desired length secured at one end, 12, to the antenna, and at the other end, 13 t0 the halliard. The intermediate portion may be coiled and seized as previously described.
The operation of this form of ratns similar to that off the in'e'lierred tor-in previously described. In this ease, however, it is impossible to immediately hoist the antenna back to its normal position after the safety link has been ruptured.
lVhile I have shown a safety link at both ends of the antenna this i s not essential and l 111a,; prefer to use only one link.
lflaving fully described my invention, What I claim as new and desire to secure by Letters Patent is:
1. A radio antenna having a sat'etx link with a weakened portion therein attached to one end, a halliard attached to the same end said link being adapted for suspending the antenna. from its masts but independent of the halli'ard.
2. A. radio antenna, a safety link for attaching the antenna to a mast, said link adapted to be ruptured when subjected to the appaan unusual stress, and a halliard attache-cl to the antenna, said halliard having abigliit; therein, whereby the antenna is slacked oll' after said link has been ruptured.
3. A radio antenna, means attaching the antenna to its support, said means adapted to release the antenna when subjected to an abnormal stress, and a halliard for supporting the antenna after it has been released by the first named means, and for returning the antenna to its normal position.
at. A radio antenna, a safety link having a Weaiened portion therein adapted to! rupture connected to the antenna and a mast, and a halliard also connecterfl to the antenna and the mast adjacent to the points 01'? connection of the link to maintain the antenna in operative position when the weakened portion is ruptured.
An antenna, a rupturahle means for attaching the antenna to a mast and a means "for receiving the weight upon rupture oi the first said means and by which the antenna is restored to its original position.
ARTHUR M. 'lllQUNICH.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US400255A US1517602A (en) | 1920-07-30 | 1920-07-30 | Antenna safety link |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US400255A US1517602A (en) | 1920-07-30 | 1920-07-30 | Antenna safety link |
Publications (1)
Publication Number | Publication Date |
---|---|
US1517602A true US1517602A (en) | 1924-12-02 |
Family
ID=23582852
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US400255A Expired - Lifetime US1517602A (en) | 1920-07-30 | 1920-07-30 | Antenna safety link |
Country Status (1)
Country | Link |
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US (1) | US1517602A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2499709A (en) * | 1946-04-19 | 1950-03-07 | George L Whitman | Service line with rupturable connector |
US3040329A (en) * | 1959-07-20 | 1962-06-26 | Bullard Co | Safety hat suspension harness |
US3121137A (en) * | 1961-04-13 | 1964-02-11 | British Insulated Callenders | Means for rupturing a thermocouple cable at a predetermined load |
US3809800A (en) * | 1973-04-25 | 1974-05-07 | Nasa | Means for accommodating large overstrain in lead wires |
US4409429A (en) * | 1981-06-16 | 1983-10-11 | Bernard Gaylard | Overhead electric transmission or distribution system |
US20090049661A1 (en) * | 2007-08-24 | 2009-02-26 | Harmon Darren L | Retainer for overmolded electrical circuit |
RU2594289C1 (en) * | 2015-03-26 | 2016-08-10 | Открытое акционерное общество "Омский научно-исследовательский институт приборостроения" (ОАО "ОНИИП") | Device for tensioning antenna beams |
-
1920
- 1920-07-30 US US400255A patent/US1517602A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2499709A (en) * | 1946-04-19 | 1950-03-07 | George L Whitman | Service line with rupturable connector |
US3040329A (en) * | 1959-07-20 | 1962-06-26 | Bullard Co | Safety hat suspension harness |
US3121137A (en) * | 1961-04-13 | 1964-02-11 | British Insulated Callenders | Means for rupturing a thermocouple cable at a predetermined load |
US3809800A (en) * | 1973-04-25 | 1974-05-07 | Nasa | Means for accommodating large overstrain in lead wires |
US4409429A (en) * | 1981-06-16 | 1983-10-11 | Bernard Gaylard | Overhead electric transmission or distribution system |
US20090049661A1 (en) * | 2007-08-24 | 2009-02-26 | Harmon Darren L | Retainer for overmolded electrical circuit |
US7963006B2 (en) * | 2007-08-24 | 2011-06-21 | Grote Industries, Inc. | Retainer for overmolded electrical circuit |
US20110223797A1 (en) * | 2007-08-24 | 2011-09-15 | Harmon Darren L | Retainer for overmolded electrical circuit |
US8272896B2 (en) | 2007-08-24 | 2012-09-25 | Grote Industries, Inc. | Retainer for overmolded electrical circuit |
RU2594289C1 (en) * | 2015-03-26 | 2016-08-10 | Открытое акционерное общество "Омский научно-исследовательский институт приборостроения" (ОАО "ОНИИП") | Device for tensioning antenna beams |
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