GB1430304A - Flying machines - Google Patents

Flying machines

Info

Publication number
GB1430304A
GB1430304A GB1296373A GB1296373A GB1430304A GB 1430304 A GB1430304 A GB 1430304A GB 1296373 A GB1296373 A GB 1296373A GB 1296373 A GB1296373 A GB 1296373A GB 1430304 A GB1430304 A GB 1430304A
Authority
GB
United Kingdom
Prior art keywords
skid
helicopter
main body
insulating
section
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
GB1296373A
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.)
Allard Way Holdings Ltd
Original Assignee
Elliott Brothers London Ltd
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 Elliott Brothers London Ltd filed Critical Elliott Brothers London Ltd
Priority to GB1296373A priority Critical patent/GB1430304A/en
Publication of GB1430304A publication Critical patent/GB1430304A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/28Adaptation for use in or on aircraft, missiles, satellites, or balloons

Abstract

1430304 Aerials ELLIOTT BROS (LONDON) Ltd 1 Feb 1974 [17 March 1973] 12963/73 Heading H4A The landing gear beneath a flying machine incorporates a skid or other extensive member of conductive material, said member being isolated at least at one end thereof from the main body of the machine and being fed at one point only by a feeder from or to transmitting or receiving equipment. As described, a helicopter has a landing gear which consists of two skids one of which, referenced 1, is visible in Fig. 1. Said skid is carried from the main body 2 of the helicopter by struts 3, 4 each of which has an interposed moulded fibre-glass section 5. A cable 7 is connected at one end to the strut 4 beyond the section 5 and at the other end via a stand-off insulator 8 to radio equipment inside the helicopter. The aerial provided by the skid may be extended, for example, by wires extending therefrom to insulators on the main body of the machine. The skid on the other side of the helicopter is insulated from the body 2 in the same way as is the skid 1, and it may either be left isolated or be associated with the skid 1 by means of a cross-connecting cable (9), Fig. 2 (not shown). In another embodiment, instead of providing the insulating sections 5 the struts are mounted in insulating fibre bushes (10), Fig. 3 (not shown), provided in the main body of the helicopter. Considering the arrangement shown in Fig. 1, it is stated that if the strut 3 is not provided with an insulating section 5, but is left as a continuous member from the skid 1 to the main body 2, an arrangement functioning as a so-called skeleton notch aerial will result.
GB1296373A 1973-03-17 1973-03-17 Flying machines Expired GB1430304A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1296373A GB1430304A (en) 1973-03-17 1973-03-17 Flying machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1296373A GB1430304A (en) 1973-03-17 1973-03-17 Flying machines

Publications (1)

Publication Number Publication Date
GB1430304A true GB1430304A (en) 1976-03-31

Family

ID=10014322

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1296373A Expired GB1430304A (en) 1973-03-17 1973-03-17 Flying machines

Country Status (1)

Country Link
GB (1) GB1430304A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4100546A (en) * 1977-01-28 1978-07-11 The United States Of America As Represented By The Secretary Of The Army Airborne antenna system employing the airframe as an antenna
US4117490A (en) * 1977-08-15 1978-09-26 The United States Of America As Represented By The Secretary Of The Army Inconspicuous antenna system employing the airframe as an antenna
GB2575974A (en) * 2018-07-27 2020-02-05 Airbus Operations Ltd Aircraft landing

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4100546A (en) * 1977-01-28 1978-07-11 The United States Of America As Represented By The Secretary Of The Army Airborne antenna system employing the airframe as an antenna
US4117490A (en) * 1977-08-15 1978-09-26 The United States Of America As Represented By The Secretary Of The Army Inconspicuous antenna system employing the airframe as an antenna
GB2575974A (en) * 2018-07-27 2020-02-05 Airbus Operations Ltd Aircraft landing
US11807390B2 (en) 2018-07-27 2023-11-07 Airbus Operations Limited Aircraft landing

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee