GB1430304A - Flying machines - Google Patents
Flying machinesInfo
- 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
Links
- 239000012212 insulator Substances 0.000 abstract 2
- 101100234822 Caenorhabditis elegans ltd-1 gene Proteins 0.000 abstract 1
- 239000004020 conductor Substances 0.000 abstract 1
- 239000000835 fiber Substances 0.000 abstract 1
- 239000011152 fibreglass Substances 0.000 abstract 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Details Of Aerials (AREA)
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.
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 (4)
| 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 |
| RU2361775C1 (en) * | 2008-01-09 | 2009-07-20 | Общество с ограниченной ответственностью "Научно-производственное предприятие "ПРИМА" | Helicopter |
| GB2575974A (en) * | 2018-07-27 | 2020-02-05 | Airbus Operations Ltd | Aircraft landing |
-
1973
- 1973-03-17 GB GB1296373A patent/GB1430304A/en not_active Expired
Cited By (5)
| 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 |
| RU2361775C1 (en) * | 2008-01-09 | 2009-07-20 | Общество с ограниченной ответственностью "Научно-производственное предприятие "ПРИМА" | Helicopter |
| 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 |