GB1331851A - Pylon for use with a tethered model aircraft - Google Patents
Pylon for use with a tethered model aircraftInfo
- Publication number
- GB1331851A GB1331851A GB1331851DA GB1331851A GB 1331851 A GB1331851 A GB 1331851A GB 1331851D A GB1331851D A GB 1331851DA GB 1331851 A GB1331851 A GB 1331851A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- wire
- lever
- shaft
- rotatable
- 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
Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/04—Captive toy aircraft
Abstract
1331851 Pylons for model aircraft MATTEL Inc 19 April 1971 [3 Feb 1970 29 Jan 1971] 5537/71 and 3467/71 Divided out of 1304441 Heading A6S A pylon 1 for use with a tethered model aircraft has one end of a wire 21 connected to a first member 18 rotatable about a shaft 16 and a lever 20 connected to the wire 21 and connected by a link 200 to a second member 14 axially slidable on the shaft 16 such that reciprocation of the second member 14 causes the lever 20 and hence the wire 21 to rotate about its axis to thereby, in use, transmit torque to a control member (e.g. an elevator 8 or a helicopter rotor) of the aircraft. The member 14 is reciprocable by means of a Bowden-type cable 7. The wire 21 passes through a post 19 on the first member 18 and is adjustably connected to the lever 20. The shaft 16 may be rotatable by a motor 11 and connected through a flexible cable 17 and a slip clutch 171 to a wire 15 operatively connectible to an aircraft propellor. The motor 11 and second member 14 are controllable by a hand member 5. Two pylons, each having an aircraft, may be mounted on opposite ends of a rotatable arm. The aircraft may be as disclosed and claimed in Specification 1304441 wherein the torque in wire 21 automatically compensates for any pitching of the aircraft.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB553771 | 1971-04-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1331851A true GB1331851A (en) | 1973-09-26 |
Family
ID=9798055
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1331851D Expired GB1331851A (en) | 1971-04-19 | 1971-04-19 | Pylon for use with a tethered model aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1331851A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115051308A (en) * | 2022-07-04 | 2022-09-13 | 深圳市亮视智能工程有限公司 | Unmanned aerial vehicle wire loop structure, mobile power supply box and lamp switching control method thereof |
-
1971
- 1971-04-19 GB GB1331851D patent/GB1331851A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115051308A (en) * | 2022-07-04 | 2022-09-13 | 深圳市亮视智能工程有限公司 | Unmanned aerial vehicle wire loop structure, mobile power supply box and lamp switching control method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |