GB1490164A - Toy - Google Patents
ToyInfo
- Publication number
- GB1490164A GB1490164A GB327475A GB327475A GB1490164A GB 1490164 A GB1490164 A GB 1490164A GB 327475 A GB327475 A GB 327475A GB 327475 A GB327475 A GB 327475A GB 1490164 A GB1490164 A GB 1490164A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aeroplane
- platform
- impeller
- hook
- toy
- 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
- A63H27/14—Starting or launching devices for toy aircraft; Arrangements on toy aircraft for starting or launching
Landscapes
- Toys (AREA)
Abstract
1490164 Toys AIRFIX PRODUCTS Ltd 17 March 1976 [24 Jan 1975] 3274/75 Heading A6S A toy comprises a platform 10, Fig. 1, with a spring-loaded impeller 21a, &c releasably coupled to a toy aeroplane A which runs along a support line L attached at one end to a hand-control 12, 13, &c and at the other to a remote point (not shown) above the platform, the aeroplane being suspended from the line by hooks 17 and a rod 16, &c which allows it to turn through 180 degrees at the end of its travel away from the platform to which it then returns nose first. A lever 18, Fig. 5, and hook 18a in the toy aeroplane coact with a cam 20a on the suspension rod 16 so that on the outward flight the hook, &c is retained in a raised position, but after the aeroplane has turned through 180 degrees the hook, &c is lowered. At the end of the platform 10, a cover 56. Fig. 1. is pivoted to its shut position; on take-off of the aeroplane, the impeller 21a, &c runs along a slot 30, and, a cam (31), Fig. 6 (not shown) at its side engages a cam 32a, Fig. 3, on a lever journalled by pins 33. The lever pivots up an H-member 34 carrying funnels 37 through which pass a landing wire 36. The returning aeroplane A engages its hook 18a with the landing wire 36, and the cover 56 is raised to the position shown. The handcontrol 12, &c is mounted to the platform by a ball and socket joint 11, and the end of the line L is attached to a finger grip 13 slidable up and down the hand-control. The handcontrol 12, &c permits adjustment of the tension, &c of the line L. The toy aeroplane A has a pin 29 slidable into a socket in the impeller 21a, &c which is drawn along the slot 30 by an adjustably-tensioned rubber band (24), Fig. 2, running over a pulley. To cock the impeller 21a, &c, a string 23 is pulled, until the impeller engages a spring biassed catch (26, 21); the catch is released by a trigger 28. Reference has been directed by the comptroller to Specification 1405938.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB327475A GB1490164A (en) | 1976-03-17 | 1976-03-17 | Toy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB327475A GB1490164A (en) | 1976-03-17 | 1976-03-17 | Toy |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1490164A true GB1490164A (en) | 1977-10-26 |
Family
ID=9755241
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB327475A Expired GB1490164A (en) | 1976-03-17 | 1976-03-17 | Toy |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1490164A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101081638B (en) * | 2006-06-02 | 2010-11-17 | 珠海星宇航空技术有限公司 | Unmanned aerial plane launching system and method |
CN113018881A (en) * | 2021-04-25 | 2021-06-25 | 航天创客(北京)科技有限公司 | Aerospace science popularization model self-adaptive ejection device |
-
1976
- 1976-03-17 GB GB327475A patent/GB1490164A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101081638B (en) * | 2006-06-02 | 2010-11-17 | 珠海星宇航空技术有限公司 | Unmanned aerial plane launching system and method |
CN113018881A (en) * | 2021-04-25 | 2021-06-25 | 航天创客(北京)科技有限公司 | Aerospace science popularization model self-adaptive ejection device |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |