ES200540U - Toy aircraft with adjustable displacement by independent modules. (Machine-translation by Google Translate, not legally binding) - Google Patents
Toy aircraft with adjustable displacement by independent modules. (Machine-translation by Google Translate, not legally binding)Info
- Publication number
- ES200540U ES200540U ES0200540U ES200540U ES200540U ES 200540 U ES200540 U ES 200540U ES 0200540 U ES0200540 U ES 0200540U ES 200540 U ES200540 U ES 200540U ES 200540 U ES200540 U ES 200540U
- Authority
- ES
- Spain
- Prior art keywords
- translation
- machine
- legally binding
- google translate
- independent modules
- 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.)
- Granted
Links
- 238000006073 displacement reaction Methods 0.000 title abstract 2
Landscapes
- Toys (AREA)
Abstract
Toy airplane with adjustable displacement by independent modules, characterized by being formed by an aerodynamic body, short and flattened hunting type, open at the top where it appears part of a figure that imitates the pilot and in front of him a vacuum or platform in which the head of a mechanism for variable orientations emerges through a set of modular pieces that is dragged by front wheels of traction and oriented through a rear steerable wheel of rudder in relation to the mentioned head of orientations and that it is controlled by a unique engine that coordinates with the propeller of the plane. (Machine-translation by Google Translate, not legally binding)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES1974200540U ES200540Y (en) | 1974-02-16 | 1974-02-16 | TOY AIRCRAFT WITH ADDRESSABLE DISPLACEMENT BY MODU-LOS INDEPENDIENTES. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES1974200540U ES200540Y (en) | 1974-02-16 | 1974-02-16 | TOY AIRCRAFT WITH ADDRESSABLE DISPLACEMENT BY MODU-LOS INDEPENDIENTES. |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES200540U true ES200540U (en) | 1975-09-01 |
| ES200540Y ES200540Y (en) | 1976-01-16 |
Family
ID=8368098
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES1974200540U Expired ES200540Y (en) | 1974-02-16 | 1974-02-16 | TOY AIRCRAFT WITH ADDRESSABLE DISPLACEMENT BY MODU-LOS INDEPENDIENTES. |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES200540Y (en) |
-
1974
- 1974-02-16 ES ES1974200540U patent/ES200540Y/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| ES200540Y (en) | 1976-01-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| SE8000355L (en) | mech | |
| GB1512719A (en) | Vertical takeoff and landing aircraft | |
| GB1212705A (en) | An aircraft | |
| GB647779A (en) | Improvements in or relating to aircraft | |
| GB1157822A (en) | VTOL Aircraft | |
| GB1518464A (en) | Aircraft | |
| GB1276732A (en) | Tandem wing aircraft | |
| ES200540U (en) | Toy aircraft with adjustable displacement by independent modules. (Machine-translation by Google Translate, not legally binding) | |
| GB1381646A (en) | Aircraft with short take-off and landing characteristics | |
| DE3775190D1 (en) | PLANE. | |
| GB1285907A (en) | A ground effect vehicle | |
| EP0101644A3 (en) | Variable sweep forward wing aircraft | |
| FR2313263A1 (en) | Multiwing aircraft for agricultural work - can fly at low speed without risk of stalling and has variable incidence front wing | |
| FR2281875A1 (en) | Variable geometry high speed aircraft - with tailplate which moves into recess of main wing for fast flight | |
| GB829183A (en) | Improvements in rotary-wing aircraft | |
| GB819665A (en) | Improvements in or relating to high speed aircraft | |
| ES2015827A6 (en) | Remote-controlled equipment-carrying aircraft | |
| FR2411128A1 (en) | Propeller-driven aircraft - has fairing formed by elevators and rudder and also including fixed surfaces | |
| Cook et al. | The aerodynamic design optimisation of a forward swept wing fighter aircraft | |
| GB593032A (en) | Improvements in or relating to aircraft | |
| SU549829A1 (en) | Training device for practical aerodynamics | |
| ES14412U (en) | Toy gyrocopter. (Machine-translation by Google Translate, not legally binding) | |
| FR2405869A1 (en) | Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed | |
| HOLFORD | Aerodynamic data for the BAC 221 up to a Mach number of 0. 955 as measured in wind-tunnel tests(Longitudinal and lateral data, lateral oscillatory derivatives, and aileron and rudder powers for BAC 221 aircraft) | |
| FR2272893A1 (en) | Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevators |