| US3568953A | 1971-03-09 | |||
| AU2009100967A4 | 2009-11-05 | |||
| US20070187547A1 | 2007-08-16 | |||
| US2471599A | 1949-05-31 |
| Claims 1. Our invention is an acquisition and landing systems of aircrafts and spacecrafts in ari and space, and its feature is that it covers push system positioning circle able to position push systems (1), push system power and control center (2), and articulatory system able to move push system positioning circle in 180 degrees in horizontal and vertical (3), hydraulic or pneumatic pump and control system (4), arm system moveable as hydraulic and pneumatic (5), push systems and equipments main body. 2. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that; it covers push system positioning circle (1) able to position push systems in itself such as one or multi phase rocket system (8) mountable into push system positioning circle, depending on situation features in acquisition and landing systems with push system, connectable to aircrafts and spacecrafts with its own external movement, or or one or multi phase fan system mountable into push system positioning circle (9) or jet motor system mountable into push system positioning circle (15). 3. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that; it covers push system power and control center, ensures to approach to aircrafts and spacecrafts with push system connected with its own external movement in acquisition and landing systems, in horizontal or vertical as well as multi-driectional depending on crafts' position, and and articulatory systems (3) able to move push system positioning circle in 180 degrees in horizontal and vertical. 4. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that it covers system that captures and holds aircrafts and spacecrafts with help of hydraulic or pneumatic pump and control system (4) on push systems and equipments main body (7) enables to acquisition and holding process from suitable points of aircrafts and spacecrafts body while ensures landing and directing aircrafts and spacecrafts to any desired direction in air and space, with push system connected with its own external movement in acquisition and landing systems, and arm system moveable as hydraulic and pneumatic (5) and clutch shoes (6). 5. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that it covers controlled magnetic lock system (13) enables opening and closing of push system and equipments main body from its suitable points (7) in special situations, optionally, when achieving easier connection to aircrafts and spacecrafts with push system connected with its own external movement in acquisition and landing systems. 6. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that push systems and equipments main body, mountable to aircrafts and spacecrafts inner body and/or external body with push system in landing systems has the feature to be mountable on aircrafts and pacecrafts external section and/or internal section as openable when necessary. 7. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that it covers push systems and equipments main body, mountable to aircrafts and spacecrafts inner body and/or external body with push system in landing systems (7), articulatory system (3), enables the mounting of push systems positioning circle to aircrafts and spacecrafts' inner body and/or external body as openable when necessary and as paralel to the body and able to move push system positioning circle as 180 degrees in horizontal and/or vertical, intermediate arm connection (10) and push system positioning circle (1). 8. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that it covers parachute system (11) able to enter in push system positioning circle (1), and able to placed in push system positioning circle that ensures aircrafts and spacecrafts being slowdown and stopped in special conditions, mountable to aircrafts and spacecrafts inner body and/or external body with push system in landing systems, connected to aircrafts and spacecrafts externally with its own movement with push system in landing systems. 9. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that depending on the conditions, equipments and equipment groups in systems can be used more than once in landing systems with push system, mountable to aircrafts and spacecrafts inner body and/or external body, with push system in acquisition and landing systems, connected to aircrafts and spacecrafts externally with its own movement. 10. Our invention in Claim 1 is an acquisition and landing systems of aircrafts and spacecrafts in air and space and its feature is that push system and equipments main body, in landing systems with push system, mountable to aircrafts and spacecrafts inner body and/or external body, with push system in acquisition and landing systems, connected to aircrafts and spacecrafts externally with its own movement, can be in circle, square and rectangular shape. |
As stated in the title, our invention includes acquisition and landing of aricrafts and spacecratfs in air and space in case of danger or in terms of being more economically.
In the present technology, this could only be done within the scope of rocket systems and aircrafts, we are trying to actualise it with external systems and systems, mountable inside the crafts, that are more practical and with enhanced functional scope.
In our systems, system aims to minimise time loss and financial loss with more practical and more functional systems.
Explanation of Images
Image A Acquisition and landing system with push system connected externally to aircraft and spacecraft with its own movement
Image B landing system with push system, mountable inner and/or external body of aircraft or spacecraft
Referece Explanation
1. Push system positioning circle
2. push system, power and control center
3. articulatory system enable to move push system positioning circle i 180degrees horizontal or vertical
4. Hydroulic or pneumatic pump and control center
5. Hydraulic or pneumatic moveable arm system
6. Clutch shoes
7. Push system and equipments main body
8. One or multi phase rockey system mountable inside push system positioning circle
9. One or multi phase fan system mountable inside push system positioning circle 10. Intermediate arm connection
11. Parachute system able to enter in push system positioning circle
12. Jet motor system able to enter in push system positioning circle
13. Controlled magnetic lock system Our invention, acquisition and landing systems of aircrafts and spacecratfs in air and space, is able to perform acquisition and landing of aircrafts and spacescrafts by push system structure connected to aircrafts and spacesrafts externally with its own movement as shown in Image A, and able to perform landing with push system mountable to inner and/or external body of aircrafts and spacecrafts as shown in Image B.
In order to explain the system starting from Image A,
By ensuring multi directional movement of push system positioning circle (1), push systems such as one or multi phase rocket system mountable into push system positioning circle depending on situation features (4) or one or multi phase fan system mountable into push system positioning circle (9) or jet motor system mountable into push system positioning circle (15) with push system, control of power and control center (2) and articulatory system (3) able to move push system positioning circle 180 degrees horizontal and/or vertical, approcahes to aircrafts and spacecrafts in horizontal or vertical position depending on crafts position, captures, holds aircrafts and spacecrafts in air and space from their suitable points on their body with clutch shoes with help of hydraulic or pneumatic pump and control system above push systems and equipments main body and with help of hydraulically or pneumatically moveable arm system (5) and ensures to landing and directing aircrafts and spacecrafts in any desired direction in air and space.
In special conditions, optionally, easier connection with aircrafts and spacecrafts is achieved by ensuring opening and closing with placement of controlled magnetic lock system to special points on push system and equipments main body.
In Image B, push systems and equipments main body (7) can be mountable on external or inner sections of aircrafts and spacecrafts as openable when necessary. During mounting, intermediate arm systems (10) and push system positioning circles are positioned as paralel to the body with help of articulatory system (3) able to move push system positioning circle (1) as 180 degrees horizontal and /or vertical.
During operation, aircrafts and spacecrafts can be ensured to land and direct to any desired direction with the help of articulatory systems (3) able to move 180 degress horizontal and/or vertical and with help of push systems such as jet motor system (13) mountabel in push system positioning circle or one or multi phase fan system (9) mountable in push system positioning circle or one or multi phase rocket system mountable in push system positioning circle in accordance with the situation, by opening of intermediate arms connections (10) and push system positioning circle (1) with help of articulatory systems moveable in 180 degrees horizontal and/or vertical.
In these special conditons, aircrafts and spacecrafts can be slowdown and stopped by installing push system positioning circle of parachute system (11) able to enter in push system positioning circle (1). Depending on the situation, equipments and equipment groups in the system can more than one.
Besides, push system and equipments main body can in circle, square and rectangular shape.