TRANSPORTATION APPARATUS AND METHOD FOR CARRYING A PAYLOAD IN A DESIRED PLANE INDEPENDENT OF 3D TILTING OF SAID APPARATUS

• US 20110276233A1
• Filed: 05/12/2011
• Published: 11/10/2011
• Est. Priority Date: 11/12/2008
• Status: Active Grant

• Current Assignee: Kipax AB, Zoomability AB (Zoomability Int AB)
• Original Assignee: Zouce AB
• Inventors: Löfstrand, Mikael
• Granted Patent: US 8,565,982 B2
• Time in Patent Office: Days
• US Class Current: 701/49
• CPC Class Codes: A61G 2203/42 for inclination
• CPC Class Codes: A61G 5/04 motor-driven A61G5/06 takes precedence; motor-operated rests A61G5/12; for vehicles with handlebars, equipped with three or more wheels B62K5/003, B62K5/023
• CPC Class Codes: A61G 5/06 with obstacle mounting facilities, e.g. for climbing stairs, kerbs or steps
• CPC Class Codes: A61G 5/061 for climbing stairs
• CPC Class Codes: A61G 5/1056 Arrangements for adjusting the seat
• CPC Class Codes: A61G 5/107 positioning the whole seat forward or rearward
• CPC Class Codes: A61G 5/1075 tilting the whole seat backwards tilting forwards for standing-up or sitting-down aids A61G5/14
• CPC Class Codes: B60N 2/02246 Electric motors therefor
• CPC Class Codes: B60N 2/0244 with logic circuits
• CPC Class Codes: B60N 2/0268 using sensors or detectors for adapting the seat or seat part, e.g. to the position of an occupant
• CPC Class Codes: B60N 2/04 the whole seat being movable
• CPC Class Codes: B60N 2/062 transversally slidable
• CPC Class Codes: B60N 2/0745 the slide path being curved
• CPC Class Codes: B60N 2/39 Seats tiltable to compensate for roll inclination of vehicles
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats
• CPC Class Codes: B64D 2011/0092 Arrangements for mounting stretchers in aircraft cabins
• CPC Class Codes: F16M 11/20 Undercarriages with or without wheels

Abstract

A transportation apparatus includes a payload receiving unit, a transportation body, and a compensation system arranged there between providing adjustment of a desired spatial relationship of a payload surface of the compensation unit. The compensation system has at least one of a first compensation unit and a second compensation unit for adjustment of the spatial relationship. The compensation units adjust the spatial relationship in different directions. Thus the compensation system maintains a desired orientation of the payload surface independent of changes of orientation of the transportation surface. Further, the compensation system substantially maintains a common point of gravity of the transportation apparatus including the payload by displacing the center of gravity of the payload receiving unit and the payload substantially opposite to a displacement of a center of gravity of the transportation apparatus. At least one of the compensation units are extendable from at least one end thereof during operation.

Claims

1. A transportation apparatus (1), said apparatus comprising

a payload receiving unit (30), a transportation body (10), and a controllable compensation system (20) arranged there between and devised to allow adjustment of a desired spatial relationship between a payload surface (250) of said compensation system (20) for attachment of said payload receiving unit (30) and a transportation surface (150) of said transportation body (10), wherein

said compensation system (20) comprises at least a first compensation unit (210) and a second compensation unit (230) arranged for adjustment of said spatial relationship, wherein said

first compensation unit (210) is arranged for adjustment of said spatial relationship in a first direction and said second compensation unit is arranged for adjustment of said spatial relationship in a second direction different from said first direction, whereby said compensation system (20) is adapted to maintain a desired orientation of said payload surface (250) substantially independent of changes of orientation of said transportation surface (150) of said transportation apparatus (1),

wherein said compensation system (20) is adapted to substantially maintain a common point of gravity of said transportation apparatus (1) including a payload by displacing a center of gravity of said payload receiving unit (30) and said payload substantially opposite to a displacement of a center of gravity of said transportation apparatus (1), and

wherein at least one of said first and/or second compensation units are extendable from at least one end thereof during operation.

2. The transportation apparatus according to claim 1, wherein said first and second compensation units are arranged in series to each other.

3. The transportation apparatus according to claim 1, wherein said first and second compensation units are attached to each other.

4. The transportation apparatus according to claim 1, wherein said first and second compensation units comprise at least one curved rail each having a curvature and being arranged in a crossed configuration.

5. The transportation apparatus according to claim 4, wherein said at least one curved rail is an in gravitational direction downwardly open curved rail having a circular curvature.

6. The transportation apparatus according to claim 4, wherein said curvature of said rails is chosen such that said common point of gravity is situated below said transportation apparatus, and wherein said curvature is continuous without a straight portion.

7. The transportation apparatus according to claim 6, wherein said at least one rail of said first compensation unit is arranged at a different height than said at least one rail of said second compensation unit, and wherein said rails of said compensation units have different curvatures having a common virtual center point.

8. The transportation apparatus according to claim 4, wherein said curvature of said at least one rail is chosen to be of a radius with its centre point placed at the average rotation point of said vehicle on the middle part of the rails.

9. The transportation apparatus according to claim 4, wherein said curvature of said rails is adapted to an individual mass and distribution of a payload to be carried by said payload surface (250).

10. The transportation apparatus according to claim 1, wherein said compensation system is configured to operate partly passively based on inertia movement of said payload unit (30) relative said transportation unit (10).

11. The transportation apparatus according to claim 10, wherein said compensation unit comprising breaking or damping elements that are actively controllable.

12. The transportation apparatus according to claim 1, wherein said compensation system is configured to operate with proportional extensions of the first and second compensation units.

13. The transportation apparatus according to claim 1, wherein said compensation system comprises at least one active controllable drive mechanism configured to provide active movement support of said first and second compensation unit to adapt said desired plane of said payload surface (250) in reaction to changes of orientation of said transportation surface (150) in real time.

14. The transportation apparatus according to claim 1, wherein said compensation system comprises a sensor actuator unit configured to provide a control feedback loop for said adjustment in real time.

15. The transportation apparatus according to claim 14, wherein said sensor actuator unit comprises at least two sensor systems, including a first sensor system adapted to provide a payload surface measurement value for the orientation in space of said payload supporting surface, and a second sensor system adapted to provide a transportation surface measurement value for the orientation in space of said transportation surface, wherein said control feedback loop has a difference between said payload surface measurement value and said transportation surface measurement value as a feedback value.

16. The transportation apparatus according to claim 1, wherein said transportation apparatus is adapted to travel along a topography with said transportation surface (150) having an angle in the range of 0 to 70 degrees in relation to a horizontal plane.

17. The transportation apparatus according to claim 1, wherein said first direction and said second direct are perpendicular to each other.

18. The transportation apparatus according to claim 1, wherein said transportation apparatus is a land based vehicle having at least two axis with at least two wheels each, and a wheelbase between said axis.

19. The transportation apparatus according to claim 18 dependent on claim 17, wherein said compensation unit is adapted to keep said common point of gravity in the vicinity of a center point of said wheelbase.

20. The transportation apparatus according to claim 1, wherein said transportation apparatus is a water carried apparatus, or an airborne apparatus.

21. The transportation apparatus according to claim 1, wherein said payload surface is adapted to receive interchangeable payloads and comprises a fastening unit.

22. The transportation apparatus according to claim 20, wherein said fastening unit is fastened to a seat for receiving a person, and wherein said desired plane is a substantially horizontal plane of a seat surface of said seat.

23. The transportation apparatus according to claim 21, wherein said fastening unit is fastened to a cargo carrier, including a stretcher.

28. The method according to claim 24, wherein said transportation apparatus is a transportation apparatus (1) according to claim 1.

31. A transportation apparatus comprising a compensation system as comprised in claim 1, wherein the transportation apparatus has a footprint area in the range of 0.9 to 0.3 m2, a wheelbase to payload surface height ratio in the range of 0.5 to 1.33, a ratio of a weight of a payload to a weight of the transportation apparatus in the range of 3 to 1, and compensation ranges in terrain angles up to 70 degrees from horizontal in all planes.

46. The apparatus of claim 45, wherein said apparatus is said apparatus of claim 1.

24. A method of substantially sustaining an orientation of payload surface (250) of a payload receiving unit (30) of transportation apparatus (1), independent of changes of orientation of a transportation surface (150) of a transportation body (10) of said transportation apparatus (1) in motion, said method comprising

real-time adjustment of a desired spatial relationship between said payload surface (250) and said transportation surface (150) by means of said compensation unit (20) attached to said payload receiving unit (30) and said transportation body (10), wherein said real-time adjustment comprises adjustment of said spatial relationship with at least a first compensation unit (210) and a second compensation unit (230) of said compensation system (20), and

adjustment of said spatial relationship in a first direction by said first compensation unit (210), and adjustment of said spatial relationship in a second direction different from said first direction by said second compensation unit (230), including expanding said first and/or second compensation unit during operation, and

substantially maintaining a common point of gravity of said transportation apparatus (1) including a payload by displacing a center of gravity of said payload receiving unit (30) and said payload with said compensation system (20) substantially opposite to a displacement of a center of gravity of said transportation apparatus (1).

25. The method according to claim 24, wherein said compensation is made vibration free in a rugged terrain environment with a stabilized desired plane of said payload surface (250).

26. The method according to claim 24, wherein said compensation system provides a displacement of said payload surface (250) while maintaining said desired plane in a direction opposite of a direction center of gravity displacement of said transportation body (10).

27. The method according to claim 26, wherein said compensation comprises an automatic proportional adjustment of said first compensation unit (210) and said second compensation unit (230) with regard to maintaining a common center of mass of said transportation apparatus (1) including a payload.

30. The computer program of claim 29 enabling carrying out of a method according to claim 24.

29. A computer program for processing by a computer and storable on a computer-readable medium for substantially sustaining an orientation of payload surface (250) of a payload receiving unit (30) of transportation apparatus (1), independent of changes of orientation of a transportation surface (150) of a transportation body (10) of said transportation apparatus (1) in motion, said computer program comprising

a code segment for real-time adjustment of a desired spatial relationship between said payload surface (250) and said transportation surface (150) by means of said compensation unit (20) attached to said payload receiving unit (30) and said transportation body (10), wherein said real-time adjustment comprises adjustment of said spatial relationship with at least a first compensation unit (210) and a second compensation unit (230) of said compensation system (20), and

a code segment for adjustment of said spatial relationship in a first direction by said first compensation unit (210), and adjustment of said spatial relationship in a second direction different from said first direction by said second compensation unit (230), and

a code segment for substantially maintaining a common point of gravity of said transportation apparatus (1) including a payload by displacing a center of gravity of said payload receiving unit (30) and said payload with said compensation system (20) substantially opposite to a displacement of a center of gravity of said transportation apparatus (1).

32. A compensation system (20) arranged between a payload receiving unit (30) and a transportation body (10), devised to allow adjustment of a desired spatial relationship between a payload surface (250) of said compensation system (20) for attachment of said payload receiving unit (30) and a transportation surface (150) of said transportation body (10), said system (20) comprising at least a first compensation unit (210) arranged for adjustment of said spatial relationship in a first direction, wherein said compensation system (20) is adapted to maintain a desired orientation of said payload surface (250) in said first direction substantially independent of changes of orientation of said transportation surface (150) of said transportation apparatus (1) in said first direction, and wherein said first compensation unit (210) is extendable from at least one end thereof during operation.

33. The system of claim 32, comprising a second compensation unit (230) arranged for adjustment of said spatial relationship, wherein said second compensation unit is arranged for adjustment of said spatial relationship in a second direction different from said first direction.

34. The system of claim 33, wherein said second compensation unit is extendable from at least one end thereof during operation.

35. The system of claim 34, whereby said compensation system (20) is adapted to maintain a desired orientation of said payload surface (250) substantially independent of changes of orientation of said transportation surface (150) of said transportation apparatus (1), and wherein said compensation system (20) is adapted to substantially maintain a common point of gravity of said transportation apparatus (1) including a payload by displacing a center of gravity of said payload receiving unit (30) and said payload substantially opposite to a displacement of a center of gravity of said transportation apparatus (1),

36. The system of claim 33, wherein said first and/or said second compensation unit comprises at least one curved rail having a curvature, and wherein said extendable capability is provided by a telescopic arrangement of said curved rail.

37. The system of claim 36, wherein said first and second compensation units being arranged in a crossed configuration.

38. The system of claim 36, wherein said curvature of said rails is chosen such that said common point of gravity is situated below said transportation apparatus, and wherein said curvature is continuous without a straight portion.

39. The system of claim 32, wherein said compensation system is configured to operate partly passively based on inertia movement of said payload unit (30) relative said transportation unit (10).

40. The system of claim 39, wherein said compensation unit comprising breaking or damping elements that are actively controllable.

41. The system of claim 32, wherein said compensation system is configured to operate with proportional extensions of at least the first compensation unit.

42. The system of claim 33, wherein said extendable capability is provided by an extension unit allowing a relative movement of the first compensation unit (210) to the second compensation unit.

43. The system of claim 42, wherein said relative movement is proportional.

44. The system of claim 32, wherein said compensation system comprises at least one active controllable drive mechanism configured to provide active movement support of said first and second compensation unit to adapt said desired plane of said payload surface (250) in reaction to changes of orientation of said transportation surface (150) in real time.

45. A transportation apparatus (1), said apparatus comprising said system of claim 32.