Patent US345891A successfully refreshed from Google Patents.
Patent US4591772A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4591772A Expired / Lapsed US ⏱️ 0.0 years remaining

Load positioning system with gravity compensation

Assignee: National Aeronautics and Space Administration
•
Filing: 1984-12-12
•
Granted: 1986-05-27
•
Expires: 2004-12-12
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A load positioning system with gravity compensation has a servo-motor (12), position sensing feedback potentiometer (38) and velocity sensing tachometer (42) in a conventional closed-loop servo arrangement to cause lead screw (14) and ball nut (20) to vertically position load (22). Gravity compensating components comprise the DC motor (32), gears (34) and (36), which couple torque from motor (32) to the lead screw (14), and constant-current power supply (37). The constant weight of the load (22) applied to the lead screw (14) via the ball nut (20) tends to cause the lead screw (14) to rotate, the constant torque of which is opposed by the constant torque produced by motor (32) when fed from the constant-current source (37). The constant current is preset as required by potentiometer (54) to effect equilibration of the load (22) which thereby enables the positioning servo-motor (12) to "see" the load (22) as weightless under both static and dynamic conditions. Positioning acceleration and velocity performance are therefore symmetrical.

Inventors

  • 👤 Richard H. Hollow

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 22:00
CPC Classifications
G; G05; G05D; G05D3/00; G05D3/12; G05D3/14

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 119 words
A load positioning system for moving a load in a first direction and a second direction in the vertical plane subjected to the force of gravity comprising first motor means for moving said load in the first and second directions, means for mechanically coupling said first motor means to said load, said force of gravity on said load inducing a torque on said coupling means, and a second motor means coupled to said coupling means for applying a torque equal and opposite to said gravity induced torque, said second motor means compensating for said force of gravity, so that acceleration and velocity of said load produced by said first motor means is symmetrical in the first and second directions.
Claim 2
Dependent Claim 119 words
A load positioning system for moving a load in a first direction and a second direction in the vertical plane subjected to the force of gravity comprising first motor means for moving said load in the first and second directions, means for mechanically coupling said first motor means to said load, said force of gravity on said load inducing a torque on said coupling means, and a second motor means coupled to said coupling means for applying a torque equal and opposite to said gravity induced torque, said second motor means compensating for said force of gravity, so that acceleration and velocity of said load produced by said first motor means is symmetrical in the first and second directions.
Claim 3
Dependent Claim 24 words
A load positioning system as set forth in claim 1 wherein said second motor means includes a DC motor supplied by a constant-current source.
Claim 4
Dependent Claim 23 words
A load positioning system as defined in claim 2 wherein said load is moved in a linear path by said first motor means.
Claim 5
Dependent Claim 25 words
A load positioning system as described in claim 3 wherein said coupling means includes a lead screw that is rotated by said first motor means.
Claim 6
Dependent Claim 19 words
A load positioning system as in claim 1 wherein said load is angularly moved by said first motor means.
Claim 7
Dependent Claim 30 words
A load positioning system as set forth in claim 5 wherein the torque generated by the second motor means varies as a function of the angular orientation of the load.

References Cited (Backward Citations)

US2415679A Cited
US2789260A Cited
US3408868A Cited
US3434025A Cited
US3771032A Cited
US3854378A Cited
US4022064A Cited
US4323828A Cited
US4126818A Cited
US4301528A Cited
US4373147A Cited
US4375047A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-05-26 1989-11-25 1990-05-27 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-05-26 1993-11-25 1994-05-27 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-05-26 1997-11-25 1998-05-27 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag