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US3838836A Expired / Lapsed US ⏱️ 0.0 years remaining

Method and apparatus for load stabilization in heavy lift helicopters

Assignee: Calspan Corp
•
Filing: 1973-08-08
•
Granted: 1974-10-01
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Expires: 1993-08-08
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Abstract

Abstract The external load produced motions in a heavy lift helicopter are stabilized by dynamically stabilizing the load. A three-point suspension system is used to support the load with each of the points being individually movable in response to sensed conditions of the relative motions of the load and helicopter.

Inventors

  • 👤 S Asseo
  • 👤 R Whitbeck

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 08:51
CPC Classifications
B; B64; B64D; B64D1/00; B64D1/22; G; G05; G05D; G05D1/00; G05D1/08; G05D1/0808; G05D1/0858

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 107 words
A method of load stabilization for use in a pilot commanded heavy lift helicopter carrying an externally slung load including the steps of: supporting each point of a 3-point suspension system by a respective one of three winch controller means secured to the helicopter; securing a load to the 3-point suspension system; sensing the motion of the helicopter and load; sensing pilot command signals; and controlling each of the winch controller means in response to the sensed motion of the helicopter and load and the pilot command signals, whereby the 3-point suspension system is positioned to dynamically stabilize the load under conditions tending to produce load oscillations.
Claim 2
Independent Claim 107 words
A method of load stabilization for use in a pilot commanded heavy lift helicopter carrying an externally slung load including the steps of: supporting each point of a 3-point suspension system by a respective one of three winch controller means secured to the helicopter; securing a load to the 3-point suspension system; sensing the motion of the helicopter and load; sensing pilot command signals; and controlling each of the winch controller means in response to the sensed motion of the helicopter and load and the pilot command signals, whereby the 3-point suspension system is positioned to dynamically stabilize the load under conditions tending to produce load oscillations.
Claim 3
Dependent Claim 24 words
The method of claim 1 further including the step of operating said winch controller means as speed regulators to raise and lower the load.
Claim 4
Dependent Claim 33 words
The method of claim 1 further including the step of moving one of said winch controller means with respect to the helicopter in response to the sensed motion of the helicopter and load.
Claim 5
Dependent Claim 141 words
Apparatus for load stabilization in a heavy lift helicopter comprising: three winch controller means secured to and supported by said helicopter; a 3-point suspension system supported at each point by a respective one of said winch controller means; means for securing a load to said 3-point suspension system; pilot actuated helicopter control means for transmitting pilot command signals indicative of desired helicopter operation; instrument means for sensing helicopter motion and transmitting signals indicative thereof; instrument means for sensing load motion and transmitting signals indicative thereof; central control means for receiving and blending the pilot command signals and the signals indicative of the helicopter motion and the load motion and, responsive thereto, transmitting control signals for controlling the flight of the helicopter and the operation of the winch controller means whereby the 3-point suspension system is positioned to dynamically stabilize the load.
Claim 6
Dependent Claim 141 words
Apparatus for load stabilization in a heavy lift helicopter comprising: three winch controller means secured to and supported by said helicopter; a 3-point suspension system supported at each point by a respective one of said winch controller means; means for securing a load to said 3-point suspension system; pilot actuated helicopter control means for transmitting pilot command signals indicative of desired helicopter operation; instrument means for sensing helicopter motion and transmitting signals indicative thereof; instrument means for sensing load motion and transmitting signals indicative thereof; central control means for receiving and blending the pilot command signals and the signals indicative of the helicopter motion and the load motion and, responsive thereto, transmitting control signals for controlling the flight of the helicopter and the operation of the winch controller means whereby the 3-point suspension system is positioned to dynamically stabilize the load.
Claim 7
Dependent Claim 31 words
The apparatus of claim 4 wherein said central control means include means for selectively operating said winch controller means to raise or lower the load or to dynamically stabilize the load.
Claim 8
Dependent Claim 44 words
The apparatus of claim 5 wherein said means for selectively operating said winch controller means includes a relay actuated in response to one of said pilot command signals for selectively supplying either of two sets of the control signals to the winch controller means.
Claim 9
Dependent Claim 28 words
The apparatus of claim 6 further comprising means for repositioning one of said winch controller means relative to said helicopter in response to one of said control signals.
Claim 10
Dependent Claim 28 words
The apparatus of claim 4 further comprising means for repositioning one of said winch controller means relative to said helicopter in response to one of said control signals.

References Cited (Backward Citations)

US3339966A Cited
US3656796A Cited
US3510107A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-09-30 1978-04-01 1978-10-01 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-09-30 1982-04-01 1982-10-01 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-09-30 1986-04-01 1986-10-01 $7700.00 Window Closed / Lapsed

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