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US4420755A Expired / Lapsed US ⏱️ 0.0 years remaining

Telemetry load link assembly

Assignee: United States Department of the Air Force
•
Filing: 1981-08-21
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Granted: 1983-12-13
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Expires: 2001-08-21
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Abstract

Abstract A mid-way recovery system having an aircraft with a winch and cable system for recovering parachute descending objects wherein a telemetry load link system monitors the strain placed upon a cable by having a telemetry load link assembly connected into the cable so strain data is transmitted to a radio receiver on board the aircraft for monitoring the strain placed upon the cable.

Inventors

  • 👤 Robert J. Primbs, Jr.

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 14:22
CPC Classifications
G; G01; G01L; G01L5/00; G01L5/04; G01L5/047; G01L5/10; G01L5/101

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 246 words
An improved mid-air recovery system having an aircraft with a winch and cable, said cable having a hook for capturing a parachute descending object, said improved mid-air recovery system comprising: a telemetry load link assembly attached to said cable to measure and to transmit strain in said cable while said object is attached to said cable on said aircraft, said telemetry load link assembly having a load link rotatably connected to said cable, a load sensing link rotatably connected to said load link, and a telemetry load link rotatably connected between said load sensing link and said cable, said telemetry load link having a transmitter for receiving strain data from said load sensing link and for transmitting an RF strain signal, a housing for fixedly holding said transmitter and for holding a power supply for said transmitter in said telemetry load link, bolting means for connecting said telemetry load link to said load sensing link and said cable, a loop guide for connecting said cable to said bolting means, and a stabilizing pin for damping out oscillations between said telemetry load link and said cable; a receiver located in said aircraft to receive said RF strain signal, said receiver outputting a strain signal; and strain monitor means for receiving said strain signal from said receiver and for outputting transformed strain data to be interpreted by a winch control for controlling a rate of winching of said cable that has hooked thereon said object to be recovered.
Claim 2
Dependent Claim 246 words
An improved mid-air recovery system having an aircraft with a winch and cable, said cable having a hook for capturing a parachute descending object, said improved mid-air recovery system comprising: a telemetry load link assembly attached to said cable to measure and to transmit strain in said cable while said object is attached to said cable on said aircraft, said telemetry load link assembly having a load link rotatably connected to said cable, a load sensing link rotatably connected to said load link, and a telemetry load link rotatably connected between said load sensing link and said cable, said telemetry load link having a transmitter for receiving strain data from said load sensing link and for transmitting an RF strain signal, a housing for fixedly holding said transmitter and for holding a power supply for said transmitter in said telemetry load link, bolting means for connecting said telemetry load link to said load sensing link and said cable, a loop guide for connecting said cable to said bolting means, and a stabilizing pin for damping out oscillations between said telemetry load link and said cable; a receiver located in said aircraft to receive said RF strain signal, said receiver outputting a strain signal; and strain monitor means for receiving said strain signal from said receiver and for outputting transformed strain data to be interpreted by a winch control for controlling a rate of winching of said cable that has hooked thereon said object to be recovered.
Claim 3
Dependent Claim 79 words
An improved mid-air recovery system as defined in claim 1, wherein said housing comprises mounting plates, a top, bottom, a front, and a back, said housing forming a rectangular compartment for fixedly holding said power supply and said transmitter, said mounting plates having arms for bolting holes and stabilizing pin holes for attaching said loop guide and said load sensing link, said plates having holes communicating to said compartment for a data line, a power control, and an antenna.
Claim 4
Dependent Claim 18 words
An improved mid-air recovery system as defined in claim 1, wherein said transmitter is an FM radio transmitter.

References Cited (Backward Citations)

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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1986-12-12 1987-06-13 1987-12-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1990-12-12 1991-06-13 1991-12-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1994-12-12 1995-06-13 1995-12-13 $7700.00 Window Closed / Lapsed

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