US4066890A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Rotor tip light control
Assignee: United States Department of the Army
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Filing: 1976-09-24
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Granted: 1978-01-03
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Expires: 1996-09-24
Abstract
Abstract A control circuit for controlling the intensity of a plurality of lights nted at the ends of the rotor blades of a helicopter. The control circuit is completely self-contained and is powered by a wind-driven generator mounted to the blades. Commands to alter the intensity of the lights or to switch the lights on or off are transmitted by a pulsed light beam mounted on the helicopter tail boom.
Inventors
- 👤 Charles W. Hamilton
- 👤 Alfred Kleider
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 22:58
CPC Classifications
B; B64; B64D; B64D47/00; B64D47/02; B64D47/06
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
129 words
In combination with a helicopter having a shaft and a plurality of rotor blades fastened at one end to said shaft; A rotor tip light mounted to the other end of at least one of said rotor blades; means mounted to said one rotor blade for supplying electrical current to said rotor tip light; means mounted to said rotor blade for controlling said current to said rotor tip light in a plurality of selective discrete incremental levels to change the intensity of said light; and means mounted on the main body of said helicopter and synchronized with the rotation of said rotor blades for transmitting coded optical signals to said controlling means to instruct the same to selectively apply said incremental levels of current to said rotor tip light.
Claim 2
Dependent Claim
129 words
In combination with a helicopter having a shaft and a plurality of rotor blades fastened at one end to said shaft; A rotor tip light mounted to the other end of at least one of said rotor blades; means mounted to said one rotor blade for supplying electrical current to said rotor tip light; means mounted to said rotor blade for controlling said current to said rotor tip light in a plurality of selective discrete incremental levels to change the intensity of said light; and means mounted on the main body of said helicopter and synchronized with the rotation of said rotor blades for transmitting coded optical signals to said controlling means to instruct the same to selectively apply said incremental levels of current to said rotor tip light.
Claim 3
Dependent Claim
28 words
The apparatus according to claim 1 wherein said means for transmitting coded optical signals is a source of light pulses synchronized with the rotation of said rotor blades.
Claim 4
Dependent Claim
87 words
The apparatus according to claim 2 wherein said source of light pulses is: a laser mounted to the main body of said helicopter for directing a beam of radiant energy onto said controlling means; and means for modulating the output of said laser with the instructions for said controlling means, and said controlling means further comprises: a photo-detector for receiving said coded optical signal; and an optical filter positioned in front of said photo-detector for filtering out all optical radiation other than the output of said laser.
Claim 5
Dependent Claim
82 words
The apparatus according to claim 3 wherein said controlling means comprises: a plurality of silicon-controlled-rectifiers and resistors connected between said current supplying means and said rotor tip light for supplying selective incremental levels of current to said light, when rendered conductive; and means, connected to the control electrodes of said silicon-control-rectifiers for decoding the coded output signal of said photo-detector and for selectively activating particular ones of said silicon-control-rectifiers whereby the desired intensity of illumination for said rotor tip light is achieved.
Claim 6
Dependent Claim
59 words
The apparatus according to claim 4 wherein said decoding means comprises a plurality of NAND-gates, each gate having an output connected to the control electrode of the corresponding silicon-control-rectifier, an input connected to the output of said photo-detector and at least one other input connected, via an inverter, to the cathode of the next succeeding silicon-control-rectifier in the decoder.
Claim 7
Dependent Claim
39 words
The apparatus according to claim 5 wherein said decoding means further includes a bistable multivibrator interconnected between the output of each gate and the corresponding control electrode of the associated silicon-control-rectifier to stretch the output pulse from said gate.
Claim 8
Dependent Claim
52 words
The apparatus according to claim 6 wherein said decoding means further comprises an additional silicon-control-rectifier to energize and deenergize said rotor tip light, said additional silicon-control-rectifier being connected between said current supplying means and the terminal of said rotor tip light which does not connect to said plurality of silicon control rectifiers.
Claim 9
Dependent Claim
53 words
The apparatus according to claim 7 wherein said decoding means further comprises a NAND-gate having an output connected to the control electrode of said additional silicon-control-rectifier, a first input connected to the output of said photo-detector and a second input connected to the cathode of the last one of said plurality of silicon-control-rectifiers.
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) | 1981-01-02 | 1981-07-04 | 1982-01-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-01-02 | 1985-07-04 | 1986-01-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-01-02 | 1989-07-04 | 1990-01-03 | $7700.00 | Window Closed / Lapsed |