US4131250A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Helicopter blade ice protection systems
Assignee: Individual
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Filing: 1977-06-13
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Granted: 1978-12-26
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Expires: 1997-06-13
Abstract
Abstract An external system installed on a helicopter to spray a freezing point depressant fluid onto the main rotor blade of a single rotor helicopter to prevent the collection of ice when flying through icing weather. Actuation of this ice protection system will cause a pump to force a glycerine-alcohol mixture through a series of fixed nozzles to create a spray of freezing point depressant. The main rotor blade will move through this spray and be coated, thus preventing the collection of ice on the blade. Such protection is of vital importance to all-weather helicopter operations as experience has shown that the collection of ice on the rotor blades of helicopters is a safety of flight problem.
Inventors
- 👤 Earle T. Binckley
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 02:18
CPC Classifications
B; B64; B64D; B64D15/00; B64D15/02; B64D15/06; B64D15/10
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
98 words
A means for preventing the accumulation of ice on a helicopter main rotor blade, the system comprising a tank for carrying the supply of freezing point depressant fluid, a pump mounted in the tank to move the fluid from the tank through tubing to the nozzles, said pump to be actuated by a switch accessible to the pilot, tubing between the tank and the nozzles for carrying the fluid, a nozzle array mounted in the shadow area of the rotor mast, external to the helicopter, and that sprays the fluid upward into the path of the rotor blades.
Claim 2
Dependent Claim
98 words
A means for preventing the accumulation of ice on a helicopter main rotor blade, the system comprising a tank for carrying the supply of freezing point depressant fluid, a pump mounted in the tank to move the fluid from the tank through tubing to the nozzles, said pump to be actuated by a switch accessible to the pilot, tubing between the tank and the nozzles for carrying the fluid, a nozzle array mounted in the shadow area of the rotor mast, external to the helicopter, and that sprays the fluid upward into the path of the rotor blades.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-12-25 | 1982-06-26 | 1982-12-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-12-25 | 1986-06-26 | 1986-12-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-12-25 | 1990-06-26 | 1990-12-26 | $7700.00 | Window Closed / Lapsed |