| Téléchargement | - Voir la version finale : Icing and de-icing flight tests of a Kaman HU2K-1 helicopter (PDF, 4.9 Mio)
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| DOI | Trouver le DOI : https://doi.org/10.4224/40004023 |
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| Auteur | Rechercher : Gibbard, G. A.1 |
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| Affiliation | - Conseil national de recherches Canada. Division de génie mécanique
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| Format | Texte, Rapport technique |
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| Description physique | 36 p. |
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| Résumé | Flight tests were performed in an artificial icing cloud on a Kaman HUZK-1 helicopter eguipped with a prototype electro-thermal rotor blade de-icing system. The results of the icing flights showed that icing protection will be required on this helicopter mainly because of icing in the engine inlet and the effects of uncontrolled shedding of ice from the rotor blades. During the runs on which it was tested, the installed main rotor blade de-icing system did not operate satisfactorily under all conditions, and the need for modifications to improve its performance was indicated. |
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| Date de publication | 1961-05 |
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| Maison d’édition | National Research Council Canada |
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| Série | |
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| Langue | anglais |
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| Publications évaluées par des pairs | Non |
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| Exporter la notice | Exporter en format RIS |
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| Signaler une correction | Signaler une correction (s'ouvre dans un nouvel onglet) |
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| Identificateur de l’enregistrement | 77b550d9-a4f6-44bd-8895-5b6d6e9621d2 |
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| Enregistrement créé | 2026-05-05 |
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| Enregistrement modifié | 2026-05-06 |
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