CA401686A - Pale en composition d'helice - Google Patents

Pale en composition d'helice

Info

Publication number
CA401686A
CA401686A CA401686A CA401686DA CA401686A CA 401686 A CA401686 A CA 401686A CA 401686 A CA401686 A CA 401686A CA 401686D A CA401686D A CA 401686DA CA 401686 A CA401686 A CA 401686A
Authority
CA
Canada
Prior art keywords
propeller blade
composite propeller
composite
blade
propeller
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA401686A
Other languages
English (en)
Inventor
Walker Caldwell Frank
Martin Erle
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
Publication date
Application granted granted Critical
Publication of CA401686A publication Critical patent/CA401686A/fr
Expired legal-status Critical Current

Links

CA401686A Pale en composition d'helice Expired CA401686A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA401686T

Publications (1)

Publication Number Publication Date
CA401686A true CA401686A (fr) 1941-12-23

Family

ID=35412132

Family Applications (1)

Application Number Title Priority Date Filing Date
CA401686A Expired CA401686A (fr) Pale en composition d'helice

Country Status (1)

Country Link
CA (1) CA401686A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2206597A2 (fr) 2009-01-07 2010-07-14 GE Aviation Systems Limited Procédé et dispositif pour la fabrication des longerons composites

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2206597A2 (fr) 2009-01-07 2010-07-14 GE Aviation Systems Limited Procédé et dispositif pour la fabrication des longerons composites
US8061253B2 (en) 2009-01-07 2011-11-22 Ge Aviation Systems Limited Composite spars

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