ES325626A2 - Rotor systems for rotating wing aircraft. (Machine-translation by Google Translate, not legally binding) - Google Patents

Rotor systems for rotating wing aircraft. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES325626A2
ES325626A2 ES0325626A ES325626A ES325626A2 ES 325626 A2 ES325626 A2 ES 325626A2 ES 0325626 A ES0325626 A ES 0325626A ES 325626 A ES325626 A ES 325626A ES 325626 A2 ES325626 A2 ES 325626A2
Authority
ES
Spain
Prior art keywords
rotor
translation
machine
legally binding
google translate
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
ES0325626A
Other languages
Spanish (es)
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.)
Bell Aerospace Corp
Original Assignee
Bell Aerospace Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Bell Aerospace Corp filed Critical Bell Aerospace Corp
Priority to ES0325626A priority Critical patent/ES325626A2/en
Publication of ES325626A2 publication Critical patent/ES325626A2/en
Expired legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Improvements introduced in the object of the main patent No. 296,397, granted on December 10, 1965, by: "Rotor systems for rotating wing aircraft", characterized in that the hub of the rotor has a central portion, fixed to a driving member of the rotor and a blade mounting extension for each of the rotor blades, each of these rotor blades, has an elongated internal terminal portion, arranged at least predominantly in depth and collateral relationship with a corresponding extension of the shovel, with support means that articulately connect each blade extension prolongation to an internal terminal portion, of the corresponding blade of the rotor, about an axis extended longitudinally, with respect to the corresponding blade of the rotor. (Machine-translation by Google Translate, not legally binding)
ES0325626A 1966-04-16 1966-04-16 Rotor systems for rotating wing aircraft. (Machine-translation by Google Translate, not legally binding) Expired ES325626A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES0325626A ES325626A2 (en) 1966-04-16 1966-04-16 Rotor systems for rotating wing aircraft. (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES0325626A ES325626A2 (en) 1966-04-16 1966-04-16 Rotor systems for rotating wing aircraft. (Machine-translation by Google Translate, not legally binding)

Publications (1)

Publication Number Publication Date
ES325626A2 true ES325626A2 (en) 1967-03-16

Family

ID=59268888

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0325626A Expired ES325626A2 (en) 1966-04-16 1966-04-16 Rotor systems for rotating wing aircraft. (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES325626A2 (en)

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Legal Events

Date Code Title Description
FD2A Announcement of lapse in spain

Effective date: 20170629