FR506633A - Rational system for stabilizing and maneuvering the transverse balance of airplanes and their horizontal evolutions - Google Patents

Rational system for stabilizing and maneuvering the transverse balance of airplanes and their horizontal evolutions

Info

Publication number
FR506633A
FR506633A FR506633A FR506633DA FR506633A FR 506633 A FR506633 A FR 506633A FR 506633 A FR506633 A FR 506633A FR 506633D A FR506633D A FR 506633DA FR 506633 A FR506633 A FR 506633A
Authority
FR
France
Prior art keywords
evolutions
airplanes
maneuvering
stabilizing
horizontal
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
FR506633A
Other languages
French (fr)
Inventor
Salvatore De Santis
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.)
SALVATORE DE SANTIS
Original Assignee
SALVATORE DE SANTIS
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 SALVATORE DE SANTIS filed Critical SALVATORE DE SANTIS
Application granted granted Critical
Publication of FR506633A publication Critical patent/FR506633A/en
Expired legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H03—ELECTRONIC CIRCUITRY
    • H03B—GENERATION OF OSCILLATIONS, DIRECTLY OR BY FREQUENCY-CHANGING, BY CIRCUITS EMPLOYING ACTIVE ELEMENTS WHICH OPERATE IN A NON-SWITCHING MANNER; GENERATION OF NOISE BY SUCH CIRCUITS
    • H03B7/00—Generation of oscillations using active element having a negative resistance between two of its electrodes
    • H03B7/02—Generation of oscillations using active element having a negative resistance between two of its electrodes with frequency-determining element comprising lumped inductance and capacitance
    • H03B7/10—Generation of oscillations using active element having a negative resistance between two of its electrodes with frequency-determining element comprising lumped inductance and capacitance active element being gas-discharge or arc-discharge tube
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR506633A 1919-11-27 1919-11-27 Rational system for stabilizing and maneuvering the transverse balance of airplanes and their horizontal evolutions Expired FR506633A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR506633T 1919-11-27

Publications (1)

Publication Number Publication Date
FR506633A true FR506633A (en) 1920-08-26

Family

ID=86325491

Family Applications (1)

Application Number Title Priority Date Filing Date
FR506633A Expired FR506633A (en) 1919-11-27 1919-11-27 Rational system for stabilizing and maneuvering the transverse balance of airplanes and their horizontal evolutions

Country Status (1)

Country Link
FR (1) FR506633A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4865274A (en) * 1988-04-29 1989-09-12 United Technologies Corporation Passive control assembly for gliding device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4865274A (en) * 1988-04-29 1989-09-12 United Technologies Corporation Passive control assembly for gliding device

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