FR2449592A1 - PLANE PROVIDED WITH GOVERNOR SURFACES ARRANGED IN FRONT AND BEHIND THE CENTER OF GRAVITY - Google Patents
PLANE PROVIDED WITH GOVERNOR SURFACES ARRANGED IN FRONT AND BEHIND THE CENTER OF GRAVITYInfo
- Publication number
- FR2449592A1 FR2449592A1 FR8001343A FR8001343A FR2449592A1 FR 2449592 A1 FR2449592 A1 FR 2449592A1 FR 8001343 A FR8001343 A FR 8001343A FR 8001343 A FR8001343 A FR 8001343A FR 2449592 A1 FR2449592 A1 FR 2449592A1
- Authority
- FR
- France
- Prior art keywords
- governor
- gravity
- behind
- center
- surfaces arranged
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Abstract
A.AVION COMPORTANT DES SURFACES DE GOUVERNE SUPPLEMENTAIRES REGLABLES AU MOYEN DE SERVO-MOTEURS. B.AVION CARACTERISE EN CE QUE LE SERVO-MOTEUR 5 D'UNE SURFACE DE GOUVERNE SUPPLEMENTAIRE 2 COMPORTE UN ORGANE A DEPLACEMENT LIBRE 12, 13 POUR PERMETTRE L'EFFACEMENT DE LA SURFACE DE GOUVERNE 2 EN FONCTION DE L'ECOULEMENT, CET ORGANE POUVANT ETRE MIS HORS-CIRCUIT PAR UN SIGNAL DE COMMANDE 14 POUR REGLER LA POSITION DE LA SURFACE DE GOUVERNE 2 EN VUE DE MANOEUVRES DE VOL DETERMINEES. C.DISPOSITION APPLICABLE NOTAMMENT AUX AVIONS DE COMBAT.A. AIRPLANE INCLUDING ADDITIONAL GOVERNING SURFACES ADJUSTABLE BY MEANS OF SERVO-MOTORS. B. AIRPLANE CHARACTERIZED IN THAT THE SERVO MOTOR 5 OF AN ADDITIONAL RUDDER SURFACE 2 INCLUDES A FREE-MOVING ORGAN 12, 13 TO ALLOW THE ERASING OF THE RUDDER SURFACE 2 AS A FUNCTION OF THE FLOW, THIS ORGAN BEING ABLE BE DISCONNECTED BY A CONTROL SIGNAL 14 TO ADJUST THE POSITION OF THE STEERING SURFACE 2 FOR DETERMINED FLIGHT MANEUVERS. C. PROVISION APPLICABLE IN PARTICULAR TO COMBAT AIRCRAFT.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19792906889 DE2906889C2 (en) | 1979-02-22 | 1979-02-22 | Airplane with control surfaces in front of and behind the center of gravity |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2449592A1 true FR2449592A1 (en) | 1980-09-19 |
FR2449592B1 FR2449592B1 (en) | 1984-11-23 |
Family
ID=6063635
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8001343A Granted FR2449592A1 (en) | 1979-02-22 | 1980-01-22 | PLANE PROVIDED WITH GOVERNOR SURFACES ARRANGED IN FRONT AND BEHIND THE CENTER OF GRAVITY |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE2906889C2 (en) |
FR (1) | FR2449592A1 (en) |
GB (1) | GB2043562B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0680877A1 (en) * | 1994-05-03 | 1995-11-08 | AEROSPATIALE Société Nationale Industrielle | Transport aircraft with forward mounted stabilizer |
EP0953504A1 (en) | 1998-04-29 | 1999-11-03 | Aerospatiale Societe Nationale Industrielle | Aircraft with reduced wing loads |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2112757A (en) * | 1935-03-03 | 1938-03-29 | Billioque Elie Jean Henri | Stabilizing device for aeroplanes |
FR2405869A1 (en) * | 1977-10-17 | 1979-05-11 | Onera (Off Nat Aerospatiale) | Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2355979B2 (en) * | 1973-11-09 | 1976-12-02 | Dornier Gmbh, 7990 Friedrichshafen | ADDITIONAL CONTROL DEVICE FOR AIRCRAFT |
-
1979
- 1979-02-22 DE DE19792906889 patent/DE2906889C2/en not_active Expired
-
1980
- 1980-01-22 FR FR8001343A patent/FR2449592A1/en active Granted
- 1980-02-21 GB GB8005928A patent/GB2043562B/en not_active Expired
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2112757A (en) * | 1935-03-03 | 1938-03-29 | Billioque Elie Jean Henri | Stabilizing device for aeroplanes |
FR2405869A1 (en) * | 1977-10-17 | 1979-05-11 | Onera (Off Nat Aerospatiale) | Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0680877A1 (en) * | 1994-05-03 | 1995-11-08 | AEROSPATIALE Société Nationale Industrielle | Transport aircraft with forward mounted stabilizer |
FR2719548A1 (en) * | 1994-05-03 | 1995-11-10 | Aerospatiale | Transport plane with front empennage. |
US5722615A (en) * | 1994-05-03 | 1998-03-03 | Aerospatiale Societe Nationale Indusrielle | Transport airplane with front empennage |
EP0953504A1 (en) | 1998-04-29 | 1999-11-03 | Aerospatiale Societe Nationale Industrielle | Aircraft with reduced wing loads |
FR2778163A1 (en) | 1998-04-29 | 1999-11-05 | Aerospatiale | AIRCRAFT WITH LOWER SAIL EFFORTS |
Also Published As
Publication number | Publication date |
---|---|
FR2449592B1 (en) | 1984-11-23 |
DE2906889A1 (en) | 1980-09-04 |
DE2906889C2 (en) | 1986-06-26 |
GB2043562B (en) | 1983-03-09 |
GB2043562A (en) | 1980-10-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse |