FR2628063A1 - Human powered helicopter - has upper rotor powered directly by hand crank assisted by foot crank pulley and cables also driving lower rotor in opposite direction - Google Patents
Human powered helicopter - has upper rotor powered directly by hand crank assisted by foot crank pulley and cables also driving lower rotor in opposite direction Download PDFInfo
- Publication number
- FR2628063A1 FR2628063A1 FR8802702A FR8802702A FR2628063A1 FR 2628063 A1 FR2628063 A1 FR 2628063A1 FR 8802702 A FR8802702 A FR 8802702A FR 8802702 A FR8802702 A FR 8802702A FR 2628063 A1 FR2628063 A1 FR 2628063A1
- Authority
- FR
- France
- Prior art keywords
- pulley
- helicopter
- crank
- assisted
- cables
- 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
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/04—Man-powered aircraft
Abstract
Description
() RÉPUBLIQUE FRAN AISE N de publication 2 628 063 (à n'utiliser que() FRENCH REPUBLIC Publication No. 2 628 063 (use only
pour les INSTITUT NATIONAL commandes de reproduction) DE LA PROPRIÉTÉ INDUSTRIELLE( N d'enregistrement national 88 02702 PARIS for NATIONAL INSTITUTE reproduction orders) OF INDUSTRIAL PROPERTY (National registration number 88 02702 PARIS
Q Int CI': B 64 C 31/04.Q Int CI ': B 64 C 31/04.
@ DEMANDE DE BREVET D'INVENTION A1@ A1 PATENT APPLICATION
__
( Date de dépôt: 3 mars 1988. t Demandeur(s): MOUROUX Louis. - FR. (Date of filing: March 3, 1988. t Applicant (s): MOUROUX Louis. - FR.
) Priorité) Priority
( Inventeur(s) Louis Mouroux.(Inventor (s) Louis Mouroux.
_ Date de la mise à disposition du public de la _ Date of public availability of the
demande: BOPI " Brevets " n 36 du 8 septembre 1989. application: BOPI "Patents" n 36 of September 8, 1989.
Références à d'autres documents nationaux appa- References to other national documents appearing
rentés: () Titulaire(s): _ Mandataire(s) Hélicoptère actionné par la force musculaire humaine. Aéronef de type hélicoptère actionné par la force muscu- 1 ? rentés: () Holder (s): _ Agent (s) Helicopter operated by human muscular force. Muscular force powered helicopter type aircraft 1?
laire dont les hélices tournent en sens inverse. area whose propellers rotate in opposite directions.
La force musculaire des bras et des jambes est captée et additionnée pour faire tourner les hélices._ Système mécanique comportant une seule courroie à l'aide, de poulies et de renvois capte l'énergie des bras et des The muscular force of the arms and legs is captured and added to rotate the propellers._ Mechanical system comprising a single belt using, pulleys and deflections captures the energy of the arms and
jambes et la distribue aux hélices. legs and distributes it to the propellers.
(o N C44 Hélicoptére actionné par la force musculaire humaine l'invention concerne un hélicoptère actionné par la force humaine destiné à s'élever dans l'air Pour tirer le maximum d'énergie de 1 'étre humain il est utilisé la force des bras plus la force des ja-mbes Un mécanisme décrit permet de capter l'énergie des jambes et des bras et de les transmettre aux (o N C44 Helicopter actuated by human muscular force the invention relates to a helicopter actuated by human force intended to rise in the air To draw the maximum energy from one human being the force of the arms is used plus the strength of the ja-mbes A mechanism described makes it possible to capture the energy of the legs and arms and to transmit them to
voiles hélices tournant en sens inverse. propeller sails rotating in opposite directions.
on trouve I hélice à prise directe 2 axe de l'hélice -0 à prise directe 3 poulie goupillée sur l'axe de prise directe 4 manivelle à main commandant l'axe de prise directe 5 rotule de manivelle à main 6 poulie du pédalier commandé par les pieds 7 poulie 'de l'hélice à sens inverse solidaire de l'hélice 8 8 hélice à sens inverse tournant librement autour de l'axe 2 9 axe de l'hélice à sens inverse IO poulie de renvoi II poulie de renvoi I2 pédalier vilbrequin commandé par les pieds I3 cabine !0 I4 ressort I5 roue I6 tabouret there is I direct drive propeller 2 propeller axis -0 direct drive 3 pulley pinned on the direct drive shaft 4 hand crank controlling the direct drive shaft 5 ball of hand crank 6 pulley of the pedal drive by the feet 7 pulley 'of the opposite propeller secured to the propeller 8 8 reverse propeller freely rotating around the axis 2 9 axis of the opposite propeller IO deflection pulley II deflection pulley I2 crankshaft crankset controlled by the feet I3 cabin! 0 I4 spring I5 wheel I6 stool
I7 courroie.I7 belt.
I8 renvoi I9 poulie de renvoiI8 return I9 return pulley
2 26280632 2628063
l'axe 2 est commandé en prise directe par la manivelle à main et en même temps par la poulie branchée sur le pédalier 6 qui commande par la courroie I7 la poulie 5 et 1' hélice 1 qui tourne 6 dans un sens l'hélice voile 8 tourne en sens inverse de l'hélice I elle est commndée par la poulie 7 calée sur l'axe 9 tournant autour de l'axe 2 cette poulie 7 reçoit la puissance provenant de la manivelle I2 commandant la poulie 6 poulie 6 par l'intermédiaire de la courroie I7 commande la poulie 7 À Cette poulie 7 reçoit en plus de l'énergie par les pieds, l'énergie fournie par les mains par S l'intermédiaire des renvois I8 et I9 (figure 3) provenant de la manivelle 4etde la poulie 3 la courroie I7 capte et distribue la puissance des pieds I2 et capte la puissance des mains en 4 et 3 la distribue en 7 et 9 à l'hélice 8 en 2o inversant le sens de rotation deux grandes hélices I et 8 tournant en sens inverse en forme de voiles captent l'air pour s'appuyer dessus les hélices ournent en sens inverse pour stabiliser la cabine axis 2 is controlled directly by the hand crank and at the same time by the pulley connected to the crankset 6 which controls the pulley I7 by the belt I7 and the propeller 1 which rotates the sail propeller 6 in one direction 8 rotates in opposite direction to the propeller I it is controlled by the pulley 7 wedged on the axis 9 rotating around the axis 2 this pulley 7 receives the power coming from the crank I2 controlling the pulley 6 pulley 6 by the Intermediate of the belt I7 controls the pulley 7 A This pulley 7 receives in addition to the energy from the feet, the energy supplied by the hands via S through the references I8 and I9 (figure 3) coming from the crank 4 and the pulley 3 the belt I7 captures and distributes the power of the feet I2 and captures the power of the hands in 4 and 3 distributes it in 7 and 9 to the propeller 8 in 2o reversing the direction of rotation two large propellers I and 8 turning in opposite in the shape of sails catch the air to lean on it the propellers turn in opposite direction to stabilize the cabin
26280632628063
revendicationsclaims
I - Aeronef de type hélicoptère actionné par là force musculaire caractérisé en ce que deux hélices tournent en sens inverse, L'une a prise directe ( I), l'autre ( 8) tournant en sens inverse sont actionnées respectivement par une manivelle ( 4) à main et par un pédalier ( I2) I - helicopter-type aircraft operated by muscular force, characterized in that two propellers rotate in opposite directions, one with direct drive (I), the other (8) rotating in opposite directions, are respectively actuated by a crank (4 ) by hand and by a pedal (I2)
utilisant la force des bras et des jambes. using the strength of the arms and legs.
2 - Aeronef selon lcL revendication I caractérisé en ce que on utilise en les additionnant la force musculaire des bras et des jambes; ig2) en captant l'énergie par la manivelle (4) pour les bras, et en captant l'énergie des jambes par le vilbrequin ( I2) on additionne ces deux énergi gies pour actionner les hélices 2 - aircraft according to lcL claim I characterized in that the muscle strength of the arms and legs is used by adding them; ig2) by capturing the energy by the crank (4) for the arms, and by capturing the energy from the legs by the crankshaft (I2), these two energies are added to activate the propellers
3 - Aeronef selon.une quelconque des revendications 3 - aircraft according to any of the claims
précédentes caractérisé en ce que avec une seule courroie on capte la puissance des bras puis celle des jambes et que l'on distribue l'énergie aux deux hélices tournant en sens inverse) (ig 2 et 3). ON capte l'énergie des bras avec la manivelle (4) qui actionne directement l'hélice ( I) et (2) et en même temps la poulie ( 3) solidaire autour de laquelle passe la courroie ( I7). On capte l'énergie des jambes par le vilbrequin( I2) qui actionnne une poulie ( 6) autour de laquelle la courroie ( I7) et les renvois ( IO) et ( II) dirige l'énergie aux disques ( 3) et ( 7) et les fait tourner en sens inverse l'un de l'autre. Les renvoie ( I8) et ( I9) complètent le systéme (9- *T i j.._:.__, r Qq4 A ) G gij2 previous characterized in that with a single belt we capture the power of the arms then that of the legs and that we distribute the energy to the two propellers rotating in opposite directions) (ig 2 and 3). We capture the energy of the arms with the crank (4) which directly actuates the propeller (I) and (2) and at the same time the pulley (3) secured around which the belt (I7) passes. The energy of the legs is captured by the crankshaft (I2) which actuates a pulley (6) around which the belt (I7) and the references (IO) and (II) directs the energy to the discs (3) and (7 ) and rotates them in opposite directions. The returns (I8) and (I9) complete the system (9- * T i j .._: .__, r Qq4 A) G gij2
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8802702A FR2628063B1 (en) | 1988-03-03 | 1988-03-03 | HELICOPTER POWERED BY HUMAN MUSCLE STRENGTH |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8802702A FR2628063B1 (en) | 1988-03-03 | 1988-03-03 | HELICOPTER POWERED BY HUMAN MUSCLE STRENGTH |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2628063A1 true FR2628063A1 (en) | 1989-09-08 |
FR2628063B1 FR2628063B1 (en) | 1995-03-31 |
Family
ID=9363875
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8802702A Expired - Fee Related FR2628063B1 (en) | 1988-03-03 | 1988-03-03 | HELICOPTER POWERED BY HUMAN MUSCLE STRENGTH |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2628063B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2024047413A1 (en) * | 2022-08-31 | 2024-03-07 | Costruzioni E Servizi S.R.L.S. | Human-powered aircraft |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR711996A (en) * | 1930-06-05 | 1931-09-22 | Improvements to air navigation devices | |
FR2307699A1 (en) * | 1975-04-16 | 1976-11-12 | Belalbre Jacques | Lightweight helicopter with twin contra-rotating rotors - has power supplied by small engine supplemented by pedal drive |
-
1988
- 1988-03-03 FR FR8802702A patent/FR2628063B1/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR711996A (en) * | 1930-06-05 | 1931-09-22 | Improvements to air navigation devices | |
FR2307699A1 (en) * | 1975-04-16 | 1976-11-12 | Belalbre Jacques | Lightweight helicopter with twin contra-rotating rotors - has power supplied by small engine supplemented by pedal drive |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2024047413A1 (en) * | 2022-08-31 | 2024-03-07 | Costruzioni E Servizi S.R.L.S. | Human-powered aircraft |
Also Published As
Publication number | Publication date |
---|---|
FR2628063B1 (en) | 1995-03-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |