US1676572A - Propelling or lifting device with automatic correction - Google Patents
Propelling or lifting device with automatic correction Download PDFInfo
- Publication number
- US1676572A US1676572A US185858A US18585827A US1676572A US 1676572 A US1676572 A US 1676572A US 185858 A US185858 A US 185858A US 18585827 A US18585827 A US 18585827A US 1676572 A US1676572 A US 1676572A
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- US
- United States
- Prior art keywords
- blades
- sides
- propelling
- lifting device
- automatic correction
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- 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.)
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/37—Rotors having articulated joints
Definitions
- the present invention relates to a pro'peL ling 0r lifting apparatus of the kind in which the blades are connected with the main axis of rotation by a device which ,comprisesone or more joints by which the blades are allowed to oscillate and which suitably combines the diametrically opposite blades in such manner as to assure the mechanical balancing of the apparatus irrespectively of the position of the blades, while permitting the said blades, by symmetrical modifications in the trajectory or the incidence, to automatically equalize the aerodynamic reactions upon the opposite blades, whatever may be the irregularities in the sustaining atmosphere.
- the connecting mechanism comprises a jointed parallelogram whereof two opposite sides are articulated in the middle of their length on the driving shaft and whereof the two other sides, directed parallelly to the said shaft, carry the blades. These latter may be mounted upon the said sides either rigidly or in a pivoting manner, their axis of pivotation being thus directed perpendicularly to the driving shaft.
- the blades mounted in this manner remain parallel to themselves during their displacements in the direction parallel to the axis of rotation; for a given displacement of the center of each blade, the outer end of this latter moves by the same amount as the said center, so that for an equal efficiency, the whole of the propeller thus arranged is less cumbersome as the analogous propellers, the blades of which oscillate about a transverse axis.
- Fig.- 1 shows a propeller provided with two blades which are rigidly secured upon the sides of the parallelogram.
- Fig. 2 shows a propeller, the blades of which are pivotally mounted upon the sides of the parallelogram.
- w indicates the axis of the driving shaft.
- said shaft are articulated at c and d, the middle of two sides e e and f f of a jointed parallelogram.
- the two other sides e f and e f of the latter car the propellers blades p and p.
- the said blades are rigidly secured upon the sides e f and e f respectively.
- the blades 1) and p are integral with shafts s 8 which are pivoted in brackets '10, w integral with the sides a f, e f and these shafts are connect- 'ed together through an intermediary shaft to which they are coupled by means of Cardan joints 4) and '12. It results therefrom that the shafts s .9 although they remain in a direction perpendicular to the axis as w, are obliged to rotate conjointly with the blades p p, so that as the angle of incidence of one of these blades increases, the
- a propelling or lifting device the combination of a driving shaft, a jointed parallelogram whereof two opposite sides are jointed at their middle to the said driving shaft, and two blades pivoted to the two other sides of the said parallelogram, the axis of pivotation of every blade being placed in a direction substantially perpendicular to that of the respective side carrying the same.
- a propelling or lifting device the combination of a drivingshaft, a. jointed parallelogram whereof two opposite sides are jointed at their middle to the said driving" shaft, two blades pivoted to the two other sides of the said parallelogram, the axis of 'pivotation of every blade being placed in a direction substantially perpendicular to that of the respective side carrying the same, and a transverse shaft whose ends are jointed to the inner ends of the blades.
Description
July 10,1928. 1,676,572
E; OEHMICHEN PROPELLING 0R LIF'IING DEVICE WITH AUTOMATIC CORRECTION Filed April 22, 1927 Patented July 10, 1928.
PATENT OFFICE.
. ETIENNE OEHMICHEN, OF VALENTIGNEY, FRANCE.
PROPELLING OR LIFTING DEVICE WITH AUTOMATIC CORRECTION,
Application filed April 22, 1927, Serial INCL-185,858, and in France May 31, 1926.
The present invention relates to a pro'peL ling 0r lifting apparatus of the kind in which the blades are connected with the main axis of rotation by a device which ,comprisesone or more joints by which the blades are allowed to oscillate and which suitably combines the diametrically opposite blades in such manner as to assure the mechanical balancing of the apparatus irrespectively of the position of the blades, while permitting the said blades, by symmetrical modifications in the trajectory or the incidence, to automatically equalize the aerodynamic reactions upon the opposite blades, whatever may be the irregularities in the sustaining atmosphere.
According to the present invention, the connecting mechanism comprises a jointed parallelogram whereof two opposite sides are articulated in the middle of their length on the driving shaft and whereof the two other sides, directed parallelly to the said shaft, carry the blades. These latter may be mounted upon the said sides either rigidly or in a pivoting manner, their axis of pivotation being thus directed perpendicularly to the driving shaft. In all cases, the blades mounted in this manner remain parallel to themselves during their displacements in the direction parallel to the axis of rotation; for a given displacement of the center of each blade, the outer end of this latter moves by the same amount as the said center, so that for an equal efficiency, the whole of the propeller thus arranged is less cumbersome as the analogous propellers, the blades of which oscillate about a transverse axis.
Two embodiments of the object of the invention are represented, by way of example, in the diagrammatic annexed drawings.
Fig.- 1 shows a propeller provided with two blades which are rigidly secured upon the sides of the parallelogram.
Fig. 2 shows a propeller, the blades of which are pivotally mounted upon the sides of the parallelogram.
a; w indicates the axis of the driving shaft. Upon the said shaft are articulated at c and d, the middle of two sides e e and f f of a jointed parallelogram. The two other sides e f and e f of the latter car the propellers blades p and p.
According to Fig. 1, the said blades are rigidly secured upon the sides e f and e f respectively.
It is shown that if the blade p rises, the blade ;0 is lowered by an equal amount and vice-versa, the said two blades remaining always parallel to an invariable direction, since the sides e j, e f remain parallel to the axis as a7;
In the case of Fig. 2, the blades 1) and p are integral with shafts s 8 which are pivoted in brackets '10, w integral with the sides a f, e f and these shafts are connect- 'ed together through an intermediary shaft to which they are coupled by means of Cardan joints 4) and '12. It results therefrom that the shafts s .9 although they remain in a direction perpendicular to the axis as w, are obliged to rotate conjointly with the blades p p, so that as the angle of incidence of one of these blades increases, the
incidence of the other diminishes, and viceversa.
It is obvious that the preceding considerations concerning a double-blade devicemay be applied to a propeller containing any number of blades, with the sole condition that they are to be mounted in pairs or in groups which may be superposed.
Having thus described my apparatus, what I claim as new therein, and my own invention, is: I
1. In a propelling or lifting device, the, combination of a driving shaft, a jointed parallelogram whereof two opposite. sides are jointed at their middle to the said driving shaft, and two blades carried by. the v,
two other sides of the said parallelogram. 2. In a propelling or lifting device, the combination of a driving shaft, a jointed parallelogram whereof two opposite sides are jointed at their middle to the said driving shaft, and two blades pivoted to the two other sides of the said parallelogram, the axis of pivotation of every blade being placed in a direction substantially perpendicular to that of the respective side carrying the same.
3. In a propelling or lifting device, the combination of a drivingshaft, a. jointed parallelogram whereof two opposite sides are jointed at their middle to the said driving" shaft, two blades pivoted to the two other sides of the said parallelogram, the axis of 'pivotation of every blade being placed in a direction substantially perpendicular to that of the respective side carrying the same, and a transverse shaft whose ends are jointed to the inner ends of the blades.
In testimony whereof I have hereunto affixed my signature.
ETIENNE OEHMICHEN.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1676572X | 1926-05-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
US1676572A true US1676572A (en) | 1928-07-10 |
Family
ID=9680119
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US185858A Expired - Lifetime US1676572A (en) | 1926-05-31 | 1927-04-22 | Propelling or lifting device with automatic correction |
Country Status (1)
Country | Link |
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US (1) | US1676572A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4297080A (en) * | 1979-12-17 | 1981-10-27 | United Technologies Corporation | Rotor blade pitch control linkage |
-
1927
- 1927-04-22 US US185858A patent/US1676572A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4297080A (en) * | 1979-12-17 | 1981-10-27 | United Technologies Corporation | Rotor blade pitch control linkage |
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