US1798299A - Rotary flexible propeller - Google Patents
Rotary flexible propeller Download PDFInfo
- Publication number
- US1798299A US1798299A US243732A US24373227A US1798299A US 1798299 A US1798299 A US 1798299A US 243732 A US243732 A US 243732A US 24373227 A US24373227 A US 24373227A US 1798299 A US1798299 A US 1798299A
- Authority
- US
- United States
- Prior art keywords
- rotary flexible
- flexible propeller
- flexible
- propeller
- wings
- 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 - Lifetime
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
Definitions
- wings should be constructed with a fore edge whose resistance decreases in the direction of arrow A, and also in the plane in direction v of arrow B to provide the flexible surface C, thus producing a larger and more flexible surface (Fig. 1)- which even when rotating with a smaller radius than the peripherical zone as regards the axis R possesses a greater flexibility with more parts normal to axis H (Fig. 2) which may be deflected, the eificiency consequently becoming very high.
- Fig. 3 shows a wing without the surface C inscribed in Fig. 1, and consequently of a very scarce efiiciency during flexures.
- a flexible rotating propeller blade having its fore edge proportioned in thickness to the resistance made in movement, the rear edge of the blade terminating in a prolonged section having greater flexibility than the blade, said section having its medial line in the central zone of the blade.
Description
March 31, 1931. u. ANTON! 1,798,299
' ROTARY FLEXIBLE PROPELLER J Filed D90.- 30, 1927 a. in/am' Patented Mar. 31, 1931 i Q UNITED AsTATs PATENT OFFICE UGO ANTONI, 02B VIABEGGIO, 'I'LPALY 1210mm FLEXIBLE PBOPELLER Application filed December 30, 1927, Serial No. 243,732, and in Italy December 31, 1928.
It is well known that according'to practice and experience, rotary flexible propellers cannot reach a degree of perfection required for their use if the plane of the wings per- 5 pendicular to the driving axle cannot be deformed.
In preceding inventions of applicant the method was tried to have a gradual diminution of the wings thickness but it was not possible to obtain a distribution of the clasticity inversely proportional to the resistance met by the wings on the axis of rotation.
To prevent said inconvenience and obtain a greater efficiency applicant has found that wings should be constructed with a fore edge whose resistance decreases in the direction of arrow A, and also in the plane in direction v of arrow B to provide the flexible surface C, thus producing a larger and more flexible surface (Fig. 1)- which even when rotating with a smaller radius than the peripherical zone as regards the axis R possesses a greater flexibility with more parts normal to axis H (Fig. 2) which may be deflected, the eificiency consequently becoming very high.
Fig. 3 shows a wing without the surface C inscribed in Fig. 1, and consequently of a very scarce efiiciency during flexures.
Having now particularly described and ascertained the nature of my said invention andin what manner the. same is to be performed I declare that what I claim is:
A flexible rotating propeller blade having its fore edge proportioned in thickness to the resistance made in movement, the rear edge of the blade terminating in a prolonged section having greater flexibility than the blade, said section having its medial line in the central zone of the blade.
In testimony whereof I have hereunto signed my name.
. UGO ANTONI.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT1798299X | 1926-12-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
US1798299A true US1798299A (en) | 1931-03-31 |
Family
ID=11434649
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US243732A Expired - Lifetime US1798299A (en) | 1926-12-31 | 1927-12-30 | Rotary flexible propeller |
Country Status (1)
Country | Link |
---|---|
US (1) | US1798299A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3275082A (en) * | 1965-08-19 | 1966-09-27 | Robert E Stark | Propellers for water craft |
US3584969A (en) * | 1968-05-25 | 1971-06-15 | Aisin Seiki | Flexible blade fan |
US3822103A (en) * | 1972-01-08 | 1974-07-02 | Aisin Seiki | Flexible fan |
US3914068A (en) * | 1972-01-25 | 1975-10-21 | Sueddeutsche Kuehler Behr | Fan for motor vehicles |
US3915591A (en) * | 1971-12-09 | 1975-10-28 | Aisin Seiki | Flexible blade fan |
US4334824A (en) * | 1979-07-27 | 1982-06-15 | Aisin Seiki Kabushiki Kaisha | Flexible fan device |
-
1927
- 1927-12-30 US US243732A patent/US1798299A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3275082A (en) * | 1965-08-19 | 1966-09-27 | Robert E Stark | Propellers for water craft |
US3584969A (en) * | 1968-05-25 | 1971-06-15 | Aisin Seiki | Flexible blade fan |
US3915591A (en) * | 1971-12-09 | 1975-10-28 | Aisin Seiki | Flexible blade fan |
US3822103A (en) * | 1972-01-08 | 1974-07-02 | Aisin Seiki | Flexible fan |
US3914068A (en) * | 1972-01-25 | 1975-10-21 | Sueddeutsche Kuehler Behr | Fan for motor vehicles |
US4334824A (en) * | 1979-07-27 | 1982-06-15 | Aisin Seiki Kabushiki Kaisha | Flexible fan device |
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