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US4863351A Expired / Lapsed US ⏱️ 0.0 years remaining

Airscrew or propeller for propelling an aircraft

Assignee: RHEIN FLUGZEUG GmbH
•
Filing: 1989-01-19
•
Granted: 1989-09-05
•
Expires: 2009-01-19
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Abstract

Abstract An airscrew for propelling an aircraft has a hub, a jacket and a plurality of propeller blades secured by blade necks to the hub. These blade necks are secured to the hub with symmetric or equal angular spacings around the hub between neighboring radial blade neck axes. Each propeller blade has a longitudinal axis. At least certain of these longitudinal blade axes extend at different sweep angles relative to the respective radial blade neck axis. When the sweep angle is positive the respective sweep of the blade is a positive sweepback with a trailing sweep of the respective blade relative to a rotational direction of the airscrew. When the sweep angle is negative the respective sweep of the blade is a negative sweep forward with a leading sweep of the respective blade relative to a rotational direction of the airscrew. These differing sweep angles achieve a substantial noise reduction compared to conventional airscrews having a completely symmetrical construction.

Inventors

  • 👤 Hans-Otto Fischer
  • 👤 Karl H. Gronau

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 19:16
CPC Classifications
B; B64; B64C; B64C11/00; B64C11/001

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 152 words
An airscrew for propelling an aircraft, comprising a hub defining a rotational axis, a plurality of propeller blades, each propeller blade having a central longitudinal blade axis, a blade neck having a radial neck axis extending radially to said rotational axis for securing each propeller blade to said hub, each blade neck having a radially inner end operatively connected to said hub and a radially outer end operatively connected to its respective propeller blade so that all blade necks are spaced from each other at equal angular spacings between neighboring radial neck axes, each propeller blade being connected to its respective blade neck so that at least certain propeller blades of said plurality of propeller blades have sweep angles (φ) that differ from the sweep angles of other propeller blades of said airscrew, said sweep angle being defined as an angle between said radial neck axis and the respective longitudinal blade axis.
Claim 2
Dependent Claim 152 words
An airscrew for propelling an aircraft, comprising a hub defining a rotational axis, a plurality of propeller blades, each propeller blade having a central longitudinal blade axis, a blade neck having a radial neck axis extending radially to said rotational axis for securing each propeller blade to said hub, each blade neck having a radially inner end operatively connected to said hub and a radially outer end operatively connected to its respective propeller blade so that all blade necks are spaced from each other at equal angular spacings between neighboring radial neck axes, each propeller blade being connected to its respective blade neck so that at least certain propeller blades of said plurality of propeller blades have sweep angles (φ) that differ from the sweep angles of other propeller blades of said airscrew, said sweep angle being defined as an angle between said radial neck axis and the respective longitudinal blade axis.
Claim 3
Dependent Claim 31 words
The airscrew of claim 1, wherein said different sweep angles include positive sweep angles, whereby the respective blade has a trailing sweep relative to a direction of rotation of said airscrew.
Claim 4
Dependent Claim 32 words
The airscrew of claim 1, wherein said different sweep angles include negative sweep forward angles, whereby the respective blade has a leading sweep relative to a direction of rotation of said airscrew.
Claim 5
Dependent Claim 17 words
The airscrew of claim 1, wherein said propeller blades have straight leading edges and straight trailing edges.
Claim 6
Dependent Claim 17 words
The airscrew of claim 1, wherein said propeller blades have curved leading edges and curved trailing edges.
Claim 7
Dependent Claim 17 words
The airscrew of claim 1, wherein said propeller blades have sickle-shaped leading edges and sickle-shaped trailing edges.
Claim 8
Dependent Claim 15 words
The airscrew of claim 1, wherein said sweep angles are within the range of 0°±30°.

References Cited (Backward Citations)

US360833A Cited
US2134660A Cited
DD138699A1 Cited
US4306839A Cited
DE3608565A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-09-04 1993-03-06 1993-09-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-09-04 1997-03-06 1997-09-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-09-04 2001-03-06 2001-09-05 $7700.00 Window Closed / Lapsed

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