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US4150920A Expired / Lapsed US ⏱️ 0.0 years remaining

Rotor blade tipweight assembly

Assignee: United States Department of the Army
•
Filing: 1977-12-02
•
Granted: 1979-04-24
•
Expires: 1997-12-02
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Abstract

Abstract Helicopter rotor blades require tip weights for spanwise and chordwise bace to assure that all of the blades rotate in the same track. The improved rotor blade tip weight assembly of the present invention comprises an elongated spar, preferably formed of a reinforced plastic, adapted to be connected at one end thereof to a rotor hub. An aft fairing structure is carried by the spar and a balancing weight assembly is bonded and/or cured in place within the spar, proximate the free end thereof. The balancing weight assembly includes, in the preferred form thereof, a fiberglass weight tube housing having a pair of internally threaded weight tubes positioned therewithin. The weight tubes form bores having longitudinal axes in a common, substantially horizontal plane, and the axes each extend in a direction parallel to the axis of the spar. One or a plurality of externally threaded cylindrical weights are locked in each weight tube during balancing of the rotor blade.

Inventors

  • 👤 Raymond P. Belko
  • 👤 Robert C. Huss

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 20:39
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/008; B64C27/32; B64C27/46; B64C27/473

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 162 words
A rotor blade balancing weight assembly secured within the rotor blade spar proximate the free-end thereof, said balancing weight assembly including a weight tube housing, a cylindrical weight tube fixed within said housing, positioned with its longitudinal axis parallel to the longitudinal axis of the spar, said weight tube being internally threaded, forming an internally threaded bore, cylindrical balancing weights within the weight tube, said weights having outside diameter equal to the inside diameter of the weight tube, said weights being externally threaded with threads which matingly match the internal threads of the weight tube, the threads being such that a fit engagement is obtained preventing a weight from moving within the weight tube while allowing the weights to be positioned independently within the weight tube to provide both spanwise and chordwise rotor blade balance, means for turning the weights within the tubes to position them within the tube, and a blade tip cover member covering the free-end tip of the spar.
Claim 2
Dependent Claim 162 words
A rotor blade balancing weight assembly secured within the rotor blade spar proximate the free-end thereof, said balancing weight assembly including a weight tube housing, a cylindrical weight tube fixed within said housing, positioned with its longitudinal axis parallel to the longitudinal axis of the spar, said weight tube being internally threaded, forming an internally threaded bore, cylindrical balancing weights within the weight tube, said weights having outside diameter equal to the inside diameter of the weight tube, said weights being externally threaded with threads which matingly match the internal threads of the weight tube, the threads being such that a fit engagement is obtained preventing a weight from moving within the weight tube while allowing the weights to be positioned independently within the weight tube to provide both spanwise and chordwise rotor blade balance, means for turning the weights within the tubes to position them within the tube, and a blade tip cover member covering the free-end tip of the spar.
Claim 3
Dependent Claim 48 words
The balancing weight assembly of claim 1 including two threaded weight tubes fixed within the weight tube housing, each of said weight tubes having a longitudinal axis parallel to the axis of the spar, said tubes being positioned within a common plane, and threaded weights within the tubes.
Claim 4
Dependent Claim 18 words
The balancing weight assembly of claim 1 wherein the spar is formed at least in part of fiberglass.

References Cited (Backward Citations)

US2430948A Cited
US3018832A Cited
US3103977A Cited
US3237697A Cited
US3323597A Cited
US3310117A Cited
US3999888A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-04-23 1982-10-23 1983-04-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-04-23 1986-10-23 1987-04-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-04-23 1990-10-23 1991-04-24 $7700.00 Window Closed / Lapsed

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