Patent US5020741A successfully refreshed from Google Patents.
US5020741A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft propeller with improved electrically de-icer leads
Assignee: HARTZELL PROPELLER Inc A CORP OF OH
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Filing: 1989-12-07
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Granted: 1991-06-04
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Expires: 2009-12-07
Abstract
Abstract A multiple blade aircraft propeller hub has a bulkhead supporting concentric slip rings connected by slide blocks to the aircraft electrical system. Electrical conducting flexible leads connect the slip rings to electrical heating elements or de-icing boots carried by the propeller blades. Each of the leads includes an elongated flexible braided copper tube for conducting electricity and which loosely surrounds a flexible multiple strand stainless steel cable, and an extruded flexible vinyl insulating tube loosely surrounds the braided tube. The leads provide for minimizing stresses and metal fatigue in the electrical conducting braided tube with changes in blade pitch and thereby provide for a substantially extended service life.
Inventors
- 👤 David E. Ziegler
- 👤 Arthur J. Bowser
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 10:19
CPC Classifications
B; B64; B64D; B64D15/00; B64D15/12; H; H01; H01B; H01B7/00; H01B7/17; H01B7/18; H01B7/22; H01B7/221; H01B7/223; H02; H02G; H02G11/00
Claims Analysis
Total Claims: 18
Claim 1
Independent Claim
172 words
A propeller assembly for use on an aircraft having an electrical power supply system, said assembly comprising a propeller hub, a plurality of angularly disposed adjustable pitch propeller blades supported by said hub, an electrical heating element carried by each said blade for de-icing said blade, means for conducting electricity from the aircraft power supply system to said heating elements, said conducting means including a plurality of elongated flexible leads, each of said leads having an intermediate portion connecting opposite end portions and including an elongated flexible element, a flexible braided tube of electrical conducting material surrounding said flexible element, said braided tube having sufficient clearance with said flexible element to provide for free axial movement of said braided tube on said flexible element along said intermediate portion of said lead in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and electrical connecting means for said opposite end portions of said leads and connected to said flexible element and said braided tube.
Claim 2
Dependent Claim
172 words
A propeller assembly for use on an aircraft having an electrical power supply system, said assembly comprising a propeller hub, a plurality of angularly disposed adjustable pitch propeller blades supported by said hub, an electrical heating element carried by each said blade for de-icing said blade, means for conducting electricity from the aircraft power supply system to said heating elements, said conducting means including a plurality of elongated flexible leads, each of said leads having an intermediate portion connecting opposite end portions and including an elongated flexible element, a flexible braided tube of electrical conducting material surrounding said flexible element, said braided tube having sufficient clearance with said flexible element to provide for free axial movement of said braided tube on said flexible element along said intermediate portion of said lead in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and electrical connecting means for said opposite end portions of said leads and connected to said flexible element and said braided tube.
Claim 3
Dependent Claim
44 words
A propeller assembly as defined in claim 1 wherein said insulating tube of each said lead has sufficient clearance with said braided tube to provide for free axial movement of said insulating tube on said braided tube along said intermediate portion of said lead.
Claim 4
Dependent Claim
24 words
A propeller assembly as defined in claim 1 wherein said flexible element, said braided tube and said insulating tube have generally the same length.
Claim 5
Dependent Claim
23 words
A propeller assembly as defined in claim 1 wherein said insulating tube is substantially transparent to permit visual inspection of said braided tube.
Claim 6
Dependent Claim
43 words
A propeller assembly as defined in claim 1 wherein said flexible element comprises a cable having multiple twisted strands each having multiple twisted wires, and said connecting means secures opposite end portions of said braided tube to corresponding end portions of said cable.
Claim 7
Dependent Claim
32 words
A propeller assembly as defined in claim 1 wherein said electrical connecting means comprise metal terminals having base portions securing together corresponding end portions of said element and surrounding said braided tube.
Claim 8
Dependent Claim
21 words
A propeller assembly as defined in claim 1 wherein said insulating tube comprises a section of extruded clear polyvinyl chloride tubing.
Claim 9
Dependent Claim
178 words
A propeller assembly for use on an aircraft having an electrical power supply system, said assembly comprising a propeller hub, a plurality of angularly disposed adjustable pitch propeller blades supported by said hub, an electrical heating element carried by each said blade for de-icing said blade, means for conducting electricity from the aircraft power supply system to said heating elements, said conducting means including a plurality of elongated flexible leads, each of said leads having an intermediate portion connecting opposite end portions and including an elongated non-stretchable flexible cable having multiple twisted strands each having multiple twisted wires, a flexible braided tube of electrical conducting material surrounding said cable, said braided tube having sufficient clearance with said cable to provide for free axial movement of said braided tube on said cable along said intermediate portion of said lead in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and electrical connecting means for said opposite end portions of said leads and connected to said cable and said braided tube.
Claim 10
Dependent Claim
178 words
A propeller assembly for use on an aircraft having an electrical power supply system, said assembly comprising a propeller hub, a plurality of angularly disposed adjustable pitch propeller blades supported by said hub, an electrical heating element carried by each said blade for de-icing said blade, means for conducting electricity from the aircraft power supply system to said heating elements, said conducting means including a plurality of elongated flexible leads, each of said leads having an intermediate portion connecting opposite end portions and including an elongated non-stretchable flexible cable having multiple twisted strands each having multiple twisted wires, a flexible braided tube of electrical conducting material surrounding said cable, said braided tube having sufficient clearance with said cable to provide for free axial movement of said braided tube on said cable along said intermediate portion of said lead in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and electrical connecting means for said opposite end portions of said leads and connected to said cable and said braided tube.
Claim 11
Dependent Claim
44 words
A propeller assembly as defined in claim 8 wherein said insulating tube of each said lead has sufficient clearance with said braided tube to provide for free axial movement of said insulating tube on said braided tube along said intermediate portion of said lead.
Claim 12
Dependent Claim
23 words
A propeller assembly as defined in claim 8 wherein said insulating tube is substantially transparent to permit visual inspection of said braided member.
Claim 13
Dependent Claim
104 words
An improved elongated flexible lead adapted for use on an aircraft, said lead comprising an elongated non-stretchable flexible cable having multiple twisted strands each having multiple twisted wires and providing for a limited degree of flexibility, a flexible braided tube of electrical conducting material surrounding said cable, said braided tube having sufficient clearance with said cable to provide for free axial movement of said braided tube on said cable along the length of said cable in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and means connected to said braided tube for conducting electricity.
Claim 14
Dependent Claim
104 words
An improved elongated flexible lead adapted for use on an aircraft, said lead comprising an elongated non-stretchable flexible cable having multiple twisted strands each having multiple twisted wires and providing for a limited degree of flexibility, a flexible braided tube of electrical conducting material surrounding said cable, said braided tube having sufficient clearance with said cable to provide for free axial movement of said braided tube on said cable along the length of said cable in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and means connected to said braided tube for conducting electricity.
Claim 15
Dependent Claim
40 words
A flexible lead as defined in claim 11 wherein said insulating tube has sufficient clearance with said braided tube to provide for free axial movement of said insulating tube on said braided tube along the length of said braided tube.
Claim 16
Dependent Claim
19 words
A flexible lead as defined in claim 11 wherein said twisted wires of said cable comprise stainless steel wires.
Claim 17
Dependent Claim
17 words
A flexible lead as defined in claim 11 wherein said flexible braided tube comprises braided copper wires.
Claim 18
Dependent Claim
23 words
A flexible lead as defined in claim 11 wherein said insulating tube is substantially transparent to permit visual inspection of said braided tube.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1994-06-03 | 1994-12-03 | 1995-06-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-06-03 | 1998-12-03 | 1999-06-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-06-03 | 2002-12-03 | 2003-06-04 | $7700.00 | Window Closed / Lapsed |