GB1291562A - Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades - Google Patents
Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller bladesInfo
- Publication number
- GB1291562A GB1291562A GB5017168A GB5017168A GB1291562A GB 1291562 A GB1291562 A GB 1291562A GB 5017168 A GB5017168 A GB 5017168A GB 5017168 A GB5017168 A GB 5017168A GB 1291562 A GB1291562 A GB 1291562A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- propeller blades
- reinforced
- relating
- construction
- 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
Links
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
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/26—Fabricated blades
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
1291562 Moulding propeller blades HAWKER SIDDELEY DYNAMICS Ltd 16 Oct 1969 [22 Oct 1968] 50171/68 Heading B5A [Also in Division B7] In a method of manufacturing a propeller blade a longitudinal load-carrying spar 11 built up from synthetic resin material reinforced with longitudinally extending carbon fibres is disposed within a containing shell 12. In the embodiment shown two individual half-blades are separately moulded, without a blade shank or root portion, in a reinforced resin material further reinforced with longitudinally laid carbon fibres and are then bonded together. The blade shank and root are then formed by compressing the protruding ends 19 of the carbon whiskers from both halves of the blade between male and female moulds 20, 21.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5017168A GB1291562A (en) | 1968-10-22 | 1968-10-22 | Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades |
| FR6936177A FR2040956A5 (en) | 1968-10-22 | 1969-10-22 | |
| DE19691954062 DE1954062A1 (en) | 1968-10-22 | 1969-10-22 | Propeller blade and process for its manufacture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5017168A GB1291562A (en) | 1968-10-22 | 1968-10-22 | Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1291562A true GB1291562A (en) | 1972-10-04 |
Family
ID=10454929
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB5017168A Expired GB1291562A (en) | 1968-10-22 | 1968-10-22 | Improvements in or relating to the construction of elongated fibre-reinforced synthetic plastics members, such as propeller blades |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE1954062A1 (en) |
| FR (1) | FR2040956A5 (en) |
| GB (1) | GB1291562A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5632602A (en) * | 1993-10-15 | 1997-05-27 | Deutsche Forschungsanstalt Fur Luft-Und Ramfarht E.V. | Rotor blade |
| FR2955083A1 (en) * | 2010-01-14 | 2011-07-15 | Snecma | Propeller blade, has member presenting longitudinal axis, where member includes part of oblong section and another part of cylindrical section presenting axis symmetry along longitudinal axis |
| GB2489546A (en) * | 2011-03-30 | 2012-10-03 | Gurit Uk Ltd | Water turbine blade with composite spar |
| US9945389B2 (en) | 2014-05-05 | 2018-04-17 | Horton, Inc. | Composite fan |
| US12060148B2 (en) | 2022-08-16 | 2024-08-13 | Honeywell International Inc. | Ground resonance detection and warning system and method |
| US20250137380A1 (en) * | 2022-01-21 | 2025-05-01 | Safran Aircraft Engines | Secondary flow guide vane of a turbomachine and turbomachine provided therewith |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3710321C1 (en) * | 1987-03-28 | 1988-06-01 | Mtu Muenchen Gmbh | Fan blade, especially for prop fan engines |
| DE3737894A1 (en) * | 1987-11-07 | 1989-05-18 | Ferdinand Dr Lutz | Propeller having adjustable blades (variable pitch propeller) |
-
1968
- 1968-10-22 GB GB5017168A patent/GB1291562A/en not_active Expired
-
1969
- 1969-10-22 FR FR6936177A patent/FR2040956A5/fr not_active Expired
- 1969-10-22 DE DE19691954062 patent/DE1954062A1/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5632602A (en) * | 1993-10-15 | 1997-05-27 | Deutsche Forschungsanstalt Fur Luft-Und Ramfarht E.V. | Rotor blade |
| FR2955083A1 (en) * | 2010-01-14 | 2011-07-15 | Snecma | Propeller blade, has member presenting longitudinal axis, where member includes part of oblong section and another part of cylindrical section presenting axis symmetry along longitudinal axis |
| GB2489546A (en) * | 2011-03-30 | 2012-10-03 | Gurit Uk Ltd | Water turbine blade with composite spar |
| GB2489546B (en) * | 2011-03-30 | 2015-09-23 | Gurit Uk Ltd | Water-turbine blade |
| US9945389B2 (en) | 2014-05-05 | 2018-04-17 | Horton, Inc. | Composite fan |
| US10415587B2 (en) | 2014-05-05 | 2019-09-17 | Horton, Inc. | Composite fan and method of manufacture |
| US10914314B2 (en) | 2014-05-05 | 2021-02-09 | Horton, Inc. | Modular fan assembly |
| US20250137380A1 (en) * | 2022-01-21 | 2025-05-01 | Safran Aircraft Engines | Secondary flow guide vane of a turbomachine and turbomachine provided therewith |
| US12372001B2 (en) * | 2022-01-21 | 2025-07-29 | Safran Aircraft Engines | Secondary flow guide vane of a turbomachine and turbomachine provided therewith |
| US12060148B2 (en) | 2022-08-16 | 2024-08-13 | Honeywell International Inc. | Ground resonance detection and warning system and method |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2040956A5 (en) | 1971-01-22 |
| DE1954062A1 (en) | 1970-04-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |