GB2170868B - Prop-fan with improved stability - Google Patents
Prop-fan with improved stabilityInfo
- Publication number
- GB2170868B GB2170868B GB08524280A GB8524280A GB2170868B GB 2170868 B GB2170868 B GB 2170868B GB 08524280 A GB08524280 A GB 08524280A GB 8524280 A GB8524280 A GB 8524280A GB 2170868 B GB2170868 B GB 2170868B
- Authority
- GB
- United Kingdom
- Prior art keywords
- prop
- fan
- improved stability
- stability
- improved
- 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
- B64C11/18—Aerodynamic features
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Percussion Or Vibration Massage (AREA)
- Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US69911985A | 1985-02-07 | 1985-02-07 |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8524280D0 GB8524280D0 (en) | 1985-11-06 |
GB2170868A GB2170868A (en) | 1986-08-13 |
GB2170868B true GB2170868B (en) | 1988-07-13 |
Family
ID=24808020
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08524280A Expired GB2170868B (en) | 1985-02-07 | 1985-10-02 | Prop-fan with improved stability |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS61181798A (en) |
BR (1) | BR8504907A (en) |
CA (1) | CA1270802A (en) |
DE (1) | DE3535399A1 (en) |
FR (1) | FR2576872B1 (en) |
GB (1) | GB2170868B (en) |
IT (1) | IT1185996B (en) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2605588B1 (en) * | 1986-10-24 | 1989-04-28 | Onera (Off Nat Aerospatiale) | IMPROVEMENTS ON AIR PROPELLERS, ESPECIALLY FOR AIRCRAFT PROPELLERS |
DE3738785A1 (en) * | 1986-11-19 | 1988-05-26 | Gen Electric | CONTRA-ROTATING AIRPLANE DRIVE BLADES |
USRE34207E (en) * | 1986-11-19 | 1993-03-30 | General Electric Company | Counterrotating aircraft propulsor blades |
US5165856A (en) * | 1988-06-02 | 1992-11-24 | General Electric Company | Fan blade mount |
US5102302A (en) * | 1988-06-02 | 1992-04-07 | General Electric Company | Fan blade mount |
GB2220712B (en) * | 1988-07-13 | 1992-12-09 | Rolls Royce Plc | Open rotor blading |
US4971641A (en) * | 1988-11-14 | 1990-11-20 | General Electric Company | Method of making counterrotating aircraft propeller blades |
US6071077A (en) * | 1996-04-09 | 2000-06-06 | Rolls-Royce Plc | Swept fan blade |
GB2469516A (en) * | 2009-04-17 | 2010-10-20 | Insensys Ltd | Rotor blade with optical strain sensors covered by erosion shield |
US20130340406A1 (en) | 2012-01-31 | 2013-12-26 | Edward J. Gallagher | Fan stagger angle for geared gas turbine engine |
US10465702B2 (en) | 2014-02-19 | 2019-11-05 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015126715A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108110B1 (en) | 2014-02-19 | 2020-04-22 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015175058A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108109B1 (en) | 2014-02-19 | 2023-09-13 | Raytheon Technologies Corporation | Gas turbine engine fan blade |
US9567858B2 (en) | 2014-02-19 | 2017-02-14 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108101B1 (en) * | 2014-02-19 | 2022-04-20 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
US10519971B2 (en) | 2014-02-19 | 2019-12-31 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015175052A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
EP3114321B1 (en) | 2014-02-19 | 2019-04-17 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108106B1 (en) | 2014-02-19 | 2022-05-04 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
WO2015126824A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108116B1 (en) | 2014-02-19 | 2024-01-17 | RTX Corporation | Gas turbine engine |
WO2015126450A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108115B8 (en) | 2014-02-19 | 2023-11-08 | RTX Corporation | Turbofan engine with geared architecture and lpc blades |
WO2015175073A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
US10502229B2 (en) | 2014-02-19 | 2019-12-10 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108113A4 (en) | 2014-02-19 | 2017-03-15 | United Technologies Corporation | Gas turbine engine airfoil |
US10393139B2 (en) | 2014-02-19 | 2019-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
US10590775B2 (en) | 2014-02-19 | 2020-03-17 | United Technologies Corporation | Gas turbine engine airfoil |
US10605259B2 (en) | 2014-02-19 | 2020-03-31 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015126454A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
FR3045564B1 (en) | 2015-12-21 | 2018-08-17 | Airbus Helicopters | AIRCRAFT ROTOR BLADE WITH GEOMETRY ADAPTED FOR ACOUSTIC IMPROVEMENT DURING APPROACH FLIGHTS AND PERFORMANCE IMPROVEMENT IN STATIONARY AND ADVANCED FLIGHTS |
FR3045565B1 (en) | 2015-12-21 | 2018-07-27 | Airbus Helicopters | AIRCRAFT ROTOR BLADE WITH GEOMETRY ADAPTED FOR ACOUSTIC IMPROVEMENT DURING AN APPROACH FLIGHT AND PERFORMANCE IMPROVEMENT IN FLYING |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3989406A (en) * | 1974-11-26 | 1976-11-02 | Bolt Beranek And Newman, Inc. | Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like |
US4171183A (en) * | 1976-09-24 | 1979-10-16 | United Technologies Corporation | Multi-bladed, high speed prop-fan |
US4358246A (en) * | 1979-07-16 | 1982-11-09 | United Technologies Corporation | Noise reduction means for prop-fan and the construction thereof |
-
1985
- 1985-08-16 CA CA000488883A patent/CA1270802A/en not_active Expired - Fee Related
- 1985-10-02 GB GB08524280A patent/GB2170868B/en not_active Expired
- 1985-10-03 DE DE19853535399 patent/DE3535399A1/en not_active Withdrawn
- 1985-10-04 BR BR8504907A patent/BR8504907A/en not_active IP Right Cessation
- 1985-10-07 FR FR8514818A patent/FR2576872B1/en not_active Expired
- 1985-10-07 IT IT22377/85A patent/IT1185996B/en active
- 1985-10-07 JP JP60223447A patent/JPS61181798A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
FR2576872B1 (en) | 1987-07-24 |
FR2576872A1 (en) | 1986-08-08 |
GB8524280D0 (en) | 1985-11-06 |
CA1270802A (en) | 1990-06-26 |
IT8522377A0 (en) | 1985-10-07 |
IT1185996B (en) | 1987-11-18 |
GB2170868A (en) | 1986-08-13 |
DE3535399A1 (en) | 1986-08-07 |
BR8504907A (en) | 1986-12-16 |
JPS61181798A (en) | 1986-08-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19941002 |