RU93032370A - POWER UNIT WITH AIR SCREW OR PROPELLER - Google Patents
POWER UNIT WITH AIR SCREW OR PROPELLERInfo
- Publication number
- RU93032370A RU93032370A RU93032370/11A RU93032370A RU93032370A RU 93032370 A RU93032370 A RU 93032370A RU 93032370/11 A RU93032370/11 A RU 93032370/11A RU 93032370 A RU93032370 A RU 93032370A RU 93032370 A RU93032370 A RU 93032370A
- Authority
- RU
- Russia
- Prior art keywords
- propeller
- power unit
- shell
- air screw
- gopriyatnoe
- Prior art date
Links
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000005755 formation reaction Methods 0.000 claims 1
Claims (1)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4039810.2 | 1990-12-13 | ||
DEP4039810.2 | 1990-12-13 | ||
DE4039810A DE4039810C1 (en) | 1990-12-13 | 1990-12-13 | |
PCT/EP1991/002040 WO1992010660A1 (en) | 1990-12-13 | 1991-10-29 | Thrust reverser for a propfan engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU93032370A true RU93032370A (en) | 1997-01-27 |
RU2094639C1 RU2094639C1 (en) | 1997-10-27 |
Family
ID=6420234
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU9193032370A RU2094639C1 (en) | 1990-12-13 | 1991-10-29 | Power plant with aircrew or propeller (versions) |
Country Status (7)
Country | Link |
---|---|
US (1) | US5343696A (en) |
EP (1) | EP0561791B1 (en) |
JP (1) | JPH06505781A (en) |
DE (2) | DE4039810C1 (en) |
ES (1) | ES2060407T3 (en) |
RU (1) | RU2094639C1 (en) |
WO (1) | WO1992010660A1 (en) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5516061A (en) * | 1994-09-19 | 1996-05-14 | Lockheed Corporation | Shroud for a reversible thrust fan |
FR2737256B1 (en) * | 1995-07-26 | 1997-10-17 | Aerospatiale | DUAL FLOW TURBOREACTOR WITH PUSH INVERSION GATES NOT SUBJECT TO THE SECONDARY FLOW IN THEIR INACTIVE POSITION |
US5730392A (en) * | 1995-09-22 | 1998-03-24 | Aeronautical Concept Of Exhaust, Ltd. | Adjustable fairing for thrust reversers |
FR2757901B1 (en) * | 1996-12-26 | 1999-01-29 | Hispano Suiza Sa | DOWNSTREAM DOUBLE FLOW TURBOREACTOR DRIVE INVERTER |
FR2766522B1 (en) * | 1997-07-24 | 1999-09-03 | Hispano Suiza Sa | TURBO BLOWER THRUST INVERTER WITH OBSTACLE WITH AXIAL GUIDANCE LINKED TO THE PRIMARY COVER |
DE10041619A1 (en) | 2000-05-22 | 2001-11-29 | Bayer Ag | Selective herbicides based on heteroaryloxyacetamides |
US6669875B2 (en) * | 2000-12-18 | 2003-12-30 | 3M Innovative Properties Company | Method for making a dental mill blank assembly |
US6938408B2 (en) * | 2001-04-26 | 2005-09-06 | Propulsion Vectoring, L.P. | Thrust vectoring and variable exhaust area for jet engine nozzle |
DE10146591A1 (en) | 2001-09-21 | 2003-04-10 | Bayer Cropscience Ag | Herbicides based on substituted thien-3-yl-sulfonylamino (thio) carbonyl-triazolin (thi) onen |
DE102004010813A1 (en) | 2004-03-05 | 2005-11-10 | Bayer Cropscience Ag | New herbicides based on substituted thien-3-yl-sulfonylamino (thio) carbonyltriazolin (thi) ones and 4-HPPD inhibitors |
US7665689B2 (en) * | 2006-11-24 | 2010-02-23 | The Boeing Company | Unconventional integrated propulsion systems and methods for blended wing body aircraft |
US7966828B2 (en) * | 2007-01-08 | 2011-06-28 | United Technologies Corporation | Variable area nozzle with woven sleeve extension |
US8959889B2 (en) | 2008-11-26 | 2015-02-24 | The Boeing Company | Method of varying a fan duct nozzle throat area of a gas turbine engine |
US8127532B2 (en) | 2008-11-26 | 2012-03-06 | The Boeing Company | Pivoting fan nozzle nacelle |
FR2958910B1 (en) * | 2010-04-20 | 2012-04-27 | Aircelle Sa | NACELLE FOR AIRCRAFT ENGINE WITH VARIABLE SECTION TUBE |
US8863491B2 (en) | 2012-01-31 | 2014-10-21 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US10400629B2 (en) | 2012-01-31 | 2019-09-03 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US8402741B1 (en) | 2012-01-31 | 2013-03-26 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US10113508B2 (en) | 2014-11-21 | 2018-10-30 | General Electric Company | Gas turbine engine and method of assembling the same |
US10465538B2 (en) * | 2014-11-21 | 2019-11-05 | General Electric Company | Gas turbine engine with reversible fan |
US10502160B2 (en) | 2016-02-09 | 2019-12-10 | General Electric Company | Reverse thrust engine |
JP6299792B2 (en) * | 2016-03-24 | 2018-03-28 | トヨタ自動車株式会社 | Air jet thrust generator for attitude control of moving objects |
FR3052191B1 (en) * | 2016-06-01 | 2019-07-12 | Safran Aircraft Engines | INVERSION OF PUSH IN A TURBOMACHINE WITH VARIABLE CALIBRATION BLOWER |
PL417832A1 (en) | 2016-07-04 | 2018-01-15 | General Electric Company | Socket expansion unit, preferably for a nozzle and method for disassembling it and the fan engine containing that unit |
US11053888B2 (en) * | 2017-11-01 | 2021-07-06 | The Boeing Company | Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode |
PL235797B1 (en) * | 2018-02-21 | 2020-10-19 | Gen Electric | Bell-shaped nozzle unit for gas-turbine engines |
FR3082186B1 (en) * | 2018-06-07 | 2021-02-12 | Safran | PROPULSION KIT FOR AN AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2570629A (en) * | 1945-10-05 | 1951-10-09 | Anxionnaz | Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles |
GB861819A (en) * | 1957-07-29 | 1961-03-01 | Boeing Co | Noise suppressor and thrust reverser for jet propulsion engines |
DE2446548A1 (en) * | 1973-10-11 | 1975-04-17 | United Aircraft Corp | POWER PLANT WITH COVERED FAN |
GB1565212A (en) * | 1975-12-22 | 1980-04-16 | British Hovercraft Corp Ltd | Ductecd fan propulsors |
GB2070691B (en) * | 1980-01-11 | 1983-08-24 | Rolls Royce | Radial splitter for reversible pitch fan propulsion unit |
US4802629A (en) * | 1982-10-22 | 1989-02-07 | The Boeing Company | Plug-type exhaust nozzle having a variable centerbody and translating shroud |
-
1990
- 1990-12-13 DE DE4039810A patent/DE4039810C1/de not_active Expired - Lifetime
-
1991
- 1991-10-29 US US08/075,510 patent/US5343696A/en not_active Expired - Fee Related
- 1991-10-29 EP EP91918014A patent/EP0561791B1/en not_active Expired - Lifetime
- 1991-10-29 RU RU9193032370A patent/RU2094639C1/en active
- 1991-10-29 DE DE59102584T patent/DE59102584D1/en not_active Expired - Fee Related
- 1991-10-29 ES ES91918014T patent/ES2060407T3/en not_active Expired - Lifetime
- 1991-10-29 WO PCT/EP1991/002040 patent/WO1992010660A1/en active IP Right Grant
- 1991-10-29 JP JP3517057A patent/JPH06505781A/en active Pending
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