GB1258148A - - Google Patents
Info
- Publication number
- GB1258148A GB1258148A GB1258148DA GB1258148A GB 1258148 A GB1258148 A GB 1258148A GB 1258148D A GB1258148D A GB 1258148DA GB 1258148 A GB1258148 A GB 1258148A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rod
- assemblies
- jet
- stowed
- axial movement
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
-
- 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
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
1,258,148. Deflecting propulsion jets. GENERAL ELECTRIC CO. 25 Nov., 1969 [2 Dec., 1968], No. 57548/69. Heading B7G. [Also in Division F1] Jet-deflecting apparatus for a jet engine 10 (Fig. 1, not shown) whose exhaust outlet is defined by an outer casing 18, Fig. 2, and a central body 28 consisting of fixed upstream and axially movable downstream portions 30, 32 comprises means 52, Fig. 4, for moving the downstream portion 32 between a retracted and an extended position, and cascade assemblies 26 of jet directing vanes 34 hinged at 36 to portion 32 for axial movement therewith and for rotational movement between stowed and deployed positions effected by actuating means 62, 64, 68, and receiving means 38 for enclosing said assemblies when stowed. Moving means 52 comprises telescopically adjustable tubular actuator rods 62, 64 moved by actuator means 66, rod 62 being secured to portion 32. and rod 64 to each assembly 26 by linkage means 68 so that axial movement of rod 64 relative to rod 62 effects corresponding rotation of assemblies 26 about hinge 36. A torque guide may be provided on rod 64 to prevent rotation therearound of portion 32 and the cascades 26.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US78032768A | 1968-12-02 | 1968-12-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1258148A true GB1258148A (en) | 1971-12-22 |
Family
ID=25119281
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1258148D Expired GB1258148A (en) | 1968-12-02 | 1969-11-25 |
Country Status (9)
| Country | Link |
|---|---|
| BE (1) | BE740622A (en) |
| CH (1) | CH524764A (en) |
| DE (1) | DE1959543A1 (en) |
| DK (1) | DK124700B (en) |
| FR (1) | FR2025052A1 (en) |
| GB (1) | GB1258148A (en) |
| NL (1) | NL6918101A (en) |
| NO (1) | NO125949B (en) |
| SE (1) | SE358603B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2180004A (en) * | 1985-09-03 | 1987-03-18 | Joy Mfg Co | Pneumatic actuator for a mechanical device |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3066788B1 (en) * | 2017-05-23 | 2019-07-12 | Airbus Operations | AIRCRAFT ENGINE COMPRISING AT LEAST ONE ACTUATOR OF A PUSH REVERSING SYSTEM AGENT IN A GAS EJECTION CONE |
-
1969
- 1969-10-22 BE BE740622D patent/BE740622A/xx unknown
- 1969-11-13 NO NO4500/69A patent/NO125949B/no unknown
- 1969-11-21 CH CH1740369A patent/CH524764A/en not_active IP Right Cessation
- 1969-11-25 GB GB1258148D patent/GB1258148A/en not_active Expired
- 1969-11-27 DE DE19691959543 patent/DE1959543A1/en active Pending
- 1969-12-01 DK DK635169AA patent/DK124700B/en unknown
- 1969-12-01 SE SE16499/69A patent/SE358603B/xx unknown
- 1969-12-02 FR FR6941583A patent/FR2025052A1/fr not_active Withdrawn
- 1969-12-02 NL NL6918101A patent/NL6918101A/xx unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2180004A (en) * | 1985-09-03 | 1987-03-18 | Joy Mfg Co | Pneumatic actuator for a mechanical device |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2025052A1 (en) | 1970-09-04 |
| CH524764A (en) | 1972-06-30 |
| DK124700B (en) | 1972-11-13 |
| BE740622A (en) | 1970-04-01 |
| NL6918101A (en) | 1970-06-04 |
| DE1959543A1 (en) | 1970-06-11 |
| SE358603B (en) | 1973-08-06 |
| NO125949B (en) | 1972-11-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4716724A (en) | Gas turbine engine powerplant with flow control devices | |
| GB1304212A (en) | ||
| US6474059B2 (en) | Thrust reverser | |
| US5228641A (en) | Cascade type aircraft engine thrust reverser with hidden link actuator | |
| US3279182A (en) | Thrust reverser | |
| GB1534583A (en) | Reversal of thrust in gas turbine engines | |
| CA2126313A1 (en) | Thrust reverser integrating a variable exhaust area nozzle | |
| GB1078421A (en) | Nozzle having a silencer effect for jet propulsion engines | |
| ATE67824T1 (en) | ADJUSTABLE FLAP OF A THRUST REVERSER FOR JET ENGINE. | |
| GB871265A (en) | Improvements relating to variable-area jet nozzles of turbojet engines | |
| US3016700A (en) | Thrust reverser for jet engines | |
| US3262269A (en) | Thrust reverser | |
| GB1009776A (en) | Supersonic jet propulsion nozzle | |
| GB1421153A (en) | Propulsion nozzle for ducted fan gas turbine jet propulsion engines | |
| ES269713A1 (en) | Openable fin arrangement | |
| US3665709A (en) | Thrust reversing apparatus | |
| GB1211923A (en) | Thrust reverser for gas turbine jet propulsion engine | |
| GB907220A (en) | Improvements in thrust spoiler and reingestion control | |
| GB1247691A (en) | Improvements in or relating to fan ducts for gas turbine ducted fan engines | |
| FR2379705A1 (en) | Thrust reversing mechanism for aircraft engine - has blades linked to sliding and moving parts of outer housing only | |
| US4216926A (en) | Linkage system for a turbo fan engine thrust reverser | |
| US4047682A (en) | Fan cowl translation lock | |
| US3600894A (en) | Thrust reversing apparatus | |
| GB1258148A (en) | ||
| US3386247A (en) | Powerplant with thrust reverser |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |