GB910056A - Engine blast absorbing fence - Google Patents
Engine blast absorbing fenceInfo
- Publication number
- GB910056A GB910056A GB3992160A GB3992160A GB910056A GB 910056 A GB910056 A GB 910056A GB 3992160 A GB3992160 A GB 3992160A GB 3992160 A GB3992160 A GB 3992160A GB 910056 A GB910056 A GB 910056A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fence
- perforations
- unit
- blast
- baffle screen
- 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
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/26—Ground or aircraft-carrier-deck installations for reducing engine or jet noise; Protecting airports from jet erosion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
Abstract
910,056. Blast deflector fences. STANRAY CORPORATION. Nov. 21, 1960, No. 39921/60. Class 51 (2). A blast deflector and silencing fence for jet engines comprises inclined, perforated, prefabricated units arranged back-to-back so that part of the blast is diverted upwardly and part passes through the perforations, the units being made of single sheets 16 of metal having flanges 18 on two opposite sides and another base flange 28 by which the fence may be weighted or anchored to the ground. Each unit is formed with perforations 30<SP>1</SP> and may be bent along lines 24 and 26 as shown in Fig. 2 or may be of arcuate form, Fig. 4 (not shown). In a modification, Fig. 11, a single fence is supported by struts 51 and 52 secured to angle iron shoes 56. A baffle screen 57 is fixed at an angle to the fence on arms 58 passing through slots 60 and attached at 59 to the strut 51. The perforations here are limited to a few near the base of each unit. The baffle screen may be applied to a back-to-back unit, Fig. 13 (not shown), or may be omitted, Fig. 9 (not shown). The aggregate area of the perforations may reach up to 60% of the area of each unit.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3992160A GB910056A (en) | 1960-11-21 | 1960-11-21 | Engine blast absorbing fence |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3992160A GB910056A (en) | 1960-11-21 | 1960-11-21 | Engine blast absorbing fence |
Publications (1)
Publication Number | Publication Date |
---|---|
GB910056A true GB910056A (en) | 1962-11-07 |
Family
ID=10412211
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3992160A Expired GB910056A (en) | 1960-11-21 | 1960-11-21 | Engine blast absorbing fence |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB910056A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2276543A (en) * | 1993-03-31 | 1994-10-05 | Mech Tool Engineering Ltd | Radiant heat shield |
US5591904A (en) * | 1993-10-21 | 1997-01-07 | Rheinhold & Mahla Ag | Apparatus for diminishing intake vortexes in jet engines |
GB2450386A (en) * | 2007-06-20 | 2008-12-24 | Keith Edward Foster | Thrust reactive surface for positioning behind aircraft |
GB2485583A (en) * | 2010-11-19 | 2012-05-23 | Ind Acoustics Company Ltd | Aircraft ground run-up enclosure |
-
1960
- 1960-11-21 GB GB3992160A patent/GB910056A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2276543A (en) * | 1993-03-31 | 1994-10-05 | Mech Tool Engineering Ltd | Radiant heat shield |
GB2276543B (en) * | 1993-03-31 | 1996-11-27 | Mech Tool Engineering Ltd | Radiant heat shield |
US5591904A (en) * | 1993-10-21 | 1997-01-07 | Rheinhold & Mahla Ag | Apparatus for diminishing intake vortexes in jet engines |
GB2450386A (en) * | 2007-06-20 | 2008-12-24 | Keith Edward Foster | Thrust reactive surface for positioning behind aircraft |
GB2450386B (en) * | 2007-06-20 | 2010-07-14 | Keith Edward Foster | Thrust reactive device for placing behind an aircraft |
GB2485583A (en) * | 2010-11-19 | 2012-05-23 | Ind Acoustics Company Ltd | Aircraft ground run-up enclosure |
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