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#31
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![]() "Casey Wilson" N2310D @ gmail.com wrote in message news:qokpf.21228$eI5.17594@trnddc05... "Keith W" wrote in message ... "Dan, U.S. Air Force, retired" wrote in message news:yDepf.66209$sg5.26836@dukeread12... Charles Talleyrand wrote: For one thing you'd be hard pressed to get 30 minutes of glide time from any airliner. Dan, U.S. Air Force, retired The Air Transat Airbus that ran out of fuel glided for 20 minutes to get to the Azores Keith And there is the 1983 (?86) story of the "Gimli Glider." An Air Canada B-767 that ran out of fuel and landed on an X-ed out runway in Canada that was, at the time, in use by sports car racers. See: http://www.silhouet.com/motorsport/tracks/gimli.html for a great photo. They talk about the RATS but I couldn't find any remarks about elapsed glide time in this story. For giggles, read the post script story about the mechanics who went to rescue the airplane. Here is a link to the RAT: http://www.hamiltonsundstrandcorp.co..._PRD38,00.html We make the hydraulic pump portion: http://www.parker.com//ead/cm2.asp?cmid=2841 |
#32
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Skywise wrote:
Damned good flying. I would have officially christend that plane the "Gimli Glider" and painted it's nose with it. I wonder if it's still in service today. That plane's got good karma. http://www.airliners.net/search/phot...eywords=C-GAUN Still in service |
#33
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Steve schrieb:
Its located just behind the left main wheel but stalls when the gear is lowered, so its a wheels up landing if you've got the balls. ![]() Well done ;-) Benjamin |
#34
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"James Hart" wrote in
: Skywise wrote: Damned good flying. I would have officially christend that plane the "Gimli Glider" and painted it's nose with it. I wonder if it's still in service today. That plane's got good karma. http://www.airliners.net/search/phot...es=500&keyword s=C-GAUN Still in service Thank you! Brian -- http://www.skywise711.com - Lasers, Seismology, Astronomy, Skepticism Seismic FAQ: http://www.skywise711.com/SeismicFAQ/SeismicFAQ.html Quake "predictions": http://www.skywise711.com/quakes/EQDB/index.html Sed quis custodiet ipsos Custodes? Like censorship and not getting support help? Switch to Supernews! They won't even answer questions through your ISP! |
#35
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![]() Benjamin Gawert wrote: Eunometic schrieb: The PA200 Tornado is fully FBW with a mechanical linkage backup system... Benjamin Then why does it need a thermal backup battery to remain airborn? Because besides power for certain important instruments and the radio the EPS battery also powers an electric motor that powers a hydraulic pump. "Mechanical linkage" does not mean that the stick is connected to pushrods and levers that move the control surfaces (which would be silly on a fighter/bomber aircraft with up to ~55000 pounds weight). Which means that PA200 Tornado when using 'mechanical' backup is actually fully power opperated as opposed to power assisted (power assisted can be designed to connect into a fully manual system with limited movement). Given the need for power it doesn't seem to make much sense to bother to use a mechanical system at all. An additional layer of redundancy and an 'analog' backup would be better use of the weight. Perhaps Panavia was worried about Electromagnetic Pulse or Weapons. I believe F-16 uses fiber optics. When in so-called "mech mode" the stick is connected to several hydraulic valves that control the hydraulic actuators. So you need hydraulics pressure, and in cases of double engine out this hydraulic pressure comes from an electric pump that powered by the EPS battery. In normal operation the potentiometers connected to the stick submit stick position data to the flight control system (CSAS and SPILS) which calculate the necessary control surface deflection and control the corresponding actuators. They use potentiometers? I though LVDT were normally used. The mechanical linkage is inactive (in emergencies the stick gets linked to the mechanical controls through a honeycomb block which gets squeezed by the stick movement applied by the panicing pilot ;-) This applies to the GR versions (bomber), I don't know if the F versions are somewhat different. Benjamin |
#36
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A higher flying Airbus or B747-400 at 44,000ft might have glided nearly
30 minutes. This suggests that a fighter plane with its lower glide ratio probably only needs half the amount of time (10 minutes) which suggests that a thermal battery is possibly more efficient or at least adaquet whereas an airliner may need twice as much. What seems extraordinary is that both airbus and boeing designers have provided insufficient RAT power to opperate all systems: spoilers, flaps, undercarriage seem to be neglected. This makes an emegency landing much harder. In both the airbus A330-200 azores and boeing 767 gimli fuel out landing case the lack of spoilers added a great deal of risk as pilots manouvered agressively to loose altitude and speed for runway lineup. |
#37
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![]() "Eunometic" wrote in message ups.com... A higher flying Airbus or B747-400 at 44,000ft might have glided nearly 30 minutes. This suggests that a fighter plane with its lower glide ratio probably only needs half the amount of time (10 minutes) which suggests that a thermal battery is possibly more efficient or at least adaquet whereas an airliner may need twice as much. What seems extraordinary is that both airbus and boeing designers have provided insufficient RAT power to opperate all systems: spoilers, flaps, undercarriage seem to be neglected. This makes an emegency landing much harder. In both the airbus A330-200 azores and boeing 767 gimli fuel out landing case the lack of spoilers added a great deal of risk as pilots manouvered agressively to loose altitude and speed for runway lineup. If you add more power to the RAT you increase drag and reduce the glide distance, the record suggests they made the right trade offs. Keith |
#38
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![]() "Eunometic" wrote in message oups.com... Benjamin Gawert wrote: Eunometic schrieb: Eunometic schrieb: It does apply for the PA200 Tornado. The APU is not operable in-flight, if you loose both engines and the one-shot battery is down you have to get out of that thing... I didn't think Tornado was fully FBW? The PA200 Tornado is fully FBW with a mechanical linkage backup system... Benjamin Then why does it need a thermal backup battery to remain airborn? The One Shot Battery is there to provide electrical power to a Fuel pump (or in combination with a Hyd pump). The engines also need electrical power to keep their systems running - without electrics, the engines will "run away" - Very bad thing if you're not near a nice big bit of tarmac...... |
#39
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Eunometic schrieb:
"Mechanical linkage" does not mean that the stick is connected to pushrods and levers that move the control surfaces (which would be silly on a fighter/bomber aircraft with up to ~55000 pounds weight). Which means that PA200 Tornado when using 'mechanical' backup is actually fully power opperated as opposed to power assisted (power assisted can be designed to connect into a fully manual system with limited movement). correct. Given the need for power it doesn't seem to make much sense to bother to use a mechanical system at all. The mechanical linkage backup is there if the 2x redundant fly-by-wire system fails or gets damaged. When in "mech mode" (FBW dead but engines are running) the aircraft is fully controllable (but of course reacts more sensible due to the lack of CSAS and also lacks things like spin prevention and AOA limiter etc). Loosing the FBW does not mean the aircraft can't return safely... An additional layer of redundancy and an 'analog' backup would be better use of the weight. Perhaps Panavia was worried about Electromagnetic Pulse or Weapons. Correct. Thanks to the mechanical linkage the aircraft is still operable even when suffering from an EMP or with a damaged electronics system. Even 4x redundant FBW wouldn't provide this safety, and the weight penalty isn't really big. I believe F-16 uses fiber optics. The Eurofighter Typhoon uses fiber optics. The F-16 used a wire harness (don't know if that has been changed in a later block but I doubt that). In normal operation the potentiometers connected to the stick submit stick position data to the flight control system (CSAS and SPILS) which calculate the necessary control surface deflection and control the corresponding actuators. They use potentiometers? I though LVDT were normally used. No, it's some sort of potentiometer, but of course a bit more sophisticated than what you can find in consumer electronics ;-) Benjamin |
#40
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On Mon, 19 Dec 2005 19:59:21 +0100, Benjamin Gawert
wrote: Eunometic schrieb: "Mechanical linkage" does not mean that the stick is connected to pushrods and levers that move the control surfaces (which would be silly on a fighter/bomber aircraft with up to ~55000 pounds weight). Which means that PA200 Tornado when using 'mechanical' backup is actually fully power opperated as opposed to power assisted (power assisted can be designed to connect into a fully manual system with limited movement). correct. Given the need for power it doesn't seem to make much sense to bother to use a mechanical system at all. The mechanical linkage backup is there if the 2x redundant fly-by-wire system fails or gets damaged. When in "mech mode" (FBW dead but engines are running) the aircraft is fully controllable (but of course reacts more sensible due to the lack of CSAS and also lacks things like spin prevention and AOA limiter etc). Loosing the FBW does not mean the aircraft can't return safely... Hmm sounds sensible in a Cold War environment with buckets of canned sunshine being thrown around. But now a question to pilots or folks in the know: Do they train flying "mech mode" and if so how? Just in the sims or sometimes for real as in. "IP to student: I flipped the switch to mech mode. Show me how you smooth you can land this baby"? And if a pilot can apparently fly safe in "mech mode" does that mean that the Tornado is not inherent unstable like the F16? Or at least not very inherent unstable? Because flying a F16 in "mech mode" (if that beast would exist) THAT would be a real challange. Greetz Mu Greetz Mu |
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