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Just to expand a little bit more... all of the major manufacturers have changed their philosophy to a greater or lesser extent around cockpit design over time. I fly an LS8, which is largely based on the later model LS6. If you look at the cockpit of an early LS6, vs the later LS6 and the LS8, you can see significant changes in the construction of the cockpit area and the seat pan in particular. The same applies to Schemp-Hirth (e.g. later Ventus2 vs. original Ventus). So, other things being equal, a later generation of a given class of glider from a given manufacturer probably affords better crash protection than the prior generation (e.g. ASW-24 vs. ASW-19; LS8 vs. LS4; Ventus 2 vs. Ventus). How the various manufacturers stack up when comparing gliders of the same generation (e.g. LS8 vs. ASW28 vs. Discus2) is probably a little harder to quantify without extensive testing. I know some has been done (see the OSTIV link in this thread), and I'm sure the "conventional wisdom" gives the nod to Schleicher. It would be nice to see some more hard data.
P3 On Thursday, October 24, 2013 8:03:47 AM UTC-4, Dave Nadler wrote: On Thursday, October 24, 2013 7:45:03 AM UTC-4, joesimmers wrote: I think [Schleichers] are the only one with the crash cockpit design. Wrong. Many modern gliders have reinforced cockpits and many have energy-absorbing gear. Lange also adds a crush zone in nose: http://www.lange-aviation.com/htm/en...0e/safety.html RAS - Rampant Aviation Speculation.... |
#2
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In article ,
Papa3 wrote: Just to expand a little bit more... all of the major manufacturers have changed their philosophy to a greater or lesser extent around cockpit design over time. I fly an LS8, which is largely based on the later model LS6. If you look at the cockpit of an early LS6, vs the later LS6 and the LS8, you can see significant changes in the construction of the cockpit area and the seat pan in particular. The same applies to Schemp-Hirth (e.g. later Ventus2 vs. original Ventus). So, other things being equal, a later generation of a given class of glider from a given manufacturer probably affords better crash protection than the prior generation (e.g. ASW-24 vs. ASW-19; LS8 vs. LS4; Ventus 2 vs. Ventus). How the various manufacturers stack up when comparing gliders of the same generation (e.g. LS8 vs. ASW28 vs. Discus2) is probably a little harder to quantify without extensive testing. I know some has been done (see the OSTIV link in this thread), and I'm sure the "conventional wisdom" gives the nod to Schleicher. It would be nice to see some more hard data. P3 I fly an early H-301 Libelle (serial #19). It has a significant safety feature not seen in many other gliders. The fuselage is so thin that it allows one see out if the canopy fogs over. Seriously, Libelles would, in no way, be construed as having a "safety cockpit", however, there have been relatively few fatalities in Libelles. I think their slightly wobbly, unstable feel encourages pilots to pay attention to their flying. --- news://freenews.netfront.net/ - complaints: --- |
#3
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On Thursday, October 24, 2013 11:17:44 AM UTC-4, WB wrote:
I fly an early H-301 Libelle (serial #19). It has a significant safety feature not seen in many other gliders. The fuselage is so thin that it allows one see out if the canopy fogs over. Seriously, Libelles would, in no way, be construed as having a "safety cockpit", however, there have been relatively few fatalities in Libelles. I think their slightly wobbly, unstable feel encourages pilots to pay attention to their flying. An extra helping of humor, on toasted wry. I'm going to chuckle about that all afternoon. T8 |
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The Scheibe trainers are enormously strong.
The Bergfalkes have a long travel sprung skid to absorb energy in a hard landing. Seen them being stress tested more than once and they have much more give before damage than a modern glass design. Conversely and unfortunately the seat design is so poor that - should you reach the end of travel on the skid there is a virtual guarantee of spinal injury. I have seen enough fatal or serious injury wrecks to have no illusions about how much protection that cockpit will provide. It is a little like the adage , that if you want people to drive carefully one should replace the airbag with a sharpened spike... The best modern cockpits are a lot better than their predecessors, but it is little comfort. Bruce On 2013/10/24 5:29 PM, Evan Ludeman wrote: On Thursday, October 24, 2013 11:17:44 AM UTC-4, WB wrote: I fly an early H-301 Libelle (serial #19). It has a significant safety feature not seen in many other gliders. The fuselage is so thin that it allows one see out if the canopy fogs over. Seriously, Libelles would, in no way, be construed as having a "safety cockpit", however, there have been relatively few fatalities in Libelles. I think their slightly wobbly, unstable feel encourages pilots to pay attention to their flying. An extra helping of humor, on toasted wry. I'm going to chuckle about that all afternoon. T8 -- Bruce Greeff T59D #1771 |
#5
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On Thursday, October 24, 2013 10:13:10 AM UTC-4, Papa3 wrote:
I'm sure the "conventional wisdom" gives the nod to Schleicher. Say what ? The modern Schleicher cockpits are huge improvements over earlier designs, however: - no crush zone in front of your feet to absorb energy and decelerate the glider before your feet do - a giant hole is cut in the side beam for air ventilation output, reducing the buckling strength needed here Again, please look at: http://www.lange-aviation.com/htm/en...0e/safety.html Hope that helps, Best Regards, Dave "YO electric" PS: Some of you will remember I donated a fuselage for crash testing some decades back, hoping to help improve cockpit safety... |
#6
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On Thursday, October 24, 2013 5:52:38 PM UTC-4, Dave Nadler wrote:
On Thursday, October 24, 2013 10:13:10 AM UTC-4, Papa3 wrote: I'm sure the "conventional wisdom" gives the nod to Schleicher. Say what ? The modern Schleicher cockpits are huge improvements over earlier designs, however: - no crush zone in front of your feet to absorb energy and decelerate the glider before your feet do - a giant hole is cut in the side beam for air ventilation output, reducing the buckling strength needed here Again, please look at: http://www.lange-aviation.com/htm/en...0e/safety.html Hope that helps, Best Regards, Dave "YO electric" PS: Some of you will remember I donated a fuselage for crash testing some decades back, hoping to help improve cockpit safety... A review of the lamination schemes for '24, 27, 28 reflects a designed in forward crush area in the nose with progressively stiffer structure once in the pilot protection zone. I have observed closely both a '24 and a'27 that had significant nose damage and niether had any failure in the area where the air vent is located. Waibel pioneered that aspect that others have wisely emulated. UH |
#7
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Dave Nadler wrote, On 10/24/2013 2:52 PM:
On Thursday, October 24, 2013 10:13:10 AM UTC-4, Papa3 wrote: I'm sure the "conventional wisdom" gives the nod to Schleicher. Say what ? The modern Schleicher cockpits are huge improvements over earlier designs, however: - no crush zone in front of your feet to absorb energy and decelerate the glider before your feet do - a giant hole is cut in the side beam for air ventilation output, reducing the buckling strength needed here The air vent is not in structural ducting. All the buckling strength needed is in the cockpit rails, which are clearly seen when the canopy is open. They are straight to improve buckling resistance, and very strong. Take a look at ASW-24, 26, and all later ones. I don't know about the ASH-25, as I haven't looked at one closely enough. -- Eric Greenwell - Washington State, USA (change ".netto" to ".us" to email me) |
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