Pratt & Whitney Aircraft
Auteur de The Aircraft Gas Turbine Engine and Its Operation
A propos de l'auteur
Œuvres de Pratt & Whitney Aircraft
Aeronautical Vest-Pocket Handbook Presented with the Compliments of Pratt and Whitney Aircraft - 1952 2 exemplaires
Aeronautical Vest-Pocket Handbook 2 exemplaires
Accuracy for Seventy Years 1860-1930 2 exemplaires
Pratt & Whitney Jet Engine Handbook 1 exemplaire
On Wire Splicing 1 exemplaire
Pratt & Whitney engine decal (one: Right) 1 exemplaire
Prat & Whitney Gages No. 10 1 exemplaire
P & W F135 Engines of Choice For F-35 Lightning II 1 exemplaire
Operators Handbook - Double Wasp B Series Engines (with Two-Stage Supercharger R-2800 -8 and -10 1 exemplaire
The Aircraft Gas Turbine Engine and Its Operation (Reprinted with Revisions August 1988) (1988) 1 exemplaire
The Rocket Engine and Its Operation - September 1997 1 exemplaire
Space Shuttle Main Engine Orientation 1 exemplaire
Pratt and Whitney Engine Handbook Hornet Series A-1 1 exemplaire
Wasp Junior Parts Catalog R-985 Series 1 exemplaire
Pratt and Whitney Engine Data 1 exemplaire
Small tools : (catalog no. 5) 1 exemplaire
The Last CF-100 to Fly - LE DERNIER CF-100 A VOLER 1 exemplaire
Mais qui chante dans le boisé ? (P01_PWC_BK_024) 1 exemplaire
Clouds of Airplanes 1 exemplaire
Pratt & Whitney Aircraft Overhaul Manual, Wasp Jr. R-985 & Wasp R-1340, Part No. 123440, Feb. 1954, Rev. March 1975 1 exemplaire
DOUBLE WASP (R-2800) CB ENGINES - MAINTENANCE MANUAL 1 exemplaire
TWIN WASP - R-1830 S1C3G MAINTENANCE MANUAL 1 exemplaire
Maintenance Manual Wasp Jr. (R-985) B4 and B5 and Wasp (R-1340) S1H1, S1H2, S3H1, and S3H2 AND S3H1-G Engines (1947) 1 exemplaire
Pratt & Whitney R-2800 A B Aircraft Engine Operators Manual - SERVICE INSTRUCTIONS R-2800-5, -6, -21, -31, -39, -41,… (1942) 1 exemplaire
Operators Handbook - Restricted - (Part No. 72663) Double Wasp B Series Engines (With Two Stage Supercharger) (1942) 1 exemplaire
Overhaul Manual (Part No. 48616) Wasp Jr. B, Wasp H1 and Hornet E Series Engines (1942) 1 exemplaire
General operating instructions. Axial compressor nonafterburning turbojet and turbofan engines 1 exemplaire
General Operating 1 exemplaire
Pratt & Whitney Aircraft Illustrated Parts Catalog (Wasp R-1340 engine) Part No. 86013 Reissue April 1962, Rev. May… 1 exemplaire
Army and Navy Airplabe Model Designations 1 exemplaire
The aircraft engine and its operation 1 exemplaire
Pratt & Whitney Twin Wasp C Series (R-1830 & R-2000) Engines Overhaul Manual (4th edition Rev. July 1942) 1 exemplaire
Pratt & Whitney Double Wasp (R-2800-27, 31, 43, 51, 59, 71, 75, 79 ) Engine Parts Catalog (May 1952) 1 exemplaire
Pratt & Whitney Engine Spare Parts Catalog (9 cylinder R-1830 S3C4G) [blue paper loose-leaf binder] 1942 1 exemplaire
Pratt & Whitney Aircraft Overhaul Manual - Wasp Jr. B, Wasp H1 & Hornet E Series Engines (R-985) Nov. 1942 1 exemplaire
Pratt & Whitney Double Wasp (R-2800-8 & 10) Engines (with two0stage supercharger) Operator's Handbook (Nov. 1943) 1 exemplaire
introduction to Jet Engine Fundamentals 1 exemplaire
Operators Handbook - Double Wasp B Series Engines (With Two-Stage Supercharger), Second edition, NAVAER 02-10GR-1 1 exemplaire
The aircraft gas turbine. An inside story 1 exemplaire
Étiqueté
Partage des connaissances
- Autres noms
- Pratt & Whitney
Pratt & Whitney Aircraft Group
Pratt & Whitney Aircraft Division - Date de naissance
- 1925
- Sexe
- n/a
- Nationalité
- USA
Membres
Critiques
Statistiques
- Œuvres
- 63
- Membres
- 103
- Popularité
- #185,855
- Évaluation
- 5.0
- Critiques
- 3
- ISBN
- 1
The JT8D is an axial-flow front turbofan engine incorporating a two-spool design. There are two coaxially-mounted independent rotating assemblies: one rotating assembly for the low pressure compressor (LPC) which consists of the first six stages (i.e. six pairs of rotating and stator blades, including the first two stages which are for the bypass turbofan), driven by the second (downstream) turbine (which consists of three stages); and a second rotating assembly for the high-pressure compressor (HPC) section, which has seven stages. The high-pressure compressor is driven by the first (upstream) turbine, which has a single stage. https://en.wikipedia.org/wiki/Pratt_%26_Whitney_JT8D… (plus d'informations)