JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation

The U.S. Army Aviation Engineering Flight Activity conducted an evaluation of the Pneumatic Boot Deicing System (PBDS) with two pneumatic deicer boot designs, referred to as second and third generation. The objective of the test was to conduct feasibility testing of the pneumatic system concept for...

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Bibliographic Details
Main Authors: Graham, Matthew S, Haworth, Loran A, Kimberly, Jack L
Other Authors: ARMY AVIATION ENGINEERING FLIGHT ACTIVITY EDWARDS AFB CA
Format: Text
Language:English
Published: 1987
Subjects:
Ice
Online Access:http://www.dtic.mil/docs/citations/ADA194918
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA194918
id ftdtic:ADA194918
record_format openpolar
spelling ftdtic:ADA194918 2023-05-15T16:37:39+02:00 JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation Graham, Matthew S Haworth, Loran A Kimberly, Jack L ARMY AVIATION ENGINEERING FLIGHT ACTIVITY EDWARDS AFB CA 1987-08 text/html http://www.dtic.mil/docs/citations/ADA194918 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA194918 en eng http://www.dtic.mil/docs/citations/ADA194918 Approved for public release; distribution is unlimited. DTIC AND NTIS Helicopters Snow Ice and Permafrost *DEICING SYSTEMS *ROTOR BLADES(ROTARY WINGS) AIRCRAFT BOOTS ENVELOPE(SPACE) FEASIBILITY STUDIES FLIGHT TESTING HANDLING HELICOPTER ROTORS HOVERING ICE FORMATION INFLIGHT LEVEL FLIGHT LOADS(FORCES) PENALTIES PERFORMANCE(ENGINEERING) PNEUMATIC EQUIPMENT QUALITY RELIABILITY STRUCTURAL PROPERTIES SURVEYS TEST AND EVALUATION PBDS(PNEUMATIC BOOT DEICING SYSTEM) JUH-1H AIRCRAFT H-1 AIRCRAFT Text 1987 ftdtic 2016-02-24T10:59:57Z The U.S. Army Aviation Engineering Flight Activity conducted an evaluation of the Pneumatic Boot Deicing System (PBDS) with two pneumatic deicer boot designs, referred to as second and third generation. The objective of the test was to conduct feasibility testing of the pneumatic system concept for deicing helicopter rotor blades in forward flight, and to assess any changes to aircraft performance and handling qualities. Phase I consisted of a ground and inflight structural loads survey which established an operational envelope. Phase 2 consisted of forward flight testing in artificial and natural icing conditions of the second generation design only. Phase 3 consisted of limited artificial rain erosion tests of the second generation design. Phase 4 consisted of performance and handling qualities evaluation of the second generation design. Hover and level flight performance were greatly improved over the first generation, but a significant performance penalty still exists. Handling qualities were essentially unchanged from the standard UH-1H. Two unsatisfactory and six undesirable reliability and maintainability characteristics were identified. Text Ice permafrost Defense Technical Information Center: DTIC Technical Reports database
institution Open Polar
collection Defense Technical Information Center: DTIC Technical Reports database
op_collection_id ftdtic
language English
topic Helicopters
Snow
Ice and Permafrost
*DEICING SYSTEMS
*ROTOR BLADES(ROTARY WINGS)
AIRCRAFT
BOOTS
ENVELOPE(SPACE)
FEASIBILITY STUDIES
FLIGHT TESTING
HANDLING
HELICOPTER ROTORS
HOVERING
ICE FORMATION
INFLIGHT
LEVEL FLIGHT
LOADS(FORCES)
PENALTIES
PERFORMANCE(ENGINEERING)
PNEUMATIC EQUIPMENT
QUALITY
RELIABILITY
STRUCTURAL PROPERTIES
SURVEYS
TEST AND EVALUATION
PBDS(PNEUMATIC BOOT DEICING SYSTEM)
JUH-1H AIRCRAFT
H-1 AIRCRAFT
spellingShingle Helicopters
Snow
Ice and Permafrost
*DEICING SYSTEMS
*ROTOR BLADES(ROTARY WINGS)
AIRCRAFT
BOOTS
ENVELOPE(SPACE)
FEASIBILITY STUDIES
FLIGHT TESTING
HANDLING
HELICOPTER ROTORS
HOVERING
ICE FORMATION
INFLIGHT
LEVEL FLIGHT
LOADS(FORCES)
PENALTIES
PERFORMANCE(ENGINEERING)
PNEUMATIC EQUIPMENT
QUALITY
RELIABILITY
STRUCTURAL PROPERTIES
SURVEYS
TEST AND EVALUATION
PBDS(PNEUMATIC BOOT DEICING SYSTEM)
JUH-1H AIRCRAFT
H-1 AIRCRAFT
Graham, Matthew S
Haworth, Loran A
Kimberly, Jack L
JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation
topic_facet Helicopters
Snow
Ice and Permafrost
*DEICING SYSTEMS
*ROTOR BLADES(ROTARY WINGS)
AIRCRAFT
BOOTS
ENVELOPE(SPACE)
FEASIBILITY STUDIES
FLIGHT TESTING
HANDLING
HELICOPTER ROTORS
HOVERING
ICE FORMATION
INFLIGHT
LEVEL FLIGHT
LOADS(FORCES)
PENALTIES
PERFORMANCE(ENGINEERING)
PNEUMATIC EQUIPMENT
QUALITY
RELIABILITY
STRUCTURAL PROPERTIES
SURVEYS
TEST AND EVALUATION
PBDS(PNEUMATIC BOOT DEICING SYSTEM)
JUH-1H AIRCRAFT
H-1 AIRCRAFT
description The U.S. Army Aviation Engineering Flight Activity conducted an evaluation of the Pneumatic Boot Deicing System (PBDS) with two pneumatic deicer boot designs, referred to as second and third generation. The objective of the test was to conduct feasibility testing of the pneumatic system concept for deicing helicopter rotor blades in forward flight, and to assess any changes to aircraft performance and handling qualities. Phase I consisted of a ground and inflight structural loads survey which established an operational envelope. Phase 2 consisted of forward flight testing in artificial and natural icing conditions of the second generation design only. Phase 3 consisted of limited artificial rain erosion tests of the second generation design. Phase 4 consisted of performance and handling qualities evaluation of the second generation design. Hover and level flight performance were greatly improved over the first generation, but a significant performance penalty still exists. Handling qualities were essentially unchanged from the standard UH-1H. Two unsatisfactory and six undesirable reliability and maintainability characteristics were identified.
author2 ARMY AVIATION ENGINEERING FLIGHT ACTIVITY EDWARDS AFB CA
format Text
author Graham, Matthew S
Haworth, Loran A
Kimberly, Jack L
author_facet Graham, Matthew S
Haworth, Loran A
Kimberly, Jack L
author_sort Graham, Matthew S
title JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation
title_short JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation
title_full JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation
title_fullStr JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation
title_full_unstemmed JUH-1H Redesigned Pneumatic Boot Deicing System Flight Test Evaluation
title_sort juh-1h redesigned pneumatic boot deicing system flight test evaluation
publishDate 1987
url http://www.dtic.mil/docs/citations/ADA194918
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA194918
genre Ice
permafrost
genre_facet Ice
permafrost
op_source DTIC AND NTIS
op_relation http://www.dtic.mil/docs/citations/ADA194918
op_rights Approved for public release; distribution is unlimited.
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